CA2437985C - Adjustable trailer underbody fairing - Google Patents
Adjustable trailer underbody fairing Download PDFInfo
- Publication number
- CA2437985C CA2437985C CA002437985A CA2437985A CA2437985C CA 2437985 C CA2437985 C CA 2437985C CA 002437985 A CA002437985 A CA 002437985A CA 2437985 A CA2437985 A CA 2437985A CA 2437985 C CA2437985 C CA 2437985C
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- Canada
- Prior art keywords
- fairing
- trailer
- assembly
- adjustable
- panel
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- Expired - Fee Related
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- 239000004744 fabric Substances 0.000 claims description 20
- 239000000446 fuel Substances 0.000 description 5
- 238000004146 energy storage Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 229920002430 Fibre-reinforced plastic Polymers 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- XMQFTWRPUQYINF-UHFFFAOYSA-N bensulfuron-methyl Chemical class COC(=O)C1=CC=CC=C1CS(=O)(=O)NC(=O)NC1=NC(OC)=CC(OC)=N1 XMQFTWRPUQYINF-UHFFFAOYSA-N 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 239000011151 fibre-reinforced plastic Substances 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- 238000009958 sewing Methods 0.000 description 1
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/80—Technologies aiming to reduce greenhouse gasses emissions common to all road transportation technologies
- Y02T10/88—Optimized components or subsystems, e.g. lighting, actively controlled glasses
Landscapes
- Body Structure For Vehicles (AREA)
- Vehicle Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)
Abstract
An adjustable trailer underbody fairing for a trailer having an adjustable rear wheel assembly and a corresponding tractor unit having rear wheels, the fairing including first arid second fairing sections attached to the rear wheel assembly and trailer, respectively, and an adjustable fairing panel coupled to the first and second fairing sections that extends and collapses as the rear wheel assembly is moved to present a planar fairing surface at alt times. The fairing can be selectively raised to provide access beneath the trailer.
Description
ADJUSTABLE TRAILER UNDERBODY FAIRING
BACKGROUND OF THE INVENTION
Field of the Invention The present invention pertains to trailer fairings, and: more particularly to a longitudinally and vertically adjustable trailer underbody fairing.
Description of the Related Art It is known that fuel economy can be improved in the long-distance haulage of trailers by utilizing fairings.mounted beneath each of the trailer's lower, outer longitudinal edges. Ideally, such fairings extend between the rear trailer wheel assembly and the wheels of a tractor unit attached to the front of the trailer.
The trailer wheel assembly is commonly longitudinally repositioned relative to the trailer to achieve proper load distribution. If the fairing cannot be adjusted quickly and easily to accommodate repositioning of the wheel assembly, then the length of the fairing will. not be optimized to reach maximum fuel economy.
Hence, the length of the fairing must be reduced to ensure that the wheel assembly can be repositioned throughout its entire range without interfering with the fairing.
Prior fairing designs did not accommodate longitudinal adjustment, resulting- in substantial gaps between the fairing and the wheel assembly.
Such gaps reduce the fairing's efficiency, and hence fuel economy, resu6ting.in greater fuel costs.
~
Attempts to overcome this disadvantage have resulted in complex, heavy fairing assemblies that, while perhaps achieving some aerodynamic efficiency, offset the resulting fuel economy with increased vveight_ That, as well as the cost of manufacturing such complicated devices and a reluctance of drivers and mechanics to use such devices, have made them unfeasible. Hence, there is a need for a lightweight, low cost, easily-adjustable fairing that maximizes aerodynamic flow of air around the trailer and that is easy to use when repositioning the rear wheels in order to minimize gaps between the fairing and the wheels of the trailer and tractor unit_ BRIEF SUMMARY OF THE INVENTION
The disclosed and claimed embodiments of the invention are directed to a fairing for a trailer, the trailer having an adjustable rear wheel assembly and configured for attachment to a tractor unit also having rear wheels, the fairing including a first fairing section configured for attachment to the trailer rear wheel assembly, a second fairing section configured for attachment to the trailer adjacent the front of the trailer and the rear wheels of the tractor unit and in slideable engagement with the first fairing section; and an adjustable fairing panel coupled to the first and second fairing sections, the adjustable fairing panel configured to extend and collapse as the position of the rear wheel assembly is adjusted longitudinally relative to the trailer.
In accordance with another aspect of the present invention, a fairing is. provided that includes a teiescopic frame having a foldable panel attached thereto. Ideally, the foldable panel includes a plurality of vertically-oriented slats slideabfy mounted on the telescopic frame, the plurality of slats having fabric mounted thereon. Preferably, the slats are mounted to rotate about a vertical axis to guide the foldable panel into a collapsed configuration and to facilitate extension of the panel_ In a-ccordance with a further aspect of the present invention, the foldable panel is constructed of fabric that, ideally, is mounted under tension on the telescopic frame.
In accordance with another embodiment of the invention, a fairing for a trailer is provided having a fairing mount system that permits the fairing to move between a lowered operational configuration and an extended and raised configuration for access to the underside of the trailer. Ideally, the fairing is slideably mounted to the fairing mounts to vertically slide with respect to the fairing mounts.
As will be readity appreciated from the foregoing, the fairing of the present invention is a light-weight planar structure designed to control airflow on the lower sides of a conventional trailer, including freight box vans. The planar structure is positioned parallel to and below the sides of the trailer extending from forward of the trailer wheels to just after the tractor wheels, and it extends as close as practical to the ground. The fairing structure enables covering a variable area between the trailer and tractor wheels, which can be adjustable axially by up to as much as eleven feet.
BRiEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWING(S) The foregoing features and advantages of the present invention will be more readily appreciated as the same become better understood from the following detailed description when taken in conjunction with the accompanying drawings, wherein:
Figure 1 is a side elevational view of a tractor unit coupled to a main trailer and a pup trailer, both trailers having fairings formed in accordance with the present invention;
Figure 2 is a side elevational view of a tractor unit coupled to a single trailer having a fairing formed in accordance with the present invention;
BACKGROUND OF THE INVENTION
Field of the Invention The present invention pertains to trailer fairings, and: more particularly to a longitudinally and vertically adjustable trailer underbody fairing.
Description of the Related Art It is known that fuel economy can be improved in the long-distance haulage of trailers by utilizing fairings.mounted beneath each of the trailer's lower, outer longitudinal edges. Ideally, such fairings extend between the rear trailer wheel assembly and the wheels of a tractor unit attached to the front of the trailer.
The trailer wheel assembly is commonly longitudinally repositioned relative to the trailer to achieve proper load distribution. If the fairing cannot be adjusted quickly and easily to accommodate repositioning of the wheel assembly, then the length of the fairing will. not be optimized to reach maximum fuel economy.
Hence, the length of the fairing must be reduced to ensure that the wheel assembly can be repositioned throughout its entire range without interfering with the fairing.
Prior fairing designs did not accommodate longitudinal adjustment, resulting- in substantial gaps between the fairing and the wheel assembly.
Such gaps reduce the fairing's efficiency, and hence fuel economy, resu6ting.in greater fuel costs.
~
Attempts to overcome this disadvantage have resulted in complex, heavy fairing assemblies that, while perhaps achieving some aerodynamic efficiency, offset the resulting fuel economy with increased vveight_ That, as well as the cost of manufacturing such complicated devices and a reluctance of drivers and mechanics to use such devices, have made them unfeasible. Hence, there is a need for a lightweight, low cost, easily-adjustable fairing that maximizes aerodynamic flow of air around the trailer and that is easy to use when repositioning the rear wheels in order to minimize gaps between the fairing and the wheels of the trailer and tractor unit_ BRIEF SUMMARY OF THE INVENTION
The disclosed and claimed embodiments of the invention are directed to a fairing for a trailer, the trailer having an adjustable rear wheel assembly and configured for attachment to a tractor unit also having rear wheels, the fairing including a first fairing section configured for attachment to the trailer rear wheel assembly, a second fairing section configured for attachment to the trailer adjacent the front of the trailer and the rear wheels of the tractor unit and in slideable engagement with the first fairing section; and an adjustable fairing panel coupled to the first and second fairing sections, the adjustable fairing panel configured to extend and collapse as the position of the rear wheel assembly is adjusted longitudinally relative to the trailer.
In accordance with another aspect of the present invention, a fairing is. provided that includes a teiescopic frame having a foldable panel attached thereto. Ideally, the foldable panel includes a plurality of vertically-oriented slats slideabfy mounted on the telescopic frame, the plurality of slats having fabric mounted thereon. Preferably, the slats are mounted to rotate about a vertical axis to guide the foldable panel into a collapsed configuration and to facilitate extension of the panel_ In a-ccordance with a further aspect of the present invention, the foldable panel is constructed of fabric that, ideally, is mounted under tension on the telescopic frame.
In accordance with another embodiment of the invention, a fairing for a trailer is provided having a fairing mount system that permits the fairing to move between a lowered operational configuration and an extended and raised configuration for access to the underside of the trailer. Ideally, the fairing is slideably mounted to the fairing mounts to vertically slide with respect to the fairing mounts.
As will be readity appreciated from the foregoing, the fairing of the present invention is a light-weight planar structure designed to control airflow on the lower sides of a conventional trailer, including freight box vans. The planar structure is positioned parallel to and below the sides of the trailer extending from forward of the trailer wheels to just after the tractor wheels, and it extends as close as practical to the ground. The fairing structure enables covering a variable area between the trailer and tractor wheels, which can be adjustable axially by up to as much as eleven feet.
BRiEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWING(S) The foregoing features and advantages of the present invention will be more readily appreciated as the same become better understood from the following detailed description when taken in conjunction with the accompanying drawings, wherein:
Figure 1 is a side elevational view of a tractor unit coupled to a main trailer and a pup trailer, both trailers having fairings formed in accordance with the present invention;
Figure 2 is a side elevational view of a tractor unit coupled to a single trailer having a fairing formed in accordance with the present invention;
Figure 3 is an isometric projection of a fairing assembly formed in accordance with the present invention;
Figure 4 is an isometric projection of the fairing assembly of Figure 3 in an extended configuration;
Figure 5 is an enlarged partial view of a fairing mount and a portion of the fairing assembly of Figure 4;
Figure 6 is an isometric projection of a fairing mount in an operational configuration;
Figure 7 is an isometric view of the fairing mount of Figure 6 in an unlatched and extended configuration;
Figure 8 is an enlarged view of the fairing of Figure 4 showing the collapsible fairing panel in a partially-collapsed configuration;
Figure 9 is an isometric projection of a portion of an alternative embodiment of a fairing assembly of the present invention showing the foldable fairing panel in an extended configuration;
Figure 10 is an isometric projection of a slider mount in an assembled configuration;
Figure 11 is an exploded isometric projection of the slider mount of Figure 10;
Figure 12 is an isometric projection of one configuration of a slat for use in the foldable panel of the present invention;
Figure 13 is an isometric projection of a fairing frame section formed in accordance with the present invention;
Figure 14 is an isometric projection of a fairing frame gusset of the present invention; and Figure 15 is an isometric projection of an attemative embodiment of a collapsible fairing panel using a take-up spool_ DETAILED DESCRIPTION OF THE INVENTION
Referring initially to Figure 1, shown therein is a tractor trailer unit 20 having a tractor 22 coupled to a main trailer 24 that in turn is coupled to a pup trailer 26. A first adjustable fairing 28 is shown in solid lines in an operational configuration on the main trailer 24. Similarly, a second adjustable fairing 30 is shown in an operational configuration on the pup trailer 26 in solid lines and in a raised configuration in dashed lines.
The present invention is also adaptable for use with a tractor trailer unit 32 having a tractor 34 and a single trailer 36. Here, an adjustable fairing 38 is shown in solid lines in an operational configuration and in dashed lines in a raised configuration_ In the embodiment shown in Figure 2, the trailer 36 has a rear wheel assembly 40 mounted thereon to slide longitudinally (towards and away from the rear wheels 33 of the tractor 34), as shown by the solid lines of the rear wheel assembly 40 in a forward position and the dashed lines in a rearward position_ The adjustable fairing 38 includes an adjustable fairing panel 42 that folds and unfolds in an accordion-like fashion to permit adjustment in the fairing 38.
Referring next to Figure 3, shown therein is a fairing assembly 44 formed in accordance with one embodiment of the invention.. The fairing assembly 44 includes a first fairing section 46 slideably attached to a second fairing section 48, preferably in telescopic fashion. An adjustable fairing panel 50 is slideably mounted to the second fairing section 48 and coupled to the first fairing section 46 to collapse and extend in response to movement of the first and second fairing sections 46, 48 with respect to each other. Lifting mounts 52 are shown in slideable engagement with a fairing mount 54 on the first and second fairing sections 46, 48. A third fairing mount 54 is shown near the center of the fairing assembly'where the first and second_ fairing sections 46, 48 are telescopically joined. For purposes of illustration, the corresponding lifting mount is not shown.
Figure 4 is an isometric projection of the fairing assembly of Figure 3 in an extended configuration;
Figure 5 is an enlarged partial view of a fairing mount and a portion of the fairing assembly of Figure 4;
Figure 6 is an isometric projection of a fairing mount in an operational configuration;
Figure 7 is an isometric view of the fairing mount of Figure 6 in an unlatched and extended configuration;
Figure 8 is an enlarged view of the fairing of Figure 4 showing the collapsible fairing panel in a partially-collapsed configuration;
Figure 9 is an isometric projection of a portion of an alternative embodiment of a fairing assembly of the present invention showing the foldable fairing panel in an extended configuration;
Figure 10 is an isometric projection of a slider mount in an assembled configuration;
Figure 11 is an exploded isometric projection of the slider mount of Figure 10;
Figure 12 is an isometric projection of one configuration of a slat for use in the foldable panel of the present invention;
Figure 13 is an isometric projection of a fairing frame section formed in accordance with the present invention;
Figure 14 is an isometric projection of a fairing frame gusset of the present invention; and Figure 15 is an isometric projection of an attemative embodiment of a collapsible fairing panel using a take-up spool_ DETAILED DESCRIPTION OF THE INVENTION
Referring initially to Figure 1, shown therein is a tractor trailer unit 20 having a tractor 22 coupled to a main trailer 24 that in turn is coupled to a pup trailer 26. A first adjustable fairing 28 is shown in solid lines in an operational configuration on the main trailer 24. Similarly, a second adjustable fairing 30 is shown in an operational configuration on the pup trailer 26 in solid lines and in a raised configuration in dashed lines.
The present invention is also adaptable for use with a tractor trailer unit 32 having a tractor 34 and a single trailer 36. Here, an adjustable fairing 38 is shown in solid lines in an operational configuration and in dashed lines in a raised configuration_ In the embodiment shown in Figure 2, the trailer 36 has a rear wheel assembly 40 mounted thereon to slide longitudinally (towards and away from the rear wheels 33 of the tractor 34), as shown by the solid lines of the rear wheel assembly 40 in a forward position and the dashed lines in a rearward position_ The adjustable fairing 38 includes an adjustable fairing panel 42 that folds and unfolds in an accordion-like fashion to permit adjustment in the fairing 38.
Referring next to Figure 3, shown therein is a fairing assembly 44 formed in accordance with one embodiment of the invention.. The fairing assembly 44 includes a first fairing section 46 slideably attached to a second fairing section 48, preferably in telescopic fashion. An adjustable fairing panel 50 is slideably mounted to the second fairing section 48 and coupled to the first fairing section 46 to collapse and extend in response to movement of the first and second fairing sections 46, 48 with respect to each other. Lifting mounts 52 are shown in slideable engagement with a fairing mount 54 on the first and second fairing sections 46, 48. A third fairing mount 54 is shown near the center of the fairing assembly'where the first and second_ fairing sections 46, 48 are telescopically joined. For purposes of illustration, the corresponding lifting mount is not shown.
The adjustable fairing panel 50 is shown in Figure 3 in a fully extended configuration so that the fairing assembly 44 is at its maximum length. In addition; the lifting mounts 52 are shown in an unlatched and partially extended configuration but without the first and second fairing sections 46, 48 in a raised position. Figure 4 shows the first and second fairing sections 46,48 in a raised position relative to the lifting mounts 52_ A more detailed view of the second fairing section with respect to its relationship with the lifting mount 52 is shown in Figure 5. As can be seen in Figures 4 and 5, the first and second fairing sections 46, 48 slide vertically relative to the lifting mount 52.
A single lifting mount 52 is shown in Figures 6*and 7 having a T-shaped bar or T-bar 56 rotatably mounted to a lower moving member 58. The T-bar 56 has a top end 60 that engages a top bar 62. Parallel swing arms 64 are pivotally coupled to the, top bar 62 and the lower moving member 58 to permit movement of the lower moving member 58 refative to the top bar 62. A mounting plate 66 is fixedly attached to the top bar 62 to provide an attachment point to the trailer 36 or rear wheel assembly 40. ldeally, the mounting plate 66 is sized .to straddle at least tinro longitudinal rails beneath the trailer (not shown) or channels (not shown) on the exterior bottom of the trailer.
The top bar 62 in this embodiment of the invention comprises a hollow tube having a square-shaped cross-sectional configuration with a projecting end 68. A slot 70 forrned in a top wall 72 and a bottom wall 74 of the projecting end 68 that is sized and shaped to receive the stem 76 on the T-bar 56. The stem 76 is retained within the slot 70 by a conventional slam latch (not shown) which is known to those of skill in the art and readily commercially available. Hence, the slam latch will not be described in more detail herein. Atternativel.y, other retaining methods may be used, such as a retaining pin slid through openings in the stem 76 and the top bar 62.
Each lifting mount 52 includes an energy storage device, such as a gas spring 78, mounted in the internal axial bore 80 of the lower moving i-nember 58. The gas spring 78 is coupled to a pair of cables 82 that extend through openings 84 in the T-bar 56. Preferably, the cables 82 lie within channels (not shoWn) formed in the exposed face 86 of the T-bar 56. These cables 82 are used to support the first and second fairing sections 46, 48 on the lifting mounts 52, as will be described in more detail hereinbelow.
As shown in Figure 7, when the T-bar 56 is unlatched from the top bar 62, the lower moving member 58 is free to extend outward via the parallel swing arms 64 such that the T-bar 56 is maintained in at least the same vertical orientation or is permitted to pivot slightly outward with the top end 60 extending away from the top bar 62. This is the configuration shown for the lifting mounts 52 in Figure 3.
Referring again to Figure 5, the fairing mount 54 comprises a planar back wall 88 having a pair of longitudinal channels 90 formed along each longitudinal side thereof. The fairing mount 54 is sized and shaped to be slideably received over the T-bar 56 as shown in Figure 5. Thus, the fairing mount 54 slides longitudinally along the T-bar 56 to move the first and second fairing sections 46, 48 from a lowered operational configuration (shown in Figure 2) to a raised configuration (shown in phantom in Figure 2 and in Figures 4 and 5). The fairing mount 54 is prevented from sliding off the T-bar 56 by attachment of the cable ends 92 to respective attachment points (not shown) on the fairing mount 54.
The cables 82 also are Used to raise the first and second fairing sections 46, 48 via operation of the gas spring 78. It is to be understood that other energy storage elements may be used, such as a mechanical spring, as will be known to those skilled in the art.
The fairing sections 46, 48 are formed around a tubular frame 94 made up of longitudinal runners 96, 98 and transverse supports 100 that form a ladder-type structure, as shown in Figure 13_ Frame gussets 102 are used to couple the transverse supports 100 to the longitudinal runners 96, 98:
A single lifting mount 52 is shown in Figures 6*and 7 having a T-shaped bar or T-bar 56 rotatably mounted to a lower moving member 58. The T-bar 56 has a top end 60 that engages a top bar 62. Parallel swing arms 64 are pivotally coupled to the, top bar 62 and the lower moving member 58 to permit movement of the lower moving member 58 refative to the top bar 62. A mounting plate 66 is fixedly attached to the top bar 62 to provide an attachment point to the trailer 36 or rear wheel assembly 40. ldeally, the mounting plate 66 is sized .to straddle at least tinro longitudinal rails beneath the trailer (not shown) or channels (not shown) on the exterior bottom of the trailer.
The top bar 62 in this embodiment of the invention comprises a hollow tube having a square-shaped cross-sectional configuration with a projecting end 68. A slot 70 forrned in a top wall 72 and a bottom wall 74 of the projecting end 68 that is sized and shaped to receive the stem 76 on the T-bar 56. The stem 76 is retained within the slot 70 by a conventional slam latch (not shown) which is known to those of skill in the art and readily commercially available. Hence, the slam latch will not be described in more detail herein. Atternativel.y, other retaining methods may be used, such as a retaining pin slid through openings in the stem 76 and the top bar 62.
Each lifting mount 52 includes an energy storage device, such as a gas spring 78, mounted in the internal axial bore 80 of the lower moving i-nember 58. The gas spring 78 is coupled to a pair of cables 82 that extend through openings 84 in the T-bar 56. Preferably, the cables 82 lie within channels (not shoWn) formed in the exposed face 86 of the T-bar 56. These cables 82 are used to support the first and second fairing sections 46, 48 on the lifting mounts 52, as will be described in more detail hereinbelow.
As shown in Figure 7, when the T-bar 56 is unlatched from the top bar 62, the lower moving member 58 is free to extend outward via the parallel swing arms 64 such that the T-bar 56 is maintained in at least the same vertical orientation or is permitted to pivot slightly outward with the top end 60 extending away from the top bar 62. This is the configuration shown for the lifting mounts 52 in Figure 3.
Referring again to Figure 5, the fairing mount 54 comprises a planar back wall 88 having a pair of longitudinal channels 90 formed along each longitudinal side thereof. The fairing mount 54 is sized and shaped to be slideably received over the T-bar 56 as shown in Figure 5. Thus, the fairing mount 54 slides longitudinally along the T-bar 56 to move the first and second fairing sections 46, 48 from a lowered operational configuration (shown in Figure 2) to a raised configuration (shown in phantom in Figure 2 and in Figures 4 and 5). The fairing mount 54 is prevented from sliding off the T-bar 56 by attachment of the cable ends 92 to respective attachment points (not shown) on the fairing mount 54.
The cables 82 also are Used to raise the first and second fairing sections 46, 48 via operation of the gas spring 78. It is to be understood that other energy storage elements may be used, such as a mechanical spring, as will be known to those skilled in the art.
The fairing sections 46, 48 are formed around a tubular frame 94 made up of longitudinal runners 96, 98 and transverse supports 100 that form a ladder-type structure, as shown in Figure 13_ Frame gussets 102 are used to couple the transverse supports 100 to the longitudinal runners 96, 98:
As shown in Figure 14, each of the gussets 102 has the configuration shown therein, which includes a base 104 having a curved bottom surface 106 sized and shaped to mate with the exterior of the longitudinal runners 96, 98., and a socket 108 projecting outward from the base 104_ A pair of triangular-shaped braces 110 reinforce the socket 108 on the base 104. The socket 108 includes an opening 112 sized-and shaped to receive the transverse support 100 therein in slideable engagement. Openings 112 are formed in the braces that receive a hook 114. Ideally the hook 114 is in the shape of a question mark.
The first fairing section 46 has its tubular frame 116 sized and shaped so that the longitudinal runners are slideably engaged with the tubular frame 118 of the second fairing section 48. Ideally, the one tubular frame - telescopically cooperates with the other tubular frame in the same manher as a trombone slide to extend and retract, thereby changing the overall length of the fairing assembly 44. The tubular frame 116 of the first fairing section 46 may be the larger or the smaller of the frame members to receive the tubular frame 118 of the second fairing section 48.
The fairing assembly 44. includes fairing panels 120 mounted to the tubular firarnes 116, 118 to form the skin of the fairing. Ideally, each fairing panel 120 is formed of a fiber reinforced plastic fabric that is cut and sewn together such that it can be attached at points along the length of each of the tubular frames 116, 118. To accommodate attachment of the fairing panels 120 to the frames 116, 118, rigid circular fasteners or D-rings 122 are sown into the comers of the fairing panels 120 for attachment to the hooks 114 on the gussets 102. Thus, the skin of the fairing assembly is divided up irato connected rectangular panels 120 with a pattern of grommet-reinforced holes 124 near the center of each panel 120. A
chord (not shown) can be inserted through these holes 124 and tightened to place each panel 120 in tension between the four corner attachment points, the D-rings 122; thus creating a structure fabricated from the tubular frame with the transverse members and the fairing panels 120.
The first fairing section 46 has its tubular frame 116 sized and shaped so that the longitudinal runners are slideably engaged with the tubular frame 118 of the second fairing section 48. Ideally, the one tubular frame - telescopically cooperates with the other tubular frame in the same manher as a trombone slide to extend and retract, thereby changing the overall length of the fairing assembly 44. The tubular frame 116 of the first fairing section 46 may be the larger or the smaller of the frame members to receive the tubular frame 118 of the second fairing section 48.
The fairing assembly 44. includes fairing panels 120 mounted to the tubular firarnes 116, 118 to form the skin of the fairing. Ideally, each fairing panel 120 is formed of a fiber reinforced plastic fabric that is cut and sewn together such that it can be attached at points along the length of each of the tubular frames 116, 118. To accommodate attachment of the fairing panels 120 to the frames 116, 118, rigid circular fasteners or D-rings 122 are sown into the comers of the fairing panels 120 for attachment to the hooks 114 on the gussets 102. Thus, the skin of the fairing assembly is divided up irato connected rectangular panels 120 with a pattern of grommet-reinforced holes 124 near the center of each panel 120. A
chord (not shown) can be inserted through these holes 124 and tightened to place each panel 120 in tension between the four corner attachment points, the D-rings 122; thus creating a structure fabricated from the tubular frame with the transverse members and the fairing panels 120.
In the embodiment shown in Figure 9, the fairing panels 120 include a flap 126 that is attached to the panel at each location of the transverse supports 100 and guided around the transverse supports so that it is captured between the flap 126 and the fairing panel 120. The flap 126 can be closed by running a chord through reinforced grommet holes (not shown) between the flap 126 and the main fabric fairing panel 120. Altematively, the entire fabric panel 120 can be constructed to fit over the tubular transverse supports 100 in the manner of a sleeve and then tensioned with a chord placed in grommet-reinforced holes and tightened. It is important that the fabric panels 120 be as tight as possible over the supporting tubular frames 116,-118 to avoid damage caused by aerodynamic forces moving the fabric rapidly against the tubular frames 116, 118.
Because the wheel assembly 40 has approximately an eleven-foot range of longitudinal movement, the eleven-foot span must be covered to ensure continuity of the aerodynamic surface. In one embodiment of the invention, a plurality of slats 128 (see Figure 8) are attached to the tubular frames 116 or 118 and covered with fabric 130 to form an accordion-like structure that folds and unfolds in response to telescopic rr~ovement of the first and second tubular frames 116, 118. Each slat 128 has a pivot point 132 formed at a top 134 and bottom thereof. These pivot points are mounted in corresponding slider mounts 138, which are shown in more detail in Figures 10 and 11. Each slider mount is formed of first and second halves 140, 142 that are pivotally attached together at the top by a hinge pin 144 and at the bottorn by suitable fasteners (not shown). A
slot 146 is formed in the bottom of each of the first and second halves 140, 142 that is sized and shaped to receive and capture the pivot point 132 on the slat 128.
In this mariner, the slat 128 can rotate about the pivot points 132 in each of the slider mounts 138.
ln addition, each slider mount 138 includes a plurality of reiller bearings or rollers 148, in this case three rollers 148, that are positioned around the interior of a tongitudinal bore 150 formed by the two halves 140, 142 to thereby bear against and provide a friction-free movement of the slider mount 138 on the tubular frames 116, 118.
Each slat 128, as shown in Figure 12, has a plurality of holes 152 formed therein to lighten the weight of the slats. Preferably, the slats are covered by the fabric 138, and preferably are attached to the fabric by sewing, bonding, or other known method, to eliminate vibration.caused by the wind. The fabric 130 is sewn together between each slat 128 to fotm a hinge point for folding of the fabric 130 as the fairing assembly collapses, as shown in Figure 8.
Thus, with the rear wheel assembly or bogey 40 in the completely extended 'configuration, as shown in Figure 9, the adjustable fairing panel 50 presents a completely planar surface where all slats are coplanar; and in the completely retracted or compressed position, the slats are al1 collapsed together in a face-to-face arrangement In an altemative embodiment a spring-powened take-up spool is mounted on the tubular frame 156 adjacent a stationary fairing panel 120. A
fabric sheet 158 has one end attached to a transverse support 100 and the other end, rolled up on- the spool 154. The spool 154 is attached to a first fairing section 160 that is telescopically engaged with a second fairing section 162 having the point of slideable engagement 164 positioned between the transverse support 100 and the spool 154. Longitudinal movement of the first fairing section relative to the second fairing section 162 causes the sheet 158 to roll up on the spool 154 and to unroll from the spool 154, providing a continuous planar surface at all times, regardless of the overall length or relative position of the first and second fairing secfions 160, 162. Altematively, a rigid planar fabric support attadied to either of the first and second fairing sections could be utilized that would move in a parallel bypass track to the main planar structure. A spring-loaded roller would maintain tension in the make-up fabric loop connecting the support panel to the inain fabric sheet , , .. , From the foregoing it will be appreciated that, although specific embodiments of the invention have been described herein for purposes of illustration, various modifications may be made without deviating from the spirit and soope of the invention. Accordingly, the invention is not limited except as by the appended claims and the equivalents thereof.
Because the wheel assembly 40 has approximately an eleven-foot range of longitudinal movement, the eleven-foot span must be covered to ensure continuity of the aerodynamic surface. In one embodiment of the invention, a plurality of slats 128 (see Figure 8) are attached to the tubular frames 116 or 118 and covered with fabric 130 to form an accordion-like structure that folds and unfolds in response to telescopic rr~ovement of the first and second tubular frames 116, 118. Each slat 128 has a pivot point 132 formed at a top 134 and bottom thereof. These pivot points are mounted in corresponding slider mounts 138, which are shown in more detail in Figures 10 and 11. Each slider mount is formed of first and second halves 140, 142 that are pivotally attached together at the top by a hinge pin 144 and at the bottorn by suitable fasteners (not shown). A
slot 146 is formed in the bottom of each of the first and second halves 140, 142 that is sized and shaped to receive and capture the pivot point 132 on the slat 128.
In this mariner, the slat 128 can rotate about the pivot points 132 in each of the slider mounts 138.
ln addition, each slider mount 138 includes a plurality of reiller bearings or rollers 148, in this case three rollers 148, that are positioned around the interior of a tongitudinal bore 150 formed by the two halves 140, 142 to thereby bear against and provide a friction-free movement of the slider mount 138 on the tubular frames 116, 118.
Each slat 128, as shown in Figure 12, has a plurality of holes 152 formed therein to lighten the weight of the slats. Preferably, the slats are covered by the fabric 138, and preferably are attached to the fabric by sewing, bonding, or other known method, to eliminate vibration.caused by the wind. The fabric 130 is sewn together between each slat 128 to fotm a hinge point for folding of the fabric 130 as the fairing assembly collapses, as shown in Figure 8.
Thus, with the rear wheel assembly or bogey 40 in the completely extended 'configuration, as shown in Figure 9, the adjustable fairing panel 50 presents a completely planar surface where all slats are coplanar; and in the completely retracted or compressed position, the slats are al1 collapsed together in a face-to-face arrangement In an altemative embodiment a spring-powened take-up spool is mounted on the tubular frame 156 adjacent a stationary fairing panel 120. A
fabric sheet 158 has one end attached to a transverse support 100 and the other end, rolled up on- the spool 154. The spool 154 is attached to a first fairing section 160 that is telescopically engaged with a second fairing section 162 having the point of slideable engagement 164 positioned between the transverse support 100 and the spool 154. Longitudinal movement of the first fairing section relative to the second fairing section 162 causes the sheet 158 to roll up on the spool 154 and to unroll from the spool 154, providing a continuous planar surface at all times, regardless of the overall length or relative position of the first and second fairing secfions 160, 162. Altematively, a rigid planar fabric support attadied to either of the first and second fairing sections could be utilized that would move in a parallel bypass track to the main planar structure. A spring-loaded roller would maintain tension in the make-up fabric loop connecting the support panel to the inain fabric sheet , , .. , From the foregoing it will be appreciated that, although specific embodiments of the invention have been described herein for purposes of illustration, various modifications may be made without deviating from the spirit and soope of the invention. Accordingly, the invention is not limited except as by the appended claims and the equivalents thereof.
Claims (16)
1. A fairing for a trailer having an adjustable rear wheel assembly and a corresponding tractor unit having rear wheels, the fairing comprising:
a first fairing section configured for attachment to the trailer rear wheel assembly;
a second fairing section configured for attachment to the trailer; and an adjustable fairing panel coupled to the first and second fairing sections and configured to extend and collapse as the position of the rear wheel assembly is adjusted longitudinally on the trailer.
a first fairing section configured for attachment to the trailer rear wheel assembly;
a second fairing section configured for attachment to the trailer; and an adjustable fairing panel coupled to the first and second fairing sections and configured to extend and collapse as the position of the rear wheel assembly is adjusted longitudinally on the trailer.
2. The fairing of claim 1 wherein the first and second fairing sections comprise a telescopic frame having a first frame member telescopically coupled to a second frame member.
3. The fairing of claim 2 wherein the adjustable fairing panel comprises a plurality of vertically-oriented slats having a foldable panel mounted thereon.
4. The fairing of claim 3 wherein the plurality of slats are slideably mounted to the telescopic frame and configured to rotate about a vertical axis to guide folding and unfolding of the foldable panel.
5. The fairing of claim 4 wherein the foldable panel is constructed of fabric.
6. The fairing of claim 5 wherein the fabric is mounted to the telescopic frame under tension.
7. A trailer assembly for use with a tractor having a moveable rear wheel assembly, the trailer assembly comprising:
a trailer having rear wheels adjustably mounted thereon and a front configured for attachment to the tractor;
a first fairing section attached to the moveable rear wheel assembly;
a second fairing section attached to the trailer to be adjacent the rear wheels of the tractor; and an adjustable fairing panel coupled to the first and second fairing sections and configured to extend and collapse as the position of the rear wheels are adjusted longitudinally on the trailer.
a trailer having rear wheels adjustably mounted thereon and a front configured for attachment to the tractor;
a first fairing section attached to the moveable rear wheel assembly;
a second fairing section attached to the trailer to be adjacent the rear wheels of the tractor; and an adjustable fairing panel coupled to the first and second fairing sections and configured to extend and collapse as the position of the rear wheels are adjusted longitudinally on the trailer.
8. The assembly of claim 7 wherein the adjustable fairing panel comprises a foldable panel.
9. The assembly of claim 8 wherein the adjustable fairing panel comprises a plurality of vertically-oriented slats slideably mounted on a telescopic frame formed by the first and second fairing sections, the plurality of slats having the foldable panel mounted thereon.
10. The assembly of claim 9 wherein the plurality of slats are mounted to each rotate about a vertical axis to guide folding and unfolding of the foldable panel.
11. The assembly of claim 10 wherein the foldable panel is constructed of fabric.
12. The assembly of claim 11 wherein the fabric is mounted to the telescopic frame under tension.
13. The assembly of claim 7 wherein the first and second fairing sections and the adjustable fairing panel are attached to the trailer to move as a unit between a raised position and a towered position.
14. The assembly of claim 7, wherein the adjustable fairing panel comprises a plurality of slats, each slat mounted on a telescopic frame by a top slider mount and a bottom slider mount, each slider mount configured to slide on the telescopic frame and to hold the respective slat in rotatable engagement for rotation about a longitudinal axis of the slat.
15. The assembly of claim 14, wherein each slider mount includes a plurality of rollers mounted thereon to support the slider mount on the telescopic frame.
16. The assembly of claim 7, comprising a first fairing mount configured to attach the first fairing section to the movable rear wheel assembly and a second fairing mount configured to attach the second fairing section to the trailer, each fairing mount comprising at least one cable attached to an actuator on the fairing mount and attached to the corresponding fairing section for moving the corresponding fairing section relative to the fairing mount.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/229,393 | 2002-08-26 | ||
| US10/229,393 US6644720B2 (en) | 2001-08-24 | 2002-08-26 | Adjustable trailer underbody fairing |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2437985A1 CA2437985A1 (en) | 2004-02-26 |
| CA2437985C true CA2437985C (en) | 2009-06-23 |
Family
ID=31990366
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002437985A Expired - Fee Related CA2437985C (en) | 2002-08-26 | 2003-08-21 | Adjustable trailer underbody fairing |
Country Status (3)
| Country | Link |
|---|---|
| AU (1) | AU2003236394B2 (en) |
| CA (1) | CA2437985C (en) |
| MX (1) | MXPA03007660A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| NL1034363C2 (en) | 2007-08-13 | 2009-02-16 | Gandert Marcel Rita Van Raemdonck | Flow conductor for use in aerodynamic device for vehicle e.g. lorry, has thickened portions formed in front edge, and streamlined outer contours in cross section that is transverse to front edge |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4518188A (en) * | 1982-06-14 | 1985-05-21 | Witten Hans J | Aerodynamic side panels for a tractor-trailer truck |
| US4640541A (en) * | 1985-09-17 | 1987-02-03 | Fitzgerald Corporation | Under-trailer air deflector |
| US5609384A (en) * | 1996-06-20 | 1997-03-11 | Loewen; Gordon | Fairing |
-
2003
- 2003-08-21 CA CA002437985A patent/CA2437985C/en not_active Expired - Fee Related
- 2003-08-21 AU AU2003236394A patent/AU2003236394B2/en not_active Ceased
- 2003-08-26 MX MXPA03007660A patent/MXPA03007660A/en active IP Right Grant
Also Published As
| Publication number | Publication date |
|---|---|
| AU2003236394B2 (en) | 2008-09-18 |
| AU2003236394A1 (en) | 2004-03-18 |
| MXPA03007660A (en) | 2004-12-03 |
| CA2437985A1 (en) | 2004-02-26 |
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