WO1995015444A1 - Propeller shaft - Google Patents
Propeller shaft Download PDFInfo
- Publication number
- WO1995015444A1 WO1995015444A1 PCT/JP1994/001996 JP9401996W WO9515444A1 WO 1995015444 A1 WO1995015444 A1 WO 1995015444A1 JP 9401996 W JP9401996 W JP 9401996W WO 9515444 A1 WO9515444 A1 WO 9515444A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- layer
- main
- joint
- main body
- partial
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Ceased
Links
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C3/00—Shafts; Axles; Cranks; Eccentrics
- F16C3/02—Shafts; Axles
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C3/00—Shafts; Axles; Cranks; Eccentrics
- F16C3/02—Shafts; Axles
- F16C3/026—Shafts made of fibre reinforced resin
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2326/00—Articles relating to transporting
- F16C2326/01—Parts of vehicles in general
- F16C2326/06—Drive shafts
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D1/00—Couplings for rigidly connecting two coaxial shafts or other movable machine elements
- F16D1/10—Quick-acting couplings in which the parts are connected by simply bringing them together axially
- F16D2001/103—Quick-acting couplings in which the parts are connected by simply bringing them together axially the torque is transmitted via splined connections
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D3/00—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive
- F16D3/16—Universal joints in which flexibility is produced by means of pivots or sliding or rolling connecting parts
- F16D3/26—Hooke's joints or other joints with an equivalent intermediate member to which each coupling part is pivotally or slidably connected
- F16D3/38—Hooke's joints or other joints with an equivalent intermediate member to which each coupling part is pivotally or slidably connected with a single intermediate member with trunnions or bearings arranged on two axes perpendicular to one another
- F16D3/382—Hooke's joints or other joints with an equivalent intermediate member to which each coupling part is pivotally or slidably connected with a single intermediate member with trunnions or bearings arranged on two axes perpendicular to one another constructional details of other than the intermediate member
- F16D3/387—Fork construction; Mounting of fork on shaft; Adapting shaft for mounting of fork
Definitions
- the present invention relates to a propeller shaft (drive propulsion shaft) for an automobile or the like.
- propeller shafts made of fiber reinforced plastic has already been adopted.
- Such a propeller shaft made of FRP has a cylindrical body made of FRP and a metal joint provided at each end of the main body.
- the propeller shaft of an automobile transmits the torque generated by the engine to the drive wheels, and therefore requires a torsional strength of about 100 to 400 kgf ⁇ m.
- the critical rotation speed is required to be about 5,000 to 15,500 rpm so that resonance does not occur during high-speed rotation. Therefore, in order to satisfy these basic requirements, the FRP main body uses parameters such as the type and content of the reinforcing fiber, the orientation of the reinforcing fiber, the layer structure, the outer diameter, the inner diameter, and the wall thickness. The design is taken into account. For example, the following are considered when selecting the arrangement direction of reinforcing fibers.
- reinforcing fibers are arranged at an angle of ⁇ 45 ° with respect to the axial direction of the main body, mainly for torsional strength, but mainly for torsional buckling strength with respect to the axial direction. It is most effective to arrange at an angle of ⁇ 80 to 90 °.
- reinforcing fibers are arranged in the axial direction as much as possible to increase the bending elastic modulus in the axial direction so that a high bending resonance frequency can be obtained.
- the design philosophy of ensuring safety has been to make the body a crushable structure, absorb the impact energy (compression load) at the time of the collision by compressing and breaking the body, and thereby reduce the sudden acceleration applied to the occupant.
- the FRP body is designed under the concept of giving priority to the critical rotation speed described above, the strength of the body against the compressive load in the axial direction will inevitably increase, and the body will be destroyed in the event of a collision, and the destruction will occur successively.
- the propeller shaft advances and reaches the propeller shaft, the propeller shaft acts like a stubborn stick, and the effect of absorbing impact energy is impaired.
- Japanese Patent Application Laid-Open No. 3-37416 discloses that the joint moves axially at the joint surface with the main body due to the compressive load at the time of collision, and at the same time, the joint moves the entire main body to its end.
- the main body and the joint in order to secure the movement of the joint, the main body and the joint must be joined via a complicated tooth profile and a separating agent, which not only complicates the structure but also increases the manufacturing cost. The complexity is inevitable.
- the joint is to be press-fitted into a spout shaft with such a configuration
- the main body must be strong enough to withstand the force at the time of press-fitting. Push and make destruction difficult. In other words, it is difficult to simultaneously satisfy the basic requirements described above and the conflicting requirements of spreading and breaking.
- Japanese Patent Application Laid-Open No. Hei 4-33992 discloses that when a compressive load in the axial direction is applied, the joint moves on the joint surface with the main body toward the inside of the main body, and the movement resistance is caused by the movement resistance. It describes a propeller shaft that absorbs impact energy.
- the outer diameter of the joint must always be smaller than the inner diameter of the main body, which not only reduces the degree of freedom in design, but also limits the travel of the joint length. Therefore, the effect of absorbing impact energy is not so large.
- An object of the present invention is to solve the above-described problems of the conventional propeller shaft, satisfy the basic requirements such as torsional strength and dangerous rotation speed, and adjust the propeller shaft in accordance with the destruction of the body during a vehicle collision.
- An object of the present invention is to provide a propeller shaft that can surely progress the destruction of the fuel and can sufficiently exert the energy absorbing effect of the body.
- the present invention provides a cylindrical body made of FRP and a joint joined to an end of the body, and the main body extends over the entire length of the body. And a partial layer provided integrally with the main layer and at an inner side of the main layer at an end of the main body, wherein the joint applies a compressive load acting in an axial direction of the joint to the main layer.
- a propeller shaft having a compressive load transmitting portion for concentrating between a layer and the partial layer and separating the main layer and the partial layer between the layers.
- a main body extending over the whole length of the main body; and a main layer extending over the entire length of the main body; At one end of the joint includes a part layer provided integrally with the main layer and inside the main layer, and the joint provided at the one end has a compressive load acting in the axial direction of the joint.
- a propeller shaft including a compression load transmitting portion that concentrates between the main layer and the partial layer and separates the main layer and the partial layer between the layers. Furthermore, it has a cylindrical body made of FRP, and a joint provided by being joined to one end and the other end of the main body. The main body extends over the entire length of the main body and is wound by a helicopter.
- a propeller shaft having a compressive load transmitting portion for separating between layers.
- the main body has a cylindrical main body made of FRP, and a joint provided by joining to one end and the other end of the main body.
- the main body extends over the entire length of the main body.
- a propeller shaft including a compression load transmitting portion that concentrates between layers between a main layer and the partial layer and separates the main layer and the partial layer between the layers.
- the compressive load transmitting portion has a downward slope facing the joint surface with the main body of the joint, or has an outer diameter equal to or less than the outer diameter of the partial layer and an upright surface facing the outer end surface of the partial layer. It is preferable to have When configured as an elevation, the elevation may be continuous in the circumferential direction of the joint, or may be divided into a plurality. In the former case, it is also preferable that the outer end surface of the main body is partially shouldered.
- the present invention has an FRP cylindrical main body, and a metal joint provided at one end and the other end of the main body. a. a main layer provided over the entire length of the main body, the main layer including reinforcing fibers helically wound at an angle of ⁇ 5 to 30 ° with respect to the axial direction of the main body;
- a partial layer including a hoop-wound reinforcing fiber provided integrally with the main layer and inside the main layer. Part and the joint provided at the other end,
- a compressive load acting adjacent to the joint surface and acting in the axial direction of the joint is concentrated between the layers of the main layer and the partial layer, and the main layer and the partial layer are separated between the layers.
- a compression load transmitting unit having a downward slope toward the joining surface;
- a propeller shaft having:
- the body has a cylindrical body made of FRP, and a metal joint provided in contact with one end and the other end of the body.
- a main layer provided over the entire length of the main body and including a reinforcing fiber wound helically at an angle of ⁇ 5 to 30 ° with respect to the axial direction of the main body;
- a compressive load acting adjacent to the joint surface and acting in the axial direction of the joint is concentrated between the layers of the main layer and the partial layer, and the main layer and the partial layer are separated between the layers.
- a compressive load transmitting portion having an outer diameter equal to or less than the outer diameter of the partial layer, and having an upright surface facing an outer end surface of the partial layer;
- the upright surface may extend in a ring shape in the circumferential direction of the joint, and a plurality thereof may be arranged in the circumferential direction. In the former case, it is also preferable to partially drop the outer end surface of the main body.
- a cylindrical body made of FRP and a joint joined to an end of the body to achieve the above object.
- a main layer extending therefrom, and a partial layer provided at an end of the main body integrally with the main layer and inside the main layer, wherein the joint acts in an axial direction of the joint.
- a propeller shaft having wedge means for applying a compressive load between the main layer and the partial layer to separate the main layer and the partial layer between the layers.
- a main body extending over the whole length of the main body; and a main layer extending over the entire length of the main body; At one end of the joint includes a part layer provided integrally with the main layer and inside the main layer, and the joint provided at the one end has a compressive load acting in the axial direction of the joint.
- a propeller shaft having wedge means which acts between the main layer and the partial layer to peel off the main layer and the partial layer between the layers. Furthermore, it has a cylindrical body made of FRP, and a joint provided by being joined to one end and the other end of the main body. The main body extends over the entire length of the main body and is wound by a helicopter.
- the joints provided at the one end and the other end are made by applying a compressive load acting in the axial direction of the joint between the main layer and the partial layer.
- a propeller shaft having wedge means for separating a main layer and a partial layer between the layers.
- the joint provided at one end and the other end includes a partial layer including a hoop-wound reinforcing fiber provided on an inner side, and a compressive load acting in an axial direction of the joint is applied to the main layer and the above-mentioned main layer.
- a propeller shaft provided with wedge means which acts between layers of a partial layer to separate the main layer and the partial layer between the layers.
- the main body has a cylindrical body made of FRP, and a metal joint joined to one end and the other end of the main body.
- a main layer provided over the entire length of the main body and including a reinforcing fiber wound helically at an angle of ⁇ 5 to 30 ° with respect to the axial direction of the main body;
- a partial layer including a hoop-wound reinforcing fiber provided integrally with the main layer and inside the main layer. Part and the joint provided at the other end,
- a compressive load acting adjacent to the joint surface and acting in the axial direction of the joint is applied between the main layer and the partial layer to separate the main layer and the partial layer between the layers.
- a propeller shaft having:
- the wedge means has a ring-shaped wedge extending along the layer between the main layer and the partial layer, or has a plurality of wedges arranged along the layer.
- the joining of the joint to the main body is preferably performed by press fitting.
- the joint preferably has a selection extending in the axial direction of the joint on the joint surface with the main body. Further, it is preferable that the main body is provided with a vibration damper.
- FIG. 1 is a schematic partial longitudinal sectional front view showing a main part of a propeller shaft according to an embodiment of the present invention.
- FIG. 2 is a schematic partial longitudinal sectional front view showing a joint used in the propeller shaft shown in FIG.
- FIG. 3 is a schematic partial longitudinal sectional front view showing a main part of the propeller shaft, showing the progress of destruction of the propeller shaft shown in FIG.
- FIG. 4 is a schematic partial longitudinal sectional front view showing a main part of a propeller shaft according to another embodiment of the present invention.
- FIG. 5 is a schematic partial longitudinal sectional front view showing a main part of the propeller shaft, showing the progress of destruction of the propeller shaft shown in FIG.
- FIG. 6 is a schematic perspective view showing a main part of a propeller shaft having a joint different from that shown in FIG.
- FIG. 7 is a schematic perspective view showing a main part of a propeller shaft having a body shape different from that shown in FIG.
- FIG. 8 is a schematic partial longitudinal sectional front view showing a main part of a propeller shaft according to still another embodiment of the present invention.
- FIG. 9 is a schematic partial longitudinal sectional front view showing a joint used in the propeller shaft shown in FIG.
- FIG. 10 is a schematic partial longitudinal sectional front view showing the main part of the propeller shaft, showing the progress of the destruction of the propeller shaft shown in FIG.
- FIG. 11 is a schematic partial longitudinal sectional front view showing a main part of a propeller shaft, showing an embodiment of a joint used by being joined to a non-destructive side end of a propeller shaft of the present invention.
- FIG. 12 is a schematic partial longitudinal sectional front view showing a main part of a main body having differently shaped partial layers.
- FIG. 13 is a schematic cross-sectional view showing an essential part of an embodiment of the vibration damper used in the propeller shaft of the present invention.
- FIG. 14 is a schematic side view showing the overall shape of the vibration damping body shown in FIG.
- FIG. 15 is a schematic cross-sectional view showing a main part of a vibration damper different from that shown in FIG.
- the propeller shaft is made of carbon fiber, glass fiber, polyalamide fiber, etc.
- Elastic modulus reinforcing fiber such as epoxy resin, unsaturated polyester resin, phenolic resin, vinyl ester resin, polyimide resin, etc., or heat of polyamide resin, polycarbonate resin, polyetherimide resin etc.
- It has a cylindrical body 1 made of FRP reinforced with a plastic resin.
- a metal joint 2 is press-fitted to one end and the other end of the main body 1. This propeller shaft is symmetrical when viewed from the longitudinal center.
- the main body 1 has a uniform inner diameter and extends over the entire length thereof, and includes a main layer la including reinforcing fibers wound helically at an angle of ⁇ 5 to 30 ° with respect to the axial direction; At both ends, a partial layer including a hoop-wrapped reinforcing fiber provided integrally with the main layer la and inside the main layer la (the reinforcing fiber is ⁇ 80 to 90 ° in the axial direction) 1b).
- the main layer 1a mainly acts to improve the bending elastic modulus of the main body 1 in the axial direction to increase the bending resonance frequency of the propeller shaft, thereby increasing the critical rotation speed and improving the torsional strength. I do.
- the partial layer lb mainly gives each end of the main body 1 to which the joint is press-fitted and joined a strength capable of withstanding the force at the time of press-fitting without hindering the progress of fracture as described later, and Acts to transmit torque (torsion tonolek) to main unit 1.
- a main body 1 can be formed by, for example, a filament winding method.
- a resin-impregnated reinforcing fiber bundle is used, and the resin-impregnated reinforcing fiber bundle is hoop-wrapped at one end of a mandrel to a desired thickness and a desired length to form a partial layer.
- the reinforcing fiber bundle is run to the other end of the mandrel and a partial layer is similarly formed at the other end.
- the resin-impregnated fiber bundle is helically wound while being reciprocated between the other end and the one end, starting from the other end, thereby forming a main layer having a desired thickness.
- a resin-impregnated fiber bundle is placed on the main layer, for example, a one-layer hoop.
- each layer can be formed continuously without cutting the reinforcing fiber bundle halfway.
- the resin is hardened or solidified preferably while rotating, and the mandrel is pulled out to obtain the main body.
- the joint 2 has a joint surface 2a inscribed in the partial layer lb and slightly shorter than the partial layer lb.
- the outer diameter of the portion where the joint surface 2a is formed is slightly larger than the inner diameter of the main body 1 before press fitting. Therefore, when the joint 2 is press-fitted into the main body 1, a compressive stress acts on the joint surface 2a of the joint, and a tensile stress in the circumferential direction acts on the main body 1, respectively. 1 and joint 2 are firmly joined.
- the joining force varies depending on the area and surface condition of the joining surface 2a.
- the ratio of the press-fitting allowance to the inner diameter of the main body 1 is selected in the range of 0.001 to 0.02, and the length of the joint surface 2a in the axial direction of the main body 1 is equal to or more than 110 of the inner diameter of the main body.
- the above-mentioned joint 2 has a convex portion 2b having a ring recess whose outer diameter is slightly larger than the inner diameter of the main body 1 adjacent to the joint surface 2a, and a descending portion from the convex portion 2b toward the joint surface 2a. It has a slope 2c.
- the projection 2 b and the slope 2 e act in the axial direction of the joint 2.
- a compressive load is transmitted between the main layer la and the partial layer lb to separate the main layer 1a and the partial layer lb from each other.
- the angle formed by the slope 2c with respect to the axial direction of the main body 1 is preferably in the range of 15 to 45 °.
- the energy in the axial direction is absorbed by the destruction of the main layer 1a, but the initial destruction of the main body 1 is induced by the slope 2e of the joint 2, and the projection 2b is formed by the main layer 1a.
- the angle formed by the slope 2 e with respect to the axial direction of the main body 1 is preferably in the range of 15 to 45 ° as described above.
- FIG. 4 shows a propeller shaft according to another embodiment.
- the inclined surface 2c of the ring-shaped convex portion 2b shown in FIG. 1 is configured as an upright surface 2d facing the outer end surface of the partial layer lb.
- the outer diameter of the projection 2b is equal to that of the partial layer lb.
- the protruding portion 2b and the upright surface 2d constitute a compressive load transmitting portion.
- the compressive load applied in the axial direction causes the vertical load facing the partial layer lb. It is transmitted from face 2d to its sublayer lb and further to the main layer la.
- the main layer la also undergoes compressive deformation, the difference in Poisson's ratio between the main layer la and the partial layer lb is large, so that a shear stress acts between the two layers to break it, and this shear stress and compression
- the layers break under a two-dimensional stress state of the shear stress generated between the layers due to the load and the tensile stress generated by the press-fit of the joint 2, and the main layer la subsequently progresses as shown in Fig. 5.
- the partial layer 1 b moves while pushing and expanding the main layer la, and the convex portion 2 b does not participate in this push. The same effect can be obtained even if the outer diameter of the convex portion 2b is smaller than that of the partial layer lb.
- the elevation 2 d may or may not be in contact with the outer end face of the partial layer lb.
- the convex portion 2 b is ring-shaped as a whole as shown in FIG. 6, but a plurality of convex portions 2 b can be arranged in the circumferential direction of the joint 2. Further, as shown in FIG. 7, the convex portion 2b has a ring shape, but the outer end face of the main body 1 facing the convex portion 2b can be partially dropped.
- the main body 1 is configured exactly the same as that of the above-described embodiment, but the configuration of the compression load transmitting portion of the joint 2 is different.
- the joint 2 is provided with a ring-shaped convex portion 2b whose outer diameter is slightly larger than the inner diameter of the main body 1 adjacent to the joint surface 2a.
- the convex portion 2b is also formed with a ring-shaped wedge 2f, the leading end of which faces the interlayer between the main layer la and the partial layer lb.
- These convex portions 2 b and wedges 2 f cause a compressive load acting in the axial direction of the joint 2 to act between the main layer 1 a and the partial layer lb, thereby forming the main layer 1 a and the partial layer lb as described above. It constitutes wedge means for peeling between the layers.
- the wedges may not be ring-shaped, but may be a plurality of wedges arranged evenly along the layers.
- the wedge may be a single-edged or double-edged wedge, but is preferably a single-edged wedge having an outer surface as shown in FIGS.
- the angle formed by the blade surface with respect to the axial direction of the main body 1 is preferably in the range of 15 to 45 °.
- the destruction of the main layer la progresses at a stretch due to the action of the projection 2b, but the partial layer lb joined to the joint 2 is destroyed without destroying the main layer 1a together with the joint 2 Move in 1 along its axis.
- the energy in the axial direction is absorbed by the rupture of the main layer 1a, but the initial fracture of the main body 1 is induced by the wedge 2f of the joint 2, and the protrusion 2b is formed by the main layer la.
- the angle formed by the blade surface of the wedge 2 f with respect to the axial direction of the main body 1 is preferably in the range of 15 to 45 ° as described above.
- the joints having a selection at the joint are described.
- the joint with the main body becomes stronger, and it is convenient for transmitting torsional torque.
- the joints are preferably joined by press-fitting, but may be joined by an adhesive, or press-fitting and joining by an adhesive may be used in combination.
- the same joint was used for one end and the other end of the main body, that is, a propeller shaft that was symmetrical when viewed from the center in the length direction was described, there was an advantage that the number of types of parts was reduced.
- a joint having no compression load transmitting portion at the other end may be used.
- the joint at the other end has a shape as shown in FIG. 11 as a whole, as shown in FIG.
- the partial layer lb has a wedge-shaped vertical cross-section at the inner end face side corresponding to the outer end face, as shown in Fig. 1 etc. It is also preferable that the thickness is gradually reduced from the outer end face side to the inner end face side as shown in FIG.
- FIG. 13 shows an example of such a vibration damper.
- the vibration damper 3 is made of thick paper, a synthetic resin film, a synthetic fiber nonwoven fabric, or the like, and is arranged along the inner peripheral surface of the main body 1.
- a plurality of frictional engagement portions 3a, a cylindrical holding portion 31) placed at a position distant from the inner peripheral surface of the main body 1, and the frictional engagement portions 3a and the holding portions 3b are connected to each other.
- a corrugated elastic support portion 3c for elastically supporting the engagement portion 3a so as to press the engagement portion 3a against the inner peripheral surface of the main body 1; As a whole, as shown in FIG.
- FIG. 14 shows another vibration damper.
- the vibration damper 3 has the function of the frictional engagement portion 3a in the vibration damper shown in FIGS. 13 and 14 combined with the top of the corrugated elastic support portion 3e.
- the body was formed by the filament winding method. That is, six carbon fiber bundles (average single yarn diameter: 7 // m, single yarn number: 12,000, tensile strength: 36 Okgf / mm 2 , tensile elasticity: 23, 50 Okgf / mm 2 ) While impregnating a bisphenol A-type epoxy resin containing a curing agent and a curing accelerator, the mandrel with an outer diameter of 70M and a length of 1,300 was first placed in the axial direction at ⁇ 10 Omm at one end.
- the main body 1 as shown in Fig. 1 was obtained, having an outer diameter of 8 Omra, an outer diameter of the partial layer of 75, an inner diameter of 7 Omm, and a length of 1,20 Omra.
- the outer diameter of the joint surface 2a is 70.5 ram, and the joint surface 2a 4 Oram.
- the metal joint 2 with the outer diameter of the convex part 2 b of 80 ⁇ and the angle of the slope 2 e with respect to the axial direction of the main body 1 30 ° of 30 ° is press-fitted and joined as shown in Fig. 1.
- the force required for the injection was 7, 000 kgi.
- the torsional strength was 350 kgf ⁇ ⁇ .
- the critical rotation speed was 8,000 rpm, and both were sufficient as propeller shafts for automobiles.
- the torsional strength was 350 kgf ⁇ ⁇ .
- the critical rotation speed was 8,000 rpm, and both were sufficient as propeller shafts for automobiles.
- Each end of the main body 1 used in Example 1 has a serration on the joint surface as shown in FIG. 9, the outer diameter of the joint surface 2a is 70.5 mm, and the outer diameter of the joint surface 2a is The length is 4 Omm, the outer diameter of the projection 2 b is 80 ram, and the angle between the wedge 2 f and the axial direction of the body 1 is 30 °.
- the metal joint 2 was press-fitted and joined to obtain the propeller shaft of the present invention as shown in FIG.
- the force required for the press-fit was 7, OOO kgf.
- the torsional strength was 350 kgf ⁇ m.
- the critical rotation speed was 8,000 rpm, which was sufficient for propeller shafts for vehicles.
- the propeller shaft of the present invention includes a compressive load transmitting portion that concentrates a compressive load acting in the axial direction of the joint between the main layer and the partial layer and separates the main layer and the partial layer between the layers. Therefore, as shown in the embodiment, the propeller shaft is destroyed in accordance with the body rupture at the time of the collision while satisfying the basic requirements such as the torsional strength and the dangerous rotation speed required for the automobile. And the energy absorption effect of the body having the crushable structure can be sufficiently exhibited.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
- Excavating Of Shafts Or Tunnels (AREA)
Description
Claims
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| EP95901602A EP0683328B1 (en) | 1993-11-30 | 1994-11-29 | Propeller shaft |
| AU10771/95A AU1077195A (en) | 1993-11-30 | 1994-11-29 | Propeller shaft |
| KR1019950703142A KR100317474B1 (ko) | 1993-11-30 | 1994-11-29 | 프로펠러샤프트 |
| DE69429911T DE69429911T2 (de) | 1993-11-30 | 1994-11-29 | Antriebswelle |
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP5/300313 | 1993-11-30 | ||
| JP30031393 | 1993-11-30 | ||
| JP5/300312 | 1993-11-30 | ||
| JP30031293 | 1993-11-30 |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US96736897A Continuation | 1993-11-30 | 1997-11-07 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO1995015444A1 true WO1995015444A1 (en) | 1995-06-08 |
Family
ID=26562292
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/JP1994/001996 Ceased WO1995015444A1 (en) | 1993-11-30 | 1994-11-29 | Propeller shaft |
Country Status (8)
| Country | Link |
|---|---|
| US (1) | US20010001769A1 (ja) |
| EP (1) | EP0683328B1 (ja) |
| KR (1) | KR100317474B1 (ja) |
| AU (1) | AU1077195A (ja) |
| CA (1) | CA2155099A1 (ja) |
| DE (1) | DE69429911T2 (ja) |
| ES (1) | ES2173164T3 (ja) |
| WO (1) | WO1995015444A1 (ja) |
Families Citing this family (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| ES2129322B1 (es) * | 1996-04-18 | 2000-02-01 | Castellon Melchor Daumal | Perfeccionamientos en los arboles telescopicos. |
| KR100515800B1 (ko) * | 2002-10-23 | 2005-09-21 | 한국과학기술원 | 복합재료가 내면에 적층된 동력전달축 및 그 제조방법 |
| FR2846942A1 (fr) * | 2002-11-13 | 2004-05-14 | Soc D Const Aeronautique Auver | Arbre et procede de transmission pour helice d'avion deportee |
| DE112007001768B4 (de) * | 2006-08-28 | 2018-05-30 | Xperion Gmbh | Antriebswelle |
| DE102008025238A1 (de) * | 2007-06-21 | 2008-12-24 | Ifa-Technologies Gmbh | Längswelle |
| GB0722933D0 (en) | 2007-11-23 | 2008-01-02 | Dewhurst Mike | Mechanical connection between composite tubular structure and an end fitting of any engineering material |
| DE102009012479B4 (de) * | 2009-03-12 | 2012-05-03 | Sew-Eurodrive Gmbh & Co. Kg | Verbindung einer Welle mit einem Aufnahmeteil |
| DE102013103769B3 (de) * | 2013-04-15 | 2014-10-16 | Inometa Gmbh & Co. Kg | Vorrichtung für eine Antriebswelle eines Kraftfahrzeuges und Verfahren zum Herstellen |
| US9441374B2 (en) | 2014-04-08 | 2016-09-13 | Goodrich Corporation | Struts and methods utilizing a compression collar |
| EP3025846B1 (en) * | 2014-11-28 | 2019-11-13 | Crompton Technology Group Limited | Composite tension/compression strut |
| GB2538511B (en) * | 2015-05-18 | 2020-12-16 | Lentus Composites Ltd | Shaft arrangement |
| DE102016121660A1 (de) * | 2016-11-11 | 2018-05-17 | xperion components GmbH & Co. KG | Aufprallenergie absorbierende antriebswelle für ein motorfahrzeug |
| KR20180076574A (ko) * | 2016-12-28 | 2018-07-06 | 주식회사 신금하 | 프로펠러 필라멘트 와인딩 샤프트와 금속 플랜지 사이 연결 부위의 직물형 카본/에폭시 프리프레그 보강 적층 구조 및 방법 |
| US11649849B2 (en) | 2021-01-22 | 2023-05-16 | Hamilton Sundstrand Corporation | Buckling-resistant thin-wall drive shafts |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6041246B2 (ja) * | 1980-02-20 | 1985-09-14 | 東レ株式会社 | 繊維強化プラスチツク製プロペラシヤフト |
| JPH0191118U (ja) * | 1987-12-08 | 1989-06-15 | ||
| JPH0348023A (ja) * | 1989-06-24 | 1991-03-01 | Gkn Automot Ag | 接続機構 |
-
1994
- 1994-11-29 CA CA002155099A patent/CA2155099A1/en not_active Abandoned
- 1994-11-29 EP EP95901602A patent/EP0683328B1/en not_active Expired - Lifetime
- 1994-11-29 WO PCT/JP1994/001996 patent/WO1995015444A1/ja not_active Ceased
- 1994-11-29 KR KR1019950703142A patent/KR100317474B1/ko not_active Expired - Fee Related
- 1994-11-29 ES ES95901602T patent/ES2173164T3/es not_active Expired - Lifetime
- 1994-11-29 DE DE69429911T patent/DE69429911T2/de not_active Expired - Lifetime
- 1994-11-29 AU AU10771/95A patent/AU1077195A/en not_active Abandoned
-
2001
- 2001-01-19 US US09/764,319 patent/US20010001769A1/en not_active Abandoned
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS6041246B2 (ja) * | 1980-02-20 | 1985-09-14 | 東レ株式会社 | 繊維強化プラスチツク製プロペラシヤフト |
| JPH0191118U (ja) * | 1987-12-08 | 1989-06-15 | ||
| JPH0348023A (ja) * | 1989-06-24 | 1991-03-01 | Gkn Automot Ag | 接続機構 |
Non-Patent Citations (1)
| Title |
|---|
| See also references of EP0683328A4 * |
Also Published As
| Publication number | Publication date |
|---|---|
| ES2173164T3 (es) | 2002-10-16 |
| EP0683328B1 (en) | 2002-02-20 |
| CA2155099A1 (en) | 1995-06-08 |
| EP0683328A1 (en) | 1995-11-22 |
| US20010001769A1 (en) | 2001-05-24 |
| DE69429911T2 (de) | 2002-09-05 |
| KR100317474B1 (ko) | 2002-07-02 |
| DE69429911D1 (de) | 2002-03-28 |
| AU1077195A (en) | 1995-06-19 |
| EP0683328A4 (en) | 1997-08-20 |
| KR960700417A (ko) | 1996-01-20 |
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