WO2017187746A1 - Hélice de navire - Google Patents

Hélice de navire Download PDF

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Publication number
WO2017187746A1
WO2017187746A1 PCT/JP2017/006812 JP2017006812W WO2017187746A1 WO 2017187746 A1 WO2017187746 A1 WO 2017187746A1 JP 2017006812 W JP2017006812 W JP 2017006812W WO 2017187746 A1 WO2017187746 A1 WO 2017187746A1
Authority
WO
WIPO (PCT)
Prior art keywords
propeller
blade
hole
pin
disk
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
Application number
PCT/JP2017/006812
Other languages
English (en)
Japanese (ja)
Inventor
和秀 鹿養
晃広 東
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Kawasaki Heavy Industries Ltd
Kawasaki Motors Ltd
Original Assignee
Kawasaki Heavy Industries Ltd
Kawasaki Jukogyo KK
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from JP2016089279A external-priority patent/JP5997408B1/ja
Priority claimed from JP2016163249A external-priority patent/JP6706560B2/ja
Application filed by Kawasaki Heavy Industries Ltd, Kawasaki Jukogyo KK filed Critical Kawasaki Heavy Industries Ltd
Priority to CN201780023057.5A priority Critical patent/CN109070980B/zh
Priority to KR1020187032711A priority patent/KR102043351B1/ko
Publication of WO2017187746A1 publication Critical patent/WO2017187746A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H1/00—Propulsive elements directly acting on water
    • B63H1/02—Propulsive elements directly acting on water of rotary type
    • B63H1/12—Propulsive elements directly acting on water of rotary type with rotation axis substantially in propulsive direction
    • B63H1/14—Propellers
    • B63H1/20—Hubs; Blade connections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H3/00—Propeller-blade pitch changing
    • B63H3/12—Propeller-blade pitch changing the pitch being adjustable only when propeller is stationary

Definitions

  • the present invention relates to an assembly-type marine propeller.
  • One of the marine propellers is a fixed pitch propeller in which a plurality of propeller blades and a propeller boss are integrated. In such a fixed pitch propeller, the pitch (angle) of the propeller blades cannot be adjusted.
  • an assembly-type marine propeller in which a plurality of propeller blades and propeller labs are separated may be used.
  • Patent Document 1 discloses an assembly-type marine propeller 100 as shown in FIGS. 13A and 13B.
  • the blade flange 121 of the propeller blade 120 is fastened to the hollow propeller boss 110 by the stud bolt 130 and the tension nut 140.
  • the propeller boss 110 is provided with a plurality of openings 111 through which the studs 130 are inserted.
  • Each opening 111 extends in the circumferential direction around the center of the blade flange 121, and the pitch of the propeller blade 120 can be adjusted by the length of the opening 111.
  • a washer 150 is interposed between the tension nut 140 and the propeller boss 110 that are screwed into the stud bolt 130. Further, the tension nut 140 is pulled in a direction away from the washer 150 by a plurality of tension screws 160, whereby the stud bolt 130 is tensioned.
  • a plurality of (for example, 16) studs 130 are required for one propeller blade, and a plurality (for example, for example) each stud 130 is provided. 16) tension screws 160 are required. Therefore, the work of attaching the propeller blades to the propeller boss is complicated.
  • a disk is disposed in the propeller boss.
  • the disc contacts the blade flange through a blade fixing hole provided in the propeller boss, and is fastened to the blade flange by a bolt to sandwich the propeller boss together with the blade flange.
  • the blade flange and the propeller boss are connected by at least one pin.
  • the blade flange is provided with a positioning hole into which the pin is fitted.
  • an adjustment hole is provided in the propeller boss, and a bush having a fitting hole for fitting with the pin is inserted into the adjustment hole.
  • an object of the present invention is to provide an assembly-type marine propeller capable of easily changing the pitch of propeller blades.
  • a marine propeller according to the present invention is a fastening member that abuts against a propeller blade including a blade flange, a hollow propeller boss provided with a blade fixing hole, and the blade flange through the blade fixing hole.
  • the disc is fastened to the vane flange and sandwiches the propeller boss with the vane flange, at least one pin held on one of the propeller boss and the disc, and provided on the other of the propeller boss and the disc.
  • the bush when the pitch of the propeller blades is changed, the bush can be replaced by removing the fastening member for fastening the disc to the blade flange and removing the disc from the propeller boss. That is, it is not necessary to remove the propeller blade from the propeller boss. For this reason, the pitch of the propeller blades can be easily changed.
  • the adjustment hole may be a long hole extending in the circumferential direction around the center of the blade flange. According to this configuration, a large adjustment range of the pitch of the propeller blades can be ensured.
  • the pin may be held on the propeller boss or the disc by fitting with a positioning hole provided on the propeller boss or the disc.
  • the disk may have an elliptical shape that is long in the axial direction of the propeller shaft, and the pin may be disposed at a position that is separated from the blade fixing hole in the axial direction of the propeller shaft. According to this configuration, even when the number of propeller blades is large, the propeller boss can be downsized.
  • the disk may have a through hole inserted through the fastening member, and the through hole may be a long hole extending in the circumferential direction around the center of the blade flange. According to this configuration, a large adjustment range of the pitch of the propeller blades can be ensured.
  • the pitch of the propeller blades can be easily changed.
  • FIG. 1 is a perspective view showing a marine propeller according to a first embodiment of the present invention. It is sectional drawing of the marine propeller shown in FIG. FIG. 3 is a sectional view taken along line III-III in FIG. 2.
  • 4A is an enlarged view of a main part of FIG. 2
  • FIG. 4B is a sectional view taken along line IV-IV of FIG. 4A
  • FIG. 4C is a bottom view corresponding to FIG. 4B. It is a bottom view which shows the other shape of an adjustment hole and a bush.
  • 6A and 6B are partial cross-sectional views of a modified marine propeller.
  • 7A and 7B are partial cross-sectional views of a modified marine propeller.
  • FIG. 8A is a partial cross-sectional view of a marine propeller according to a second embodiment of the present invention
  • FIG. 8B is a cross-sectional view taken along line VIIIB-VIIIB in FIG. 8A
  • FIG. 8C is taken along line VIIIC-VIIIC in FIG.
  • 9A and 9B are partial cross-sectional views of a modified marine propeller.
  • 10A and 10B are partial cross-sectional views of a modified marine propeller. It is a fragmentary sectional view of the marine propeller of a modification. It is a bottom view which shows the other shape of the through-hole of a disk.
  • 13A is a partial cross-sectional view of a conventional marine propeller
  • FIG. 13B is a cross-sectional view taken along line XIII-XIII in FIG. 13A.
  • (First embodiment) 1 to 3 show a marine propeller 1 according to a first embodiment of the present invention.
  • This marine propeller 1 is an assembly type in which a plurality of propeller blades 3 and a propeller boss 2 are separated.
  • the number of propeller blades 3 is 4, but the number of propeller blades 3 may be 3 or less, or 5 or more.
  • Propellerabos 2 is hollow.
  • the propeller boss 2 has a cylindrical shape extending in the axial direction of the propeller shaft 11.
  • One end of the propeller boss 2 is fixed to a flange 12 provided at the tip of the propeller shaft 11 by a plurality of bolts 13.
  • a cover 14 is fixed to the other end of the propeller boss 2 by a plurality of bolts (not shown). The cover 14 closes the internal space of the propeller boss 2 from the side opposite to the propeller shaft 11.
  • the propeller boss 2 is provided with a plurality of blade fixing holes 21 penetrating the propeller boss 2 in the radial direction.
  • the outer portion (portion close to the outer peripheral surface of the propeller boss 2) of each blade fixing hole 21 has a large diameter
  • the inner portion (portion close to the inner peripheral surface of the propeller boss 2) has a small diameter.
  • an annular protrusion that protrudes inward in the radial direction of the blade fixing hole 21 is formed in an inner portion of each blade fixing hole 21.
  • Each propeller blade 3 includes a blade flange 31 for connection with the propeller boss 2.
  • the blade flange 31 has a stepped shape that matches the shape of the blade fixing hole 21, and the entire blade flange 31 is inserted into the blade fixing hole 21. That is, the front surface of the blade flange 31 (the surface located on the radially outer side of the propeller boss 2) constitutes a wall surface continuous with the outer peripheral surface of the propeller boss 2.
  • a plurality of (eight in the illustrated example) screw holes 32 are formed on the back side surface of the blade flange 31 (the surface located on the radially inner side of the propeller boss 2) to be screwed with bolts 41 described later.
  • the screw holes 32 are arranged at equiangular intervals around the center of the blade flange 31, but the intervals between the screw holes 32 may not be equiangular.
  • each disk 4 is larger than the inner opening of the blade fixing hole 21 and is in contact with the blade flange 31 through the blade fixing hole 21.
  • each disk 4 has an elliptical shape that is long in the axial direction of the propeller shaft 11.
  • the shape of each disk 4 may be circular.
  • Each disk 4 is fastened to the blade flange 31 by a plurality of bolts 41 (corresponding to the fastening member of the present invention) extending in the axial direction of the blade fixing hole 21.
  • the bolt 41 penetrates the disk 4 from the inside of the propeller boss 2 and is screwed into the screw hole 32. That is, the disk 4 has a through hole 42 inserted through the bolt 41.
  • the through hole 42 is circular.
  • the disc 4 clamps the propeller boss 2 (more precisely, the annular protrusion formed in the inner portion of the blade fixing hole 21 described above) together with the blade flange 31 by fastening the blade 41 to the blade flange 31.
  • each pin 6 has a cylindrical shape whose axial length is longer than the diameter.
  • the length of each pin 6 may be shorter than the diameter.
  • each pin 6 may be, for example, a rectangular parallelepiped that is long in the axial direction of the blade fixing hole 21 or in a direction orthogonal thereto.
  • the two pins 6 are arranged at positions spaced apart from the blade fixing hole 21 in one axial direction of the propeller shaft 11, and the remaining two pins 6 are arranged in the axial direction of the propeller shaft 11 from the blade fixing hole 21. It is arranged at a position away from the other. In other words, each pin 6 is located in a region overlapping with the blade fixing hole 21 when viewed from the axial direction of the propeller shaft 11.
  • each pin 6 is held by the propeller boss 2.
  • the propeller boss 2 is provided with a bottomed positioning hole 5, and the pin 6 is held in the propeller boss 2 by fitting into the positioning hole 5.
  • the pin 6 is fixed to the propeller boss 2 by a bolt 91 that passes through the center of the pin 6.
  • the disk 4 is provided with a circular adjustment hole 7 penetrating the disk 4 at a position corresponding to the positioning hole 5, and a bush 8 is inserted into the adjustment hole 7.
  • the bush 8 has a fitting hole 8a into which the pin 6 is fitted.
  • the bush 8 has a length equal to the thickness of the disk 4 and defines the fitting hole 8a, and the opposite end from the end of the tubular portion 81 opposite to the propeller boss 2 A pair of flange portions 82 are provided.
  • the flange portion 82 is fixed to the disk 4 with a bolt 92.
  • the bushes 8 can be replaced by removing the bolts 41 and removing the disk 4 from the propeller labs 2. That is, it is not necessary to remove the propeller blade 3 from the propeller boss 2. For this reason, the pitch of the propeller blades 3 can be easily changed.
  • the disk 4 has an elliptical shape, and the pins 6 are disposed on both sides of the blade fixing hole 21 in the axial direction of the propeller shaft 11, so even if the number of propeller blades 3 is large, the propeller The boss 2 can be reduced in size.
  • the blade flange 31 has a stepped shape, but has a stepped shape so that the disk 4 is partially inserted into the blade fixing hole 21, and the blade flange 31 is flat. May be.
  • the blade fixing hole 21 does not have an annular protrusion, and the blade flange 31 may not be inserted into the blade fixing hole 21.
  • This modification can also be applied to a second embodiment described later.
  • the disk 4 does not necessarily need to directly contact the blade flange 31, and may contact the blade flange 31 indirectly through another member inserted into the blade fixing hole 21. This modification is also applicable to the second embodiment described later.
  • the adjustment hole 7 into which the bush 8 is inserted is circular.
  • the adjustment hole 7 may be a long hole extending in the circumferential direction around the center of the blade flange 31. According to this configuration, a large adjustment range of the pitch of the propeller blades 3 can be ensured. This modification can also be applied to a second embodiment described later.
  • the fixing method of the pin 6 and the bush 8 can be changed as appropriate.
  • the length of the cylindrical portion 81 of the bush 8 may be increased, and the flange portion 82 may be positioned outside the adjustment hole 7.
  • a blocking portion 83 may be provided at the end of the cylindrical portion 81 opposite to the propeller boss 2, and the pin 6 may be supported by the blocking portion 83.
  • the positioning hole 5 provided in the propeller boss 2 is a screw hole, and a screw thread that engages with the screw hole may be formed on the pin 6.
  • the flange portion 82 of the bush 8 may be provided at the end portion of the cylindrical portion 81 on the propeller boss 2 side.
  • the adjustment hole 7 may be a bottomed hole, and the pin 6 may be supported by the bottom of the adjustment hole 7.
  • the pin 6 when the adjustment hole 7 passes through the disk 4, the pin 6 may be supported by the closing portion 83 provided at the end of the cylindrical portion 81 opposite to the propeller boss 2. Good.
  • (Second Embodiment) 8A to 8C show a part of a marine propeller according to a second embodiment of the present invention.
  • the overall configuration of the marine propeller of this embodiment is the same as that of the first embodiment shown in FIGS.
  • the same components as those in the first embodiment are denoted by the same reference numerals, and a duplicate description is omitted.
  • each pin 6 is held on the disk 4.
  • the disk 4 is provided with a positioning hole 5 penetrating the disk 4, and the pin 6 is held in the disk 4 by fitting into the positioning hole 5.
  • the pin 6 is fixed to the propeller boss 2 by a bolt 93 that is screwed into a screw hole provided on the side surface of the disk 4.
  • a shaft portion may be provided at the tip of the bolt 93, and the shaft portion may penetrate the pin 6.
  • the propeller boss 2 is provided with a bottomed circular adjustment hole 7 at a position corresponding to the positioning hole 5, and a bush 8 is inserted into the adjustment hole 7.
  • the bush 8 has a fitting hole 8a into which the pin 6 is fitted.
  • the bush 8 spreads in the opposite direction from the cylindrical portion 81 that defines the fitting hole 8a having the same length as the depth of the adjustment hole 7 and the end of the cylindrical portion 81 on the disk 4 side.
  • a pair of flange portions 82 are provided.
  • the flange portion 82 is fixed to the propeller boss 2 with a bolt 92.
  • the fixing method of the pin 6 and the bush 8 can be changed as appropriate.
  • the length of the pin 6 may be increased and the pin 6 may be supported by a support plate 94 fixed to the inner surface of the disk 4 by a bolt 95.
  • the length of the pin 6 is further increased, and a groove is formed in the peripheral surface of the pin 6, and the key plate fixed to the inner surface of the disk 4 by a bolt 97 in the groove. 96 may engage.
  • the positioning hole 5 may be a bottomed hole, and the pin 6 may be supported by the bottom of the positioning hole 5.
  • a blocking portion 84 may be provided at the end of the cylindrical portion 81 opposite to the disk 4.
  • the positioning hole 5 provided in the disk 4 may be a screw hole, and a screw thread that engages with the screw hole may be formed on the pin 6.
  • the pin 6 may be held on the disk 4 by being formed integrally with the disk 4.
  • the pin 6 is held by the propeller boss 2 as in the first embodiment, if the pin 6 is formed integrally with the propeller boss 2, the manufacturing cost of the propeller boss 2 is increased.
  • the disk 4 is formed in a plate shape, so that the disk 4 on which the pins 6 are integrally formed can be manufactured at low cost.
  • the through hole 42 of the disk 4 inserted through the bolt 41 may be a long hole extending in the circumferential direction around the center of the blade flange 31. According to this configuration, a large adjustment range of the pitch of the propeller blades 3 can be ensured.
  • the adjustment hole 7 is also a long hole, but the adjustment hole 7 may be circular.
  • the screw hole 32 to be screwed with the bolt 41 may be provided in the disk 4 instead of the blade flange 31, and the bolt 41 may be screwed into the screw hole 32 through the blade flange 31 from the outside of the propeller boss 2. .
  • the fastening member of the present invention is not necessarily a bolt, and may be a pin whose diameter can be changed by hydraulic pressure, for example.
  • the number of pins 6 that connect the propeller boss 2 and the disk 4 is not necessarily plural, and may be one.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

L'invention concerne une hélice de navire comprenant les éléments suivants : une pale d'hélice comprenant une collerette de pale ; un bossage d'hélice creux pourvu d'un trou de fixation de pale ; un disque qui vient en butée contre la collerette de pale à travers le trou de fixation de pale, qui est fixé à la collerette de pale par un élément de fixation, et qui, conjointement avec la collerette de pale, prend en sandwich le bossage d'hélice ; au moins une broche maintenue dans l'un ou l'autre élément parmi le bossage d'hélice et le disque ; et une chemise qui est insérée dans un trou d'ajustement ménagé dans l'autre élément parmi le bossage d'hélice et le disque, la chemise ayant un trou de mise en prise qui est en prise avec la broche.
PCT/JP2017/006812 2016-04-27 2017-02-23 Hélice de navire Ceased WO2017187746A1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
CN201780023057.5A CN109070980B (zh) 2016-04-27 2017-02-23 船用螺旋桨
KR1020187032711A KR102043351B1 (ko) 2016-04-27 2017-02-23 선박용 프로펠러

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
JP2016089279A JP5997408B1 (ja) 2016-04-27 2016-04-27 舶用プロペラ
JP2016-089279 2016-04-27
JP2016-163249 2016-08-24
JP2016163249A JP6706560B2 (ja) 2016-08-24 2016-08-24 舶用プロペラ

Publications (1)

Publication Number Publication Date
WO2017187746A1 true WO2017187746A1 (fr) 2017-11-02

Family

ID=60160249

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/JP2017/006812 Ceased WO2017187746A1 (fr) 2016-04-27 2017-02-23 Hélice de navire

Country Status (3)

Country Link
KR (1) KR102043351B1 (fr)
CN (1) CN109070980B (fr)
WO (1) WO2017187746A1 (fr)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3594099A (en) * 1968-04-29 1971-07-20 Glacier Metal Co Ltd Pitch adjustment in screw-bladed devices, such as propellers
JPS62143599U (fr) * 1986-03-05 1987-09-10
JPS6410496U (fr) * 1987-07-09 1989-01-19
JP2002544063A (ja) * 1999-05-19 2002-12-24 ロールス・ロイス・アクチボラゲット 脱着可能な羽根を備えた船用プロペラ

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FI890014A7 (fi) * 1988-03-02 1989-09-03 Neptun Schiffswerft Veb Reglerpropeller.
US7357686B2 (en) * 2005-06-22 2008-04-15 Huei-Jeng Lin Boat propeller with adjustable blades for adjusting the pitch thereof
CN101602397A (zh) * 2009-07-17 2009-12-16 南京高精船用设备有限公司 新型船舶用推进器桨毂
CN202449194U (zh) * 2011-12-29 2012-09-26 江苏华阳重工股份有限公司 有定位机构的可调距螺旋桨
CN103612735B (zh) * 2013-11-01 2017-01-11 武汉船用机械有限责任公司 一种可调螺距螺旋桨装置
GB2526302B (en) * 2014-05-20 2019-07-03 Teignbridge Propellers International Ltd Propeller with detachable blades

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3594099A (en) * 1968-04-29 1971-07-20 Glacier Metal Co Ltd Pitch adjustment in screw-bladed devices, such as propellers
JPS62143599U (fr) * 1986-03-05 1987-09-10
JPS6410496U (fr) * 1987-07-09 1989-01-19
JP2002544063A (ja) * 1999-05-19 2002-12-24 ロールス・ロイス・アクチボラゲット 脱着可能な羽根を備えた船用プロペラ

Also Published As

Publication number Publication date
KR102043351B1 (ko) 2019-11-12
CN109070980A (zh) 2018-12-21
CN109070980B (zh) 2020-07-28
KR20190015223A (ko) 2019-02-13

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