CN203477006U - Bolt shaft with split pins installed in two directions - Google Patents

Bolt shaft with split pins installed in two directions Download PDF

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Publication number
CN203477006U
CN203477006U CN201320475001.2U CN201320475001U CN203477006U CN 203477006 U CN203477006 U CN 203477006U CN 201320475001 U CN201320475001 U CN 201320475001U CN 203477006 U CN203477006 U CN 203477006U
Authority
CN
China
Prior art keywords
cotter
bolt shaft
pin
split
directions
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.)
Expired - Fee Related
Application number
CN201320475001.2U
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Chinese (zh)
Inventor
马小伟
王征
王君
李文龙
李波
朱恒阳
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.)
Harbin Aircraft Industry Group Co Ltd
Original Assignee
Harbin Aircraft Industry Group Co Ltd
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
Application filed by Harbin Aircraft Industry Group Co Ltd filed Critical Harbin Aircraft Industry Group Co Ltd
Priority to CN201320475001.2U priority Critical patent/CN203477006U/en
Application granted granted Critical
Publication of CN203477006U publication Critical patent/CN203477006U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model belongs to the technical field of airplane connecting piece design and particularly relates to a bolt shaft with split pins installed in two directions. The bolt shaft with the split pins installed in the two directions is characterized in that threads are arranged on the end portion of the bolt shaft, two split pin holes which are matched with notches of hexagon slotted nuts are formed in the end portion of the bolt shaft, and hole axes of the two split pin holes are located on the same plane and cross with each other. The bolt shaft with the split pins installed in the two directions is widely applicable to the installation of split pins of helicopters and fixed-wing planes, the structure and installation are simple, maintenance is convenient, and the bolt shaft is easy to obtain. According to the bolt shaft with the split pins installed in the two directions, due to the fact that the split pin holes cross with each other, when the split pin hole in the vertical direction is blocked, it still can be guaranteed that the split pin hole in the horizontal direction is exposed, and then the corresponding split pin can be inserted into the split pin hole in the horizontal direction.

Description

A kind of two bolt axis to construction opening pin
Technical field
Aircraft stud connector design technical field of the present invention, particularly designs a kind of two bolt axis to construction opening pin.
Background technique
In aircraft flight control system, the locking of bolt conventionally adopts and play cotter pin in the cotter-pin hold of bolt head, and the hexagon slotted nut rotation that utilizes cotter pin to stop to coordinate with bolt, to play the effect of screw retention.Hexagon slotted nut is standard piece, on its six outer side surfaces, all respectively has a groove, and the groove on two relative faces is coaxial, and the angle between adjacent fluted shaft is 60 degree.
Bolt for construction opening pin on existing domestic helicopter and fixed wing machine has a cotter-pin hold, if it is inaccurate that in installation process, hexagon slotted nut screw-down torque is determined power, in six grooves of hexagon slotted nut, the cotter-pin hold of neither one and bolt connects, cotter-pin hold has just been blocked by hexagon slotted nut, cannot insert, cause cotter pin to install, bolt cannot lock.Now, can only cotter pin be inserted in cotter-pin hold by readjusting the relative position of bolt axis and hexagonal self-locking nut, readjust and can cause the position of hexagonal self-locking nut can not meet installation requirement.
Summary of the invention
The technical problem to be solved in the present invention:
The utility model is in bolt axis, to add a cotter-pin hold, forms the cotter-pin hold of criss-crossing, when a direction cannot construction opening pin, can install from another one hole, has both reduced structure weight, maintains easily again.The utility model is just for above-mentioned deficiency of the prior art, and the mounting type of a kind of cotter pin of proposition, when construction opening pin, is selectively used cotter-pin hold to carry out the fastening of screw bolt and nut.Its objective is and be convenient to construction opening pin in producing and using.
Technological scheme of the present invention:
The technical solution of the utility model is: for the bolt axis that hexagon slotted nut and cotter pin are installed, form due to hexagon slotted nut groove, in former cotter-pin hold position, 90-degree rotation increases by a cotter-pin hold, make when hexagon slotted nut rotates in bolt axis, can can expose cotter-pin hold all the time, and then construction opening pin easily.
Two bolt axis to construction opening pin, there is screw thread bolt axis 1 end, and is provided with two cotter-pin holds that coordinate with the fluting of hexagon slotted nut 4, and two cotter-pin hold hole axles are in a plane, and criss-crossing.
Beneficial effect of the present invention:
The utility model is widely used in the cotter pin of helicopter and fixed wing machine and installs, and structure and installation are simple, easy to maintenance, is easy to realize.This bolt axis 1, because cotter-pin hold becomes criss-crossing, the cotter-pin hold of Vertical direction is blocked while making in as Fig. 1, still can guarantee that the cotter-pin hold of substantially horizontal exposes, and cotter pin 3 can be inserted.
Accompanying drawing explanation
Fig. 1 is bolt axis construction opening pin schematic diagram; 1 is bolt axis, and 2 is cotter pin, and 3 is cotter pin, and 4 is hexagon slotted nut,
Fig. 2 is conventional hexagon slotted nut;
Fig. 3 bolt axis schematic diagram, 5 is cotter-pin hold.
Embodiment
Below in conjunction with drawings and Examples, the present invention is explained as follows:
At Fig. 3, can see, there is screw thread bolt axis 1 end, and is provided with two cotter-pin holds that coordinate with hexagon slotted nut 4 flutings, and two cotter-pin hold hole axles are in a plane, and criss-crossing.There is screw thread bolt axis 1 end, and is provided with 5, two cotter-pin hold hole axles of two cotter-pin holds in a plane, and criss-crossing.Its relative position is in a plane, and criss-crossing.Normally used bolt axis only has a cotter-pin hold, if after the first-class screw-down torque of hexagon slotted nut 4 just when position shown in Fig. 1, just the corresponding cotter-pin hold of cotter pin 2 has been blocked by hexagon slotted nut 4, cannot insert.Can only with the relative position of hexagon slotted nut 4, cotter pin 2 can be inserted in cotter-pin hold by readjusting bolt axis 1.And for the design's bolt axis 1, due to 5 one-tenth criss-crossings of cotter-pin hold, the cotter-pin hold of Vertical direction is blocked while making in as Fig. 1, still can guarantee that the cotter-pin hold of substantially horizontal exposes, and cotter pin 3 can be inserted.

Claims (1)

1. two bolt axis to construction opening pin, is characterized in that, there is screw thread bolt axis end, and are provided with two cotter-pin holds that coordinate with the fluting of hexagon slotted nut, and two cotter-pin hold hole axles are in a plane, and criss-crossing.
CN201320475001.2U 2013-08-05 2013-08-05 Bolt shaft with split pins installed in two directions Expired - Fee Related CN203477006U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201320475001.2U CN203477006U (en) 2013-08-05 2013-08-05 Bolt shaft with split pins installed in two directions

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201320475001.2U CN203477006U (en) 2013-08-05 2013-08-05 Bolt shaft with split pins installed in two directions

Publications (1)

Publication Number Publication Date
CN203477006U true CN203477006U (en) 2014-03-12

Family

ID=50225342

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201320475001.2U Expired - Fee Related CN203477006U (en) 2013-08-05 2013-08-05 Bolt shaft with split pins installed in two directions

Country Status (1)

Country Link
CN (1) CN203477006U (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107255113A (en) * 2017-08-04 2017-10-17 海盐联众紧固件有限公司 A kind of automobile modified form stop nut
CN107269660A (en) * 2017-08-04 2017-10-20 海盐联众紧固件有限公司 A kind of vapour nut for automobile
CN107299932A (en) * 2017-08-04 2017-10-27 海盐联众紧固件有限公司 A kind of automobile Combined locknut
CN107327462A (en) * 2017-08-04 2017-11-07 海盐联众紧固件有限公司 A kind of automobile modular nut
CN108561398A (en) * 2018-07-24 2018-09-21 江苏双汇电力发展股份有限公司 A kind of bolt fastener and apply its electric armour clamp
CN111677743A (en) * 2020-06-19 2020-09-18 嘉兴同辉汽配有限公司 Anti-loosening connecting piece for automobile lamp
CN112013005A (en) * 2020-08-12 2020-12-01 苏州剑派实业有限公司 Hexagonal head slotted nut with self-locking function

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107255113A (en) * 2017-08-04 2017-10-17 海盐联众紧固件有限公司 A kind of automobile modified form stop nut
CN107269660A (en) * 2017-08-04 2017-10-20 海盐联众紧固件有限公司 A kind of vapour nut for automobile
CN107299932A (en) * 2017-08-04 2017-10-27 海盐联众紧固件有限公司 A kind of automobile Combined locknut
CN107327462A (en) * 2017-08-04 2017-11-07 海盐联众紧固件有限公司 A kind of automobile modular nut
CN108561398A (en) * 2018-07-24 2018-09-21 江苏双汇电力发展股份有限公司 A kind of bolt fastener and apply its electric armour clamp
CN111677743A (en) * 2020-06-19 2020-09-18 嘉兴同辉汽配有限公司 Anti-loosening connecting piece for automobile lamp
CN112013005A (en) * 2020-08-12 2020-12-01 苏州剑派实业有限公司 Hexagonal head slotted nut with self-locking function
CN112013005B (en) * 2020-08-12 2022-03-25 苏州剑派实业有限公司 Hexagonal head slotted nut with self-locking function

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20140312

Termination date: 20160805