CN205271852U - Engine nut mounting tool - Google Patents

Engine nut mounting tool Download PDF

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Publication number
CN205271852U
CN205271852U CN201520947790.4U CN201520947790U CN205271852U CN 205271852 U CN205271852 U CN 205271852U CN 201520947790 U CN201520947790 U CN 201520947790U CN 205271852 U CN205271852 U CN 205271852U
Authority
CN
China
Prior art keywords
pole
steel pipe
pin
nut
branch
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.)
Active
Application number
CN201520947790.4U
Other languages
Chinese (zh)
Inventor
李赞
孙玉林
宋慧军
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.)
AECC Shenyang Liming Aero Engine Co Ltd
Original Assignee
Shenyang Liming Aero Engine 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 Shenyang Liming Aero Engine Group Co Ltd filed Critical Shenyang Liming Aero Engine Group Co Ltd
Priority to CN201520947790.4U priority Critical patent/CN205271852U/en
Application granted granted Critical
Publication of CN205271852U publication Critical patent/CN205271852U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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  • Details Of Spanners, Wrenches, And Screw Drivers And Accessories (AREA)

Abstract

The utility model discloses an engine nut mounting tool, include: support, wrench end, pin I, torsional spring, cable subassembly, the support includes the steel pipe and locates the branch I and branch II at steel pipe both ends, pin I and torsion spring connect are passed through with the wrench end to branch II, be equipped with the torque wrench mounting hole on the branch I, be equipped with on the wrench end with the nut mounting hole of torque wrench mounting hole on same water flat line, cable subassembly one end is fixed on the wrench end, and the other end is located on the steel pipe and is stretched out to I one side of branch. The utility model discloses an installation of nut can be realized to folding of wrench end in narrow and small space. Convenient operation uses safe and reliable.

Description

A kind of engine nut setting tool
Technical field
The utility model relates to the fan rotor such as aircraft engine, civil aircraft assembling field, a kind of engine nut setting tool of special offer.
Background technology
When the fan rotor such as aircraft engine, civil aircraft assembles, by the restriction of spare part size so that assembling narrow space, spanner not easily launches, assembling difficulty.
Practical novel content
The purpose of this utility model is to provide a kind of engine nut setting tool, it is possible to launch in cylinder axle inside, it is achieved in the installation of narrow and small space inner nut.
The technical solution of the utility model is: a kind of engine nut setting tool, comprising: support 1, spanner head 2, pin I 3, torsion spring 4, traction cable 6; Described support 1 comprises steel pipe 1a and is located at pole I 1b and pole II 1c at steel pipe 1a two ends, described pole II 1c is connected by pin I 3 and torsion spring 4 with spanner head 2, described pole I 1b is provided with torque wrench open holes 1d, described spanner head 2 is provided with and torque wrench open holes 1d nut open holes 2a in the same horizontal line, described traction cable 6 one end is fixed on spanner head 2, and the other end is located on steel pipe 1a and is extend out to pole I 1b side.
Preferably, described pole I 1b and pole II 1c is provided with steel pipe 1a coupling end and is connected hanger, and the connection hanger of described pole I 1b and pole II 1c is located in steel pipe 1a by pin II 5 to connect and is welded into one-piece construction.
The utility model has following useful effect:
The utility model folding by spanner head, it is possible to realize the installation of nut in small space. Easy to operate, it may also be useful to safe and reliable.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the schematic diagram that the utility model spanner head folds;
In figure: 1, support; 1a, steel pipe; 1b, pole I; 1c, pole II; 1d, torque wrench open holes; 2, spanner head; 2a, nut open holes; 3, pin I; 4, torsion spring; 5, pin II; 6, traction cable.
Embodiment
Below in conjunction with drawings and Examples, the utility model is described in detail.
The assembling position being assembled part in the present embodiment is positioned at first row's nut on the right side of engine fan rotor balance assembly, and limiter requires within the scope of 72N-78N, and instrument must enter in cavity from portlet, and nut installs position at �� 225mm circumferentially.
Use the utility model engine nut setting tool it to be assembled, as shown in Figure 1, comprising: support 1, spanner head 2, pin I 3, torsion spring 4, traction cable 6; Support 1 comprises steel pipe 1a and is located at pole I 1b and pole II 1c at steel pipe 1a two ends, pole I 1b and pole II 1c is provided with steel pipe 1a coupling end and is connected hanger, and the connection hanger of pole I 1b and pole II 1c is located in steel pipe 1a by pin II 5 to connect and is welded into one-piece construction; Pole II 1c is connected by pin I 3 and torsion spring 4 with spanner head 2, pole I 1b is provided with torque wrench open holes 1d, spanner head 2 is provided with and torque wrench open holes 1d nut open holes 2a in the same horizontal line, traction cable 6 one end is fixed on spanner head 2, and the other end is located on steel pipe 1a and is extend out to pole I 1b side.
During assembling, engine nut setting tool to be entered from right output port after folding up, as shown in Figure 2, instrument unclamps traction cable 6 after entering cavity, spanner head 2 is by torsion spring 4 elasticity, making spanner head 2 be bound to working position, spanner head 2 is processed with the nut open holes 2a coordinated with fastening nut, its central position is consistent with the torque wrench open holes 1d center on pole I 1b, power loss when avoiding exerting a force, prevents torque wrench reading value can not be subject to power actual value by actual response nut. Support 1 main body adopts steel pipe 1a structure, namely alleviates the weight of instrument, can not produce bending phenomenon when exerting a force again, ensure that the rigidity of instrument, installs through in-site modeling, and each item data all meets design requirements, reaches the object of expection.
Above-described embodiment, only for technical conceive of the present utility model and feature are described, its object is to allow person skilled in the art can understand content of the present utility model and implement according to this, can not limit protection domain of the present utility model with this. All equivalences done according to the utility model spirit change or modify, and all should be encompassed within protection domain of the present utility model.

Claims (2)

1. an engine nut setting tool, it is characterised in that, comprising: support (1), spanner head (2), pin I (3), torsion spring (4), traction cable (6), described support (1) comprises steel pipe (1a) and is located at pole I (1b) and the pole II (1c) at steel pipe (1a) two ends, described pole II (1c) is connected by pin I (3) and torsion spring (4) with spanner head (2), described pole I (1b) is provided with torque wrench open holes (1d), described spanner head (2) is provided with and torque wrench open holes (1d) nut open holes (2a) in the same horizontal line, described traction cable (6) one end is fixed on spanner head (2), the other end is located at steel pipe (1a) and is gone up and extend out to pole I (1b) side.
2. according to a kind of engine nut setting tool according to claim 1, it is characterized in that, described pole I (1b) and pole II (1c) are provided with steel pipe (1a) coupling end and are connected hanger, and the connection hanger of described pole I (1b) and pole II (1c) is located in steel pipe (1a) by pin II (5) to connect and is welded into one-piece construction.
CN201520947790.4U 2015-11-24 2015-11-24 Engine nut mounting tool Active CN205271852U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520947790.4U CN205271852U (en) 2015-11-24 2015-11-24 Engine nut mounting tool

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520947790.4U CN205271852U (en) 2015-11-24 2015-11-24 Engine nut mounting tool

Publications (1)

Publication Number Publication Date
CN205271852U true CN205271852U (en) 2016-06-01

Family

ID=56056473

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201520947790.4U Active CN205271852U (en) 2015-11-24 2015-11-24 Engine nut mounting tool

Country Status (1)

Country Link
CN (1) CN205271852U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109352568A (en) * 2018-11-21 2019-02-19 中国航发沈阳黎明航空发动机有限责任公司 A kind of engine nut installation tool for preventing torque to be distorted
CN115741070A (en) * 2022-11-30 2023-03-07 中国航发沈阳发动机研究所 Tool and method for disassembling and assembling connecting nut in shaft cavity of aircraft engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109352568A (en) * 2018-11-21 2019-02-19 中国航发沈阳黎明航空发动机有限责任公司 A kind of engine nut installation tool for preventing torque to be distorted
CN115741070A (en) * 2022-11-30 2023-03-07 中国航发沈阳发动机研究所 Tool and method for disassembling and assembling connecting nut in shaft cavity of aircraft engine
CN115741070B (en) * 2022-11-30 2024-01-30 苏州海通机器人系统有限公司 Tool and method for disassembling and assembling nut in shaft cavity of aero-engine

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CP01 Change in the name or title of a patent holder
CP01 Change in the name or title of a patent holder

Address after: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6

Patentee after: Chinese Hangfa Shenyang Liming Aero engine limited liability company

Address before: 110043 Dong TA street, Dadong District, Shenyang, Liaoning Province, No. 6

Patentee before: Liming Aeroplane Engine (Group) Co., Ltd., Shenyang City