CN207554535U - A kind of supporting plate self-lock nut - Google Patents

A kind of supporting plate self-lock nut Download PDF

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Publication number
CN207554535U
CN207554535U CN201721673454.0U CN201721673454U CN207554535U CN 207554535 U CN207554535 U CN 207554535U CN 201721673454 U CN201721673454 U CN 201721673454U CN 207554535 U CN207554535 U CN 207554535U
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CN
China
Prior art keywords
self
supporting plate
lock nut
utility
model
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Active
Application number
CN201721673454.0U
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Chinese (zh)
Inventor
沈丽娟
楚亚春
郑冬梅
司荣宁
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AECC Shenyang Engine Research Institute
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AECC Shenyang Engine Research Institute
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Priority to CN201721673454.0U priority Critical patent/CN207554535U/en
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Publication of CN207554535U publication Critical patent/CN207554535U/en
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Abstract

The utility model provides a kind of supporting plate self-lock nut, is related to connector field, including:Self-lock nut supporting plate (1) and self-locking nut (2).The supporting plate self-lock nut of the utility model, eliminate the connection structure of bolt/screw, it is fixed in the bayonet of stent by the U-shaped flaring boss (3) of self-lock nut supporting plate (1), reduces the quantity of dismounting part, avoid the hidden danger of bolt/screw drop in assembling and dissembling process;U-shaped flaring boss (3) is disengaged out of bayonet by compressing self-lock nut supporting plate (1) during dismounting, decomposition of the supporting plate self-lock nut from aero-engine body can be realized in once-through operation.The supporting plate self-lock nut of the utility model, simplify for fix aero-engine exterior line, attachment and cable supporting plate self-lock nut structure, improve installation and removal efficiency, dismounting and working service are convenient, have larger practical value.

Description

A kind of supporting plate self-lock nut
Technical field
The utility model is related to connector field, more particularly to a kind of supporting plate self-lock nut.
Background technology
The fixation of a large amount of pipeline, attachment and cable employs supporting plate self-lock nut structure outside aero-engine, tradition Supporting plate self-lock nut be connected on aero-engine body using bolt/screw, be provided on the supporting plate of supporting plate self-lock nut Bolt/screw hole generally requires two bolt/screws and is fixed, and number of parts is more, removes and installs inconvenience, not only time-consuming Arduously, and in disassembly process there are the hidden danger that bolt/screw is scattered;Due to aero-engine exterior line, attachment and cable count Measure various so that assemble and disassemble the limited space of supporting plate self-lock nut, and traditional supporting plate self-lock nut remove and install need it is dedicated Spanner or sleeve have operating space certain requirement.Therefore, it need to design a kind of for fixing aeroengine pipeline, attached Supporting plate self-lock nut that the structure of part and cable simplifies, easy-to-mount, to meet the assembling of aero-engine continuous improvement With the requirement of maintainability.
Invention content
The utility model provides a kind of supporting plate self-lock nut, and to solve, traditional plate nut number of parts is more, dismounts The problem of inconvenient.
In order to achieve the above object, the utility model adopts the following technical solution:
A kind of supporting plate self-lock nut, including:
Self-lock nut supporting plate, it is rectangular, U-shaped flaring boss is set on the self-lock nut supporting plate, in the self-locking nut Limit hole is set respectively on two opposite sides of supporting plate;
Self-locking nut, mounting ear is provided in the position being adapted with the limit hole, and the self-locking nut passes through described Mounting ear is mounted in the limit hole of the self-lock nut supporting plate.
Optionally, the limit hole has scheduled displacement.
The beneficial effects of the utility model:The supporting plate self-lock nut of the utility model, by the self-lock nut supporting plate upper limit Position hole, realizes the installation of self-locking nut, reduces the quantity of dismounting part, by setting U-shaped flaring boss, by supporting plate self-locking spiral shell Mother is fixed in the bayonet of stent, can realize fast assembling-disassembling, easy to operate, meets aero-engine to assembling and maintainability Increasing requirement.
Description of the drawings
Attached drawing herein is incorporated into specification and forms the part of this specification, shows and meets the utility model Embodiment, and for explaining the principle of the utility model together with specification.
Fig. 1 is the supporting plate self-lock nut general illustration of the utility model;
Fig. 2 is the self-lock nut supporting plate schematic diagram of the utility model;
Fig. 3 is the sectional view of the self-locking nut of the utility model.
Specific embodiment
Here exemplary embodiment will be illustrated in detail, example is illustrated in the accompanying drawings.Following description is related to During attached drawing, unless otherwise indicated, the same numbers in different attached drawings represent the same or similar element.
As shown in Figure 1 to Figure 3, the supporting plate self-lock nut of the utility model, including:Self-lock nut supporting plate 1 and self-locking spiral shell Mother 2.
Specifically, self-lock nut supporting plate 1 is rectangular, U-shaped flaring boss 3 is provided with, in two phases of self-lock nut supporting plate 1 To side on be respectively arranged with limit hole 4;Self-locking nut 2 is provided with mounting ear 5, self-locking in the position being adapted with limit hole 4 Nut 2 is mounted on by mounting ear 5 in the limit hole 4 of self-lock nut supporting plate 1.Advantageously, the limit hole of self-lock nut supporting plate 1 4 are equipped with scheduled displacement, convenient for the dismounting of self-locking nut 2.In the present embodiment, supporting plate self-lock nut is passed through into self-locking nut support The U-shaped flaring boss 3 of plate 1 is fixed in the bayonet of stent, and when dismounting need to only compress self-lock nut supporting plate 1 by U-shaped flaring boss 3 It is disengaged out of bayonet, it is easy to operate.
The supporting plate self-lock nut of the utility model has carried out Curve guide impeller to traditional supporting plate self-lock nut structure, cancels The connection structure of bolt/screw, by supporting plate self-lock nut is fixed on stent by the U-shaped flaring boss 3 of self-lock nut supporting plate 1 Bayonet in, reduce dismounting part quantity, effectively eliminate the hidden danger that bolt/screw is scattered, eliminate assembling-disassembling bolt/screw The demand of limiting operation and operating space is carried out using specific purpose tool;Self-lock nut supporting plate 1 need to be only compressed during dismounting by U-shaped flaring Boss 3 is disengaged out of stent bayonet, and decomposition of the supporting plate self-lock nut from aero-engine body can be realized in once-through operation, behaviour Make simplicity, can realize rapid-assembling/disassembling, meet aero-engine to assembling and the increasing requirement of maintainability.This practicality is new The supporting plate self-lock nut of type simplifies the supporting plate self-lock nut for fixing aero-engine exterior line, attachment and cable Structure improves installation and removal efficiency, and dismounting and working service are convenient, have larger practical value.
The above, only specific embodiment of the present utility model, but the scope of protection of the utility model is not limited to In this, in the technical scope that any one skilled in the art discloses in the utility model, the change that can readily occur in Change or replace, should be covered within the scope of the utility model.Therefore, the scope of protection of the utility model should be with described Subject to scope of the claims.

Claims (2)

1. a kind of supporting plate self-lock nut, which is characterized in that including:
Self-lock nut supporting plate (1), it is rectangular, U-shaped flaring boss (3) is set on the self-lock nut supporting plate (1), in the self-locking Limit hole (4) is set respectively on two opposite sides of nut supporting plate (1);
Self-locking nut (2) is provided with mounting ear (5), the self-locking nut (2) in the position being adapted with the limit hole (4) By the mounting ear (5) in the limit hole (4) of the self-lock nut supporting plate (1).
2. supporting plate self-lock nut according to claim 1, which is characterized in that the limit hole (4) has scheduled displacement Amount.
CN201721673454.0U 2017-12-05 2017-12-05 A kind of supporting plate self-lock nut Active CN207554535U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201721673454.0U CN207554535U (en) 2017-12-05 2017-12-05 A kind of supporting plate self-lock nut

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201721673454.0U CN207554535U (en) 2017-12-05 2017-12-05 A kind of supporting plate self-lock nut

Publications (1)

Publication Number Publication Date
CN207554535U true CN207554535U (en) 2018-06-29

Family

ID=62665883

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201721673454.0U Active CN207554535U (en) 2017-12-05 2017-12-05 A kind of supporting plate self-lock nut

Country Status (1)

Country Link
CN (1) CN207554535U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109681512A (en) * 2018-11-30 2019-04-26 河南航天精工制造有限公司 A kind of supporting plate self-lock nut

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109681512A (en) * 2018-11-30 2019-04-26 河南航天精工制造有限公司 A kind of supporting plate self-lock nut

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