CN203822790U - Structure for connecting locking nail cap and stopping ring - Google Patents

Structure for connecting locking nail cap and stopping ring Download PDF

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Publication number
CN203822790U
CN203822790U CN201420260669.XU CN201420260669U CN203822790U CN 203822790 U CN203822790 U CN 203822790U CN 201420260669 U CN201420260669 U CN 201420260669U CN 203822790 U CN203822790 U CN 203822790U
Authority
CN
China
Prior art keywords
stopper ring
cap
pinning
pinning cap
nail cap
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
CN201420260669.XU
Other languages
Chinese (zh)
Inventor
王道益
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.)
GUIZHOU HANGRUI AVIATION PRECISION PARTS MANUFACTURING Co Ltd
Original Assignee
GUIZHOU HANGRUI AVIATION PRECISION PARTS MANUFACTURING 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 GUIZHOU HANGRUI AVIATION PRECISION PARTS MANUFACTURING Co Ltd filed Critical GUIZHOU HANGRUI AVIATION PRECISION PARTS MANUFACTURING Co Ltd
Priority to CN201420260669.XU priority Critical patent/CN203822790U/en
Application granted granted Critical
Publication of CN203822790U publication Critical patent/CN203822790U/en
Anticipated expiration legal-status Critical
Active legal-status Critical Current

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Abstract

A structure for connecting a locking nail cap and a stopping ring comprises the locking nail cap, the stopping ring and the sandwich layer board, wherein the nail foot of the locking nail cap is rectangular and is integrally connected with a nail cap to form the T-shaped locking nail cap; the stopping ring is a circular sheet; radial recesses are formed in the circumferential edge of a circular hole. Compared with the conventional structure, the structure provided by the utility model, is convenient to mount, demount and overhaul, improves the production efficiency and saves the cost. Since the structure is simple, the production and maintenance are very convenient, the quality consistency is good, and the quality is ensured.

Description

The linkage structure of a kind of pinning cap and stopper ring
Technical field
The utility model relates to a kind of quick-detachable lock structure, is a kind of mode of structure of the connection of pinning cap and stopper ring, and object is that pinning cap and stopper ring are assemblied in after sandwich plate, pinning cap and the stopper ring phenomenon that all can not get loose.
Background technique
Domestic-developed has many types to unload lock construction at present, but much quality all can not be guaranteed, and can not meet the technical requirements of ASM5591, and aircraft is caused to immeasurable consequence.Now corresponding product extrusion pressure is 200N left and right, and the extrusion pressure of this product is greater than 800N.
Summary of the invention
The purpose of this utility model is to provide a kind of simple in structure, can ensure the quality of products again, thereby solve the deficiency of various corresponding products.Meet extrusion pressure and be greater than 800N.Thereby ensured the safety of aircraft, and open and close lock is more convenient.
This is simple in structure, can ensure the quality of products again.
Described a kind of pinning cap and the linkage structure of stopper ring composition comprise: pinning cap, stopper ring, sandwich plate, the nail pin of pinning cap is made as cylindrical shape, cylinder staple foot plate surface central authorities have hole, the one, weight reduction, the 2nd, enhance mechanical strength, cylinder staple pin is also connected as a single entity and forms T shape pinning cap with the head of a nail; Stopper ring is a circular piece, and circle center hole circle edge has radial recess on edge.When assembling, first pinning cap is packed in sandwich plate, stopper ring is packed into from the bottom of pinning cap with special assembly tooling, be then loaded into 180kN.
Adopt the beneficial effect of the technical program: compared with former mode of structure, have the following advantages:
1, mounting or dismounting are convenient, are convenient to aircraft maintenance, improved manufacturing efficiency, it simple in structure.
2, cost-saving, due to simple in structure, no matter produce, maintenance is all very convenient, and other all share.
3, quality of product high conformity, quality is guaranteed, and has not only ensured product requirement performance, and more than can also ensureing that extrusion pressure reaches 900N.
Brief description of the drawings
Fig. 1 is of the present utility model group of view.
Fig. 2 a, 2b, 2c are respectively the structural drawing of pinning cap, stopper ring, sandwich plate.
In figure: 1-pinning cap, 2-stopper ring, 3-sandwich plate.
Embodiment
The linkage structure of a kind of pinning cap described in the utility model and stopper ring, embodiment now contrasts accompanying drawing and explains, its structure composition comprises: pinning cap 1, stopper ring 2, sandwich plate 3, the nail pin of pinning cap 1 is made as cylindrical shape cylindrical shape, nail foot plate surface central authorities have hole, the one, weight reduction, the 2nd, enhance mechanical strength, cylinder staple pin is also connected as a single entity and forms T shape pinning cap with the head of a nail; Stopper ring 2 is a circular piece, and hollow circle center hole circle edge has radial recess and double wedge on edge.When assembling, pinning cap is packed in sandwich plate, stopper ring is packed into from the bottom of pinning cap with special assembly tooling, be then loaded into 180kN.Firmly be locked at the object that reaches fixing clamp laminate 3 on nail pin by the double wedge on stopper ring 2, radial recess and the double wedge of stopper ring 2 are made as symmetrical recess and double wedge.

Claims (2)

1. the linkage structure of a pinning cap and stopper ring, it is characterized in that: its structure composition comprises: pinning cap (1), stopper ring (2), sandwich plate (3), the nail pin of pinning cap (1) is made as cylindrical base and is provided with hole, top is also connected as a single entity and forms T shape pinning cap with the head of a nail, in the middle of whole T shape pinning cap, be cavity, head of a nail top outer edge is to the bending of nail pin, and stopper ring (2) is a circular piece, center is circular hole, and hole circle has radial recess and alternate double wedge on all edges; When assembling, pinning cap is packed in sandwich plate, stopper ring (2) is packed into from the bottom of pinning cap (1) with special assembly tooling, be then loaded into 180kN, make stopper ring (2) have radial recess and alternate double wedge is locked head of a nail pin.
2. according to the pinning cap of claim 1 and the linkage structure of stopper ring, it is characterized in that: the radial recess of described stopper ring (2), is made as symmetrical recess.
CN201420260669.XU 2014-05-21 2014-05-21 Structure for connecting locking nail cap and stopping ring Active CN203822790U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420260669.XU CN203822790U (en) 2014-05-21 2014-05-21 Structure for connecting locking nail cap and stopping ring

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420260669.XU CN203822790U (en) 2014-05-21 2014-05-21 Structure for connecting locking nail cap and stopping ring

Publications (1)

Publication Number Publication Date
CN203822790U true CN203822790U (en) 2014-09-10

Family

ID=51478299

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420260669.XU Active CN203822790U (en) 2014-05-21 2014-05-21 Structure for connecting locking nail cap and stopping ring

Country Status (1)

Country Link
CN (1) CN203822790U (en)

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of utility model: Connection structure of nail locking cap and stop ring

Effective date of registration: 20221219

Granted publication date: 20140910

Pledgee: China Construction Bank Corporation Zunyi branch

Pledgor: GUIZHOU HANGRUI AVIATION PRECISION PARTS MANUFACTURING Co.,Ltd.

Registration number: Y2022520000054

PE01 Entry into force of the registration of the contract for pledge of patent right
PC01 Cancellation of the registration of the contract for pledge of patent right

Granted publication date: 20140910

Pledgee: China Construction Bank Corporation Zunyi branch

Pledgor: GUIZHOU HANGRUI AVIATION PRECISION PARTS MANUFACTURING Co.,Ltd.

Registration number: Y2022520000054

PC01 Cancellation of the registration of the contract for pledge of patent right