CN205464158U - Aircraft riveter presser foot seat - Google Patents

Aircraft riveter presser foot seat Download PDF

Info

Publication number
CN205464158U
CN205464158U CN201620257407.7U CN201620257407U CN205464158U CN 205464158 U CN205464158 U CN 205464158U CN 201620257407 U CN201620257407 U CN 201620257407U CN 205464158 U CN205464158 U CN 205464158U
Authority
CN
China
Prior art keywords
presser foot
presser feet
foot seat
feet seat
seat main
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
CN201620257407.7U
Other languages
Chinese (zh)
Inventor
周峰
吴烂平
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.)
AVIC Beijing Aeronautical Manufacturing Technology Research Institute
Original Assignee
Yixing Rongxing Casting 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 Yixing Rongxing Casting Co ltd filed Critical Yixing Rongxing Casting Co ltd
Priority to CN201620257407.7U priority Critical patent/CN205464158U/en
Application granted granted Critical
Publication of CN205464158U publication Critical patent/CN205464158U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Toys (AREA)

Abstract

The utility model discloses an aircraft riveter presser foot seat, its structure includes presser foot seat main part (1), and airborne laser range finder mounting panel (2) is connected to presser foot seat main part (1), and open at airborne laser range finder mounting panel (2) center has main shaft mounting hole (3), and main shaft spacing groove (4) are established to presser foot seat main part (1) inboard, and piston rod mounting hole (5) are established to presser foot seat main part (1) bottom, and fixed orifices (6) are established to piston rod mounting hole (5) both sides. The utility model discloses an advantage: be equipped with aircraft riveter compact structure, stable performance, the convenient operation safety of this presser foot seat, realize that automatic fixed position rotation punches, it is accurate high -efficient, sturdy and durable.

Description

Airplane riveting machine presser feet seat
Technical field
The utility model relates to airplane riveting machine presser feet seat.
Background technology
In the manufacture of aircraft produces, being Manual punching before rivet hole, efficiency is low, and speed is slow, There is also the inaccurate situation of punch position.
Rivet driver is based on the riveting equipment that cold rolling principle develops, and referring to can be with rivet article riveting Pick up mechanized equipment.Common are pneumatic, oil pressure and electronic, single head and double end equal-specification model. Common type mainly has automatic riveter and riveter.
But common rivet driver insufficient strength, and the high-precision requirement in airplane riveting hole cannot be met.
Summary of the invention
The utility model proposes airplane riveting machine presser feet seat, its purpose is intended to overcome prior art Above shortcomings, it is achieved High Precision Automatic position rotating is punched.
Technical solution of the present utility model: airplane riveting machine presser feet seat, its structure includes presser feet Seat main body, presser feet seat main body connects airborne laser range finder installing plate, and airborne laser range finder installing plate center is opened Having spindle mounting hole, set main shaft stopper slot inside presser feet seat main body, presser feet seat bottom part body sets piston Bar installing hole, piston rod installing hole both sides set fixing hole.
Preferably, described presser feet seat main body is 90 ° with the angle of airborne laser range finder installing plate.
Advantage of the present utility model: with the airplane riveting machine compact conformation of this presser feet seat, performance steady Fixed, easy and safe to operate, it is achieved automatic positioning rotating punches, precise and high efficiency, sturdy and durable.
Accompanying drawing explanation
Fig. 1 is the structural representation of airplane riveting machine presser feet seat.
In figure 1 be presser feet seat main body, 2 be airborne laser range finder installing plate, 3 be spindle mounting hole, 4 it is main shaft stopper slot, 5 is piston rod installing hole, 6 is fixing hole.
Detailed description of the invention
Below in conjunction with embodiment and detailed description of the invention, this utility model made further details of theory Bright.
As it is shown in figure 1, airplane riveting machine presser feet seat, its structure includes presser feet seat main body 1, presser feet Seat main body 1 connects airborne laser range finder installing plate 2, and airborne laser range finder installing plate 2 center has main shaft peace Dress hole 3, sets main shaft stopper slot 4, sets piston rod bottom presser feet seat main body 1 inside presser feet seat main body 1 Installing hole 5, piston rod installing hole 5 both sides set fixing hole 6.
Described presser feet seat main body 1 is 90 ° with the angle of airborne laser range finder installing plate 2.
Above-described is only preferred implementation of the present utility model, it is noted that for ability For the those of ordinary skill in territory, on the premise of creating design without departing from this utility model, also may be used To make some deformation and improvement, these broadly fall into protection domain of the present utility model.

Claims (2)

1. airplane riveting machine presser feet seat, its feature includes presser feet seat main body (1), presser feet seat main body (1) Connecting airborne laser range finder installing plate (2), airborne laser range finder installing plate (2) center has main shaft and installs Hole (3), presser feet seat main body (1) inner side sets main shaft stopper slot (4), presser feet seat main body (1) end Portion sets piston rod installing hole (5), and piston rod installing hole (5) both sides set fixing hole (6).
2. airplane riveting machine presser feet seat as claimed in claim 1, is characterized in that described presser feet seat Main body (1) is 90 ° with the angle of airborne laser range finder installing plate (2).
CN201620257407.7U 2016-03-30 2016-03-30 Aircraft riveter presser foot seat Active CN205464158U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201620257407.7U CN205464158U (en) 2016-03-30 2016-03-30 Aircraft riveter presser foot seat

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201620257407.7U CN205464158U (en) 2016-03-30 2016-03-30 Aircraft riveter presser foot seat

Publications (1)

Publication Number Publication Date
CN205464158U true CN205464158U (en) 2016-08-17

Family

ID=56648064

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201620257407.7U Active CN205464158U (en) 2016-03-30 2016-03-30 Aircraft riveter presser foot seat

Country Status (1)

Country Link
CN (1) CN205464158U (en)

Similar Documents

Publication Publication Date Title
CN204646924U (en) A kind of spring detent
CN103452409A (en) Hinge with door stopper structure and door closer structure
CN203245761U (en) Push-pull-type positioning device
CN205464158U (en) Aircraft riveter presser foot seat
CN205478772U (en) Special type clutch driven plate assembly stop pin riveting equipment
CN213080167U (en) Furniture design is with positioner that punches
CN103967905A (en) Non-falling structure for access panel lock
CN205464152U (en) Aircraft riveter encoder axle
CN104607587A (en) Device for assembling printer hinge base
CN205464159U (en) Aircraft riveter main shaft feeds a ram cover
CN205464456U (en) Seat is fed in drilling of aircraft riveter
CN205571310U (en) Aircraft riveter gas -liquid pressure cylinder
CN205464153U (en) Aircraft riveter reading head support
CN208116672U (en) Aircraft automatic riveter nails introducer follows closely slot
CN205464150U (en) Aircraft riveter main shaft feed mechanism
CN202824334U (en) Localizable dinking
CN105642953A (en) Drilling feeding seat of aircraft riveting machine
CN203986398U (en) A kind of easy mounting shoe buckle
CN208555685U (en) A kind of stamping die of door lock substrate
CN204396603U (en) Automobile-used mould single-side cutting edge is tossed about device
CN203380317U (en) Raised head solid rivet head punch
CN105665602A (en) Aircraft riveter pneumatic-hydraulic pressure cylinder
CN204686976U (en) A kind of universal adjustable drill bushing installation form
CN208116675U (en) Aircraft automatic riveter nails introducer follows closely slot push plate
CN208116670U (en) Aircraft automatic riveter nails introducer nail clip

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: Presser foot seat of aircraft riveting machine

Effective date of registration: 20200921

Granted publication date: 20160817

Pledgee: Jiangsu Yixing rural commercial bank Limited by Share Ltd. Branch Park Branch

Pledgor: YIXING RONGXING CASTING Co.,Ltd.

Registration number: Y2020990001143

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

Date of cancellation: 20210825

Granted publication date: 20160817

Pledgee: Jiangsu Yixing rural commercial bank Limited by Share Ltd. Branch Park Branch

Pledgor: YIXING RONGXING CASTING Co.,Ltd.

Registration number: Y2020990001143

PC01 Cancellation of the registration of the contract for pledge of patent right
TR01 Transfer of patent right

Effective date of registration: 20220518

Address after: 100000 courtyard 1, Chaoyang Road, Chaoyang District, Beijing

Patentee after: AVIC BEIJING AERONAUTICAL MANUFACTURING TECHNOLOGY Research Institute

Address before: 214200 Yixing Rongxing Foundry Co., Ltd., No. 15, Huixing North Road, Zhuqiao Economic Development Zone, Yixing City, Wuxi City, Jiangsu Province

Patentee before: YIXING RONGXING CASTING CO.,LTD.

TR01 Transfer of patent right