CN206140356U - Frock is used in equipment of whole drive electricity generation pump motor sub -assembly of aircraft - Google Patents
Frock is used in equipment of whole drive electricity generation pump motor sub -assembly of aircraft Download PDFInfo
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- CN206140356U CN206140356U CN201620845125.9U CN201620845125U CN206140356U CN 206140356 U CN206140356 U CN 206140356U CN 201620845125 U CN201620845125 U CN 201620845125U CN 206140356 U CN206140356 U CN 206140356U
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Abstract
The utility model relates to a frock is used in equipment of whole drive electricity generation pump motor sub -assembly of aircraft, including the base, the middle part is equipped with solid fixed ring on the base, and gu the fixed ring center is equipped with logical groove, the support post is installed to the right part on the base, and the support post upper end is connected with the briquetting with clearance fit's mode, and the briquetting right -hand member is connected with the locating lever, under the locating lever end screw thread connection have with the base offset to the post, the briquetting left end has and is unciform convex part, the left part is equipped with the mount pad on the base. The utility model discloses a to fixing of casing, can conveniently pack subsequent spare part into and assemble in fixed sloping cam plate casing, reached the effect that has reduced the equipment degree of difficulty and improvement work efficiency then. And the utility model discloses replaced traditional simple fixed bolster and instrument, it is fixed effectively to make the product obtain, accomplishes the equipment at crucial position, has solved former assembly and has not fixed well, assembles coarse problem, has improved product Assembly efficiency and quality.
Description
Technical field
This utility model is related to a kind of frock repaired and install, specifically a kind of aircraft Integrated Driven Generator pump
Motor sub-assembly assembling frock.
Background technology
When the pump motor component of aircraft Integrated Driven Generator is repaired, need to carry out the fixed cell of pump motor component
Assembling, the fixed cell structure of the pump motor component is by housing, stationary housing axle, fixed swash plate, pin, piston shoes disk, cylinder body
Constitute with plunger, guide ring etc., but in man-made assembly, be required in most cases it is artificial on the other hand housing is fixed,
The correspondence position in housing is assembled and be installed to other assemblies by another handss, and relative operation is comparatively laborious.
The content of the invention
Pump motor assembling components based on above-mentioned aircraft Integrated Driven Generator operate comparatively laborious defect, and this practicality is new
Type proposes a kind of aircraft Integrated Driven Generator pump motor component that can be used to fixing that oblique disk shell is assembled in order to each part
Assembling frock.
Technical problem to be solved in the utility model employs the following technical solutions to realize：
A kind of aircraft Integrated Driven Generator pump motor assembling components frock, including base, on the base, middle part sets
Have retainer ring, the retainer ring center is provided with groove, right part is provided with support column on the base, the support column upper end with
The mode that gap coordinates is connected with briquetting, and the briquetting right-hand member is connected with locating rod, the locating rod lower end be threaded with
Base offset to post, the briquetting left end has in hook-shaped convex portion, and on the base, left part is provided with mounting seat.
The convex portion is located at the left side of groove.
This utility model is mainly used in the convenient assembling for sending out aircraft overall drive motor pump motor component, before assembly,
First furbuckles compression pin, axle group is installed on fixed oblique disk shell, housing assembly is encased in fixed oblique disk shell then
It is interior.
When in use, fixed oblique disk shell can be first seated in mounting seat so that fixed oblique disk shell is in the big of axial direction
Hole face is fitted with retainer ring left end, and so that the right part of briquetting penetrates into the inside of fixed oblique disk shell.Then manually on
Lower regulation locating rod so that convex portion is penetrated in the areole of fixed oblique disk shell from fixed oblique disk shell, and with fixed swash plate
The side wall of housing tightly offsets, rotatable to post on this basis so that is supported with base again to post and is closed, and then is reached briquetting
And the effect that whole fixed oblique disk shell is fixed, and then conveniently follow-up parts are encased in fixed oblique disk shell.
This utility model has reached the effect for reducing assembling difficulty and improving work efficiency by aforesaid operations.
The beneficial effects of the utility model are：
This utility model can be facilitated and follow-up parts are encased in fixed oblique disk shell by the fixation to housing
Assembled, reached then the effect for reducing assembling difficulty and improving work efficiency.And this utility model instead of biography
Unite simple fixed support and instrument, product is effectively fixed, complete the assembling of key position, assembling before solving
Bad fixation, assembles inaccurate problem, improves Product Assembly efficiency and quality.
Description of the drawings
With reference to the accompanying drawings and examples this utility model is further illustrated.
Fig. 1 is axonometric chart of the present utility model；
Fig. 2 is the part detonation configuration figure of aircraft Integrated Driven Generator pump motor component of the present utility model.
Specific embodiment
In order that technological means, creation characteristic, reached purpose and effect that this utility model is realized are easy to understand, under
It is expanded on further in the face of this utility model.
As shown in figure 1, a kind of aircraft Integrated Driven Generator pump motor assembling components frock, including base 1, the bottom
On seat 1, middle part is provided with retainer ring 4, and 4 center of the retainer ring is provided with groove 2a, and on the base 1, right part is provided with support column 6,
6 upper end of the support column is connected with briquetting 3 in the way of the cooperation of gap, and 3 right-hand member of the briquetting is connected with locating rod 2, described fixed
Position bar 2 lower end be threaded with base 1 offset to post 7,3 left end of the briquetting has in hook-shaped convex portion 3a, the bottom
On seat 1, left part is provided with mounting seat 5.
The convex portion 3a is positioned at the left side of groove 2a.
This utility model is mainly used in the convenient assembling for sending out aircraft overall drive motor pump motor component, before assembly,
As shown in Fig. 2 first furbuckles compression pin 90, axle group 100 is installed on fixed oblique disk shell 130, then by housing assembly
10 are encased in fixed oblique disk shell 130.
When in use, fixed oblique disk shell 130 can be first seated in mounting seat 5 so that fixed oblique disk shell 130 is in axle
To macropore side fitted with 4 left end of retainer ring, and cause the right part of briquetting 3 to penetrate into the inside of fixed oblique disk shell 130.
Then adjust locating rod 2 manually up and down so that convex portion 3a penetrates into the side of fixed oblique disk shell 130 from fixed oblique disk shell 130
In cinclides, and tightly offset with the side wall of fixed oblique disk shell 130, it is rotatable to post 7 on this basis so as to post 7 and bottom
Seat 1 is supported again and is closed, and then reaches the effect for fixing briquetting 3 and whole fixed oblique disk shell 130, so it is convenient will be follow-up
Parts are encased in fixed oblique disk shell 130.
Ultimate principle of the present utility model, principal character and advantage of the present utility model has been shown and described above.One's own profession
The technical staff of industry it should be appreciated that this utility model is not restricted to the described embodiments, described in above-described embodiment and description
Simply principle of the present utility model, on the premise of without departing from this utility model spirit and scope, this utility model also has
Various changes and modifications, these changes and improvements are both fallen within claimed this utility model.This utility model is claimed
Scope is by appending claims and its equivalent thereof.
Claims (2)
1. a kind of aircraft Integrated Driven Generator pump motor assembling components frock, including base (1), it is characterised in that：It is described
On base (1), middle part is provided with retainer ring (4), and retainer ring (4) center is provided with groove (2a), right part peace on the base (1)
Equipped with support column (6), support column (6) upper end is connected with briquetting (3), briquetting (3) right-hand member in the way of the cooperation of gap
Be connected with locating rod (2), locating rod (2) lower end be threaded with base (1) offset to post (7), the briquetting (3)
Left end has in hook-shaped convex portion (3a), and on the base (1), left part is provided with mounting seat (5).
2. a kind of aircraft Integrated Driven Generator pump motor assembling components frock according to claim 1, its feature exist
In：The convex portion (3a) is positioned at the left side of groove (2a).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620845125.9U CN206140356U (en) | 2016-08-07 | 2016-08-07 | Frock is used in equipment of whole drive electricity generation pump motor sub -assembly of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620845125.9U CN206140356U (en) | 2016-08-07 | 2016-08-07 | Frock is used in equipment of whole drive electricity generation pump motor sub -assembly of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206140356U true CN206140356U (en) | 2017-05-03 |
Family
ID=58628891
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620845125.9U Active CN206140356U (en) | 2016-08-07 | 2016-08-07 | Frock is used in equipment of whole drive electricity generation pump motor sub -assembly of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206140356U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114770412A (en) * | 2022-06-01 | 2022-07-22 | 沈阳飞机工业（集团）有限公司 | Airplane combined transmission generator mounting fixture and using method |
-
2016
- 2016-08-07 CN CN201620845125.9U patent/CN206140356U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114770412A (en) * | 2022-06-01 | 2022-07-22 | 沈阳飞机工业（集团）有限公司 | Airplane combined transmission generator mounting fixture and using method |
| CN114770412B (en) * | 2022-06-01 | 2024-03-08 | 沈阳飞机工业（集团）有限公司 | Mounting fixture for aircraft combined transmission generator and using method |
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