CN206704554U - Aircraft engine composite side guard plate - Google Patents
Aircraft engine composite side guard plate Download PDFInfo
- Publication number
- CN206704554U CN206704554U CN201720390630.3U CN201720390630U CN206704554U CN 206704554 U CN206704554 U CN 206704554U CN 201720390630 U CN201720390630 U CN 201720390630U CN 206704554 U CN206704554 U CN 206704554U
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- China
- Prior art keywords
- backplate
- composite
- handle
- aircraft engine
- pressing plate
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- 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.)
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Abstract
A kind of aircraft engine composite side guard plate is the utility model is related to, belongs to aircraft maintenance apparatus field.Provided with backplate, it is characterized in that, backplate bends to square, backplate bending part is arc lead angle, side above backplate is provided with handle through pressing plate, screw, side and front end above backplate are machined with the side groove and forward recess of bar shaped respectively, and the side of backplate is trapezium structure, and backplate, handle, pressing plate use composite.The utility model uses modularized design, and one solidification is formed by connecting, and solves the defects of conventional engines backplate volume is heavy, security performance is unstable；Enhance the anti-shock-absorbing capacity of composite backplate, heat-insulated and sealing simultaneously；It is easily assembled to, regular job is simple, and production efficiency is high.
Description
Technical field
Aircraft maintenance apparatus field is the utility model is related to, is particularly a kind of aircraft engine composite side shield
Plate.
Background technology
It is well-known：Aircraft engine protective plate has two kinds of metal structure protective plate, glass fibre reinforced plastic structure protective plate forms, its
Structure type is all split-type structural, and security performance is unstable, and the defects of low production efficiency, volume heaviness, and it is difficult to group
Dress, regular job are complicated.
The content of the invention
The purpose of this utility model is that overcome the deficiencies in the prior art, there is provided a kind of aircraft engine composite
Side guard plate, using modularized design, and one solidification is formed by connecting, and solves conventional engines backplate volume heaviness, security
Can be unstable the defects of；Enhance the anti-shock-absorbing capacity of composite backplate, heat-insulated and sealing simultaneously；It is easily assembled to, daily behaviour
Make simply, and production efficiency is high.
The utility model uses following technical solution：A kind of aircraft engine composite side guard plate, provided with shield
Plate, it is characterised in that backplate bends to square, and backplate bending part is arc lead angle, and the side above backplate is through pressing plate, spiral shell
Follow closely and handle is installed, the side and front end above backplate are machined with the side groove and forward recess of bar shaped respectively, and the side of backplate is
Trapezium structure, backplate, handle, pressing plate use composite.
The beneficial effects of the utility model are that using modularized design, and one solidification is formed by connecting, and solves traditional hair
The defects of motivation backplate volume is heavy, security performance is unstable；Simultaneously enhance the anti-shock-absorbing capacity of composite backplate, it is heat-insulated and
Sealing；It is easily assembled to, regular job is simple, and production efficiency is high.
Brief description of the drawings
The utility model is further illustrated with reference to the accompanying drawings and examples.
Fig. 1 is structural representation of the present utility model.
1. backplate in figure, 2. arc lead angles, 3. handles, 4. side grooves, 5. forward recess, 6. pressing plates, 7. screws.
Embodiment
As shown in figure 1, the utility model is provided with backplate 1, backplate 1 bends to square, and the bending part of backplate 1 is led for arc
Angle 2, the side of the top of backplate 1 are provided with handle 3 through pressing plate 6, screw 7, and the side and front end of the top of backplate 1 are machined with bar respectively
The side groove 4 and forward recess 5 of shape, the side of backplate 1 is trapezium structure, and side groove 4 and forward recess 5 are used for regular job, backplate
1st, handle 3, pressing plate 6 use composite.
Claims (1)
1. a kind of aircraft engine composite side guard plate, provided with backplate, it is characterised in that backplate bends to square, shield
Plate bending part is arc lead angle, and the side above backplate is provided with handle through pressing plate, screw, side and front end above backplate
The side groove and forward recess of bar shaped are machined with respectively, and the side of backplate is trapezium structure, and backplate, handle, pressing plate use composite wood
Material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720390630.3U CN206704554U (en) | 2017-04-14 | 2017-04-14 | Aircraft engine composite side guard plate |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720390630.3U CN206704554U (en) | 2017-04-14 | 2017-04-14 | Aircraft engine composite side guard plate |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206704554U true CN206704554U (en) | 2017-12-05 |
Family
ID=60455917
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720390630.3U Active CN206704554U (en) | 2017-04-14 | 2017-04-14 | Aircraft engine composite side guard plate |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206704554U (en) |
-
2017
- 2017-04-14 CN CN201720390630.3U patent/CN206704554U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |