CN203889053U - Wing assembly adapter of small rocket - Google Patents
Wing assembly adapter of small rocket Download PDFInfo
- Publication number
- CN203889053U CN203889053U CN201420228960.9U CN201420228960U CN203889053U CN 203889053 U CN203889053 U CN 203889053U CN 201420228960 U CN201420228960 U CN 201420228960U CN 203889053 U CN203889053 U CN 203889053U
- Authority
- CN
- China
- Prior art keywords
- wing
- holes
- small rocket
- wing tip
- adapter
- 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.)
- Expired - Fee Related
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Abstract
The utility model belongs to the field of flight test technologies of airplanes and in particular relates to an adapter which is applied to a wing tip in a flight flutter test. The wing assembly adapter of a small rocket is characterized in that the assembly adapter is an aluminum plate; one side of the aluminum plate is closely attached to the front edge of the wing tip; a through hole is drilled in the aluminum plate and connected with the small rocket, and parts, close to the attached side of the wing tip, of the through holes are enlarged, so that screw heads connected with the small rocket are parallel and level with the attached side; other through holes are drilled in the aluminum plate, and screws penetrate through the through holes and are fixedly connected with onboard stripper plate nuts. By virtue of the adapter, the assembly tightness is guaranteed, and the directionality of the action force for launching the small rocket is also guaranteed.
Description
Technical field
The invention belongs to aircraft flight testing technique field, particularly relate to flutter take a flight test wing wing tip adopt adaptor.
Background technology
During flutter is taken a flight test, mouse need be arranged on to wing wing tip place, require fixingly reliable, and application force vertical ground is downward while ensureing mouse transmitting.Former certain type machine flutter adaptor that wing wing tip adopts of taking a flight test is to be the aluminium sheet of plane up and down, cannot fit tightly with wing wing tip place, also cannot ensure the directivity of the application force of the reliability that connects and mouse transmitting.
Summary of the invention
Goal of the invention
A kind of adaptor of installing of design, the directivity of the application force of the reliability that guarantee connects and mouse transmitting.
Invention technical scheme
Wing mouse is installed adaptor, this installation adaptor is the aluminium sheet that one side fits tightly with wing wing tip leading edge, on aluminium sheet, be drilled with through hole and connect mouse, and the part that these through holes approach wing wing tip binding face is expanded, the screw head that makes to connect mouse is concordant with binding face; On aluminium sheet, be drilled with other through holes, use screw to be fixedly connected with de-crab bolt on machine through through hole.
Invention effect
This adaptor had both ensured the tightness of installing, and had also ensured the directivity of the application force of mouse transmitting.
Brief description of the drawings
Fig. 1 is that wing wing tip place rocket is installed adaptor schematic diagram.
Detailed description of the invention
This adaptor, in certain type machine flutter middle use of taking a flight test, fixes wing wing tip mouse, in the process of taking a flight test, connects reliably, and downrange is perpendicular to ground.For achieving the above object, use CATIA design adaptor, wing mouse is installed adaptor, this installation adaptor is the aluminium sheet that one side fits tightly with wing wing tip leading edge, on aluminium sheet, be drilled with 12 Φ 4 through holes and connect mouse, and the part that these through holes approach wing wing tip binding face is expanded as to Φ 8, the screw head that makes to connect mouse is concordant with binding face; On aluminium sheet, be drilled with other through holes, use screw to be fixedly connected with de-crab bolt on machine through through hole.
Claims (1)
1. wing mouse is installed adaptor, it is characterized in that, this installation adaptor is the aluminium sheet that one side fits tightly with wing wing tip leading edge, on aluminium sheet, be drilled with through hole and connect mouse, and the part that these through holes approach wing wing tip binding face is expanded, the screw head that makes to connect mouse is concordant with binding face; On aluminium sheet, be drilled with other through holes, use screw to be fixedly connected with de-crab bolt on machine through through hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420228960.9U CN203889053U (en) | 2014-05-07 | 2014-05-07 | Wing assembly adapter of small rocket |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420228960.9U CN203889053U (en) | 2014-05-07 | 2014-05-07 | Wing assembly adapter of small rocket |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203889053U true CN203889053U (en) | 2014-10-22 |
Family
ID=51715488
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420228960.9U Expired - Fee Related CN203889053U (en) | 2014-05-07 | 2014-05-07 | Wing assembly adapter of small rocket |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203889053U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106441780A (en) * | 2016-09-06 | 2017-02-22 | 中国航空工业集团公司沈阳飞机设计研究所 | Scaling model flight flutter test pulse excitation method |
| CN106609790A (en) * | 2015-10-21 | 2017-05-03 | 波音公司 | High fracture toughness ceramic support nut plate and gang channel |
-
2014
- 2014-05-07 CN CN201420228960.9U patent/CN203889053U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106609790A (en) * | 2015-10-21 | 2017-05-03 | 波音公司 | High fracture toughness ceramic support nut plate and gang channel |
| CN106441780A (en) * | 2016-09-06 | 2017-02-22 | 中国航空工业集团公司沈阳飞机设计研究所 | Scaling model flight flutter test pulse excitation method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20141022 Termination date: 20170507 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |