SU470725A1 - Copier support for aircraft landing gear testing - Google Patents
Copier support for aircraft landing gear testingInfo
- Publication number
- SU470725A1 SU470725A1 SU1640561A SU1640561A SU470725A1 SU 470725 A1 SU470725 A1 SU 470725A1 SU 1640561 A SU1640561 A SU 1640561A SU 1640561 A SU1640561 A SU 1640561A SU 470725 A1 SU470725 A1 SU 470725A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- support
- landing gear
- aircraft landing
- frame
- runway
- Prior art date
Links
Landscapes
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
Description
ос м Х; У; Z (Р-,, P,j, Р) определ ютс углом ai и углом 02 клиньев 12.os m x; W; Z (P-, P, j, P) are determined by the angle ai and the angle 02 of the wedges 12.
Предмет нзобретенн Subject matter
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU1640561A SU470725A1 (en) | 1971-03-22 | 1971-03-22 | Copier support for aircraft landing gear testing |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU1640561A SU470725A1 (en) | 1971-03-22 | 1971-03-22 | Copier support for aircraft landing gear testing |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU904798054A Addition SU1728692A2 (en) | 1990-03-05 | 1990-03-05 | Device to test tightness of gas-filled articles |
Publications (1)
Publication Number | Publication Date |
---|---|
SU470725A1 true SU470725A1 (en) | 1975-05-15 |
Family
ID=20470672
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU1640561A SU470725A1 (en) | 1971-03-22 | 1971-03-22 | Copier support for aircraft landing gear testing |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU470725A1 (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104142221A (en) * | 2013-05-10 | 2014-11-12 | 中国直升机设计研究所 | Device for driving helicopter wheel to rotate |
CN106644347A (en) * | 2017-01-16 | 2017-05-10 | 南京航空航天大学 | Drop test device and drop test method of lander landing gear |
CN110155367A (en) * | 2019-05-29 | 2019-08-23 | 南京工业职业技术学院 | A kind of aircraft main landing gear anti-impact force test device |
CN111693309A (en) * | 2020-05-13 | 2020-09-22 | 南京航空航天大学 | Suspension releasing device for observing landing attitude change of lander and test method |
CN113049207A (en) * | 2021-03-30 | 2021-06-29 | 中国飞机强度研究所 | Drop test device and method thereof |
-
1971
- 1971-03-22 SU SU1640561A patent/SU470725A1/en active
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104142221A (en) * | 2013-05-10 | 2014-11-12 | 中国直升机设计研究所 | Device for driving helicopter wheel to rotate |
CN104142221B (en) * | 2013-05-10 | 2016-10-19 | 中国直升机设计研究所 | A kind of machine wheel rotating device |
CN106644347A (en) * | 2017-01-16 | 2017-05-10 | 南京航空航天大学 | Drop test device and drop test method of lander landing gear |
CN106644347B (en) * | 2017-01-16 | 2019-04-19 | 南京航空航天大学 | A kind of lander take-off and landing device drop test device and test method |
CN110155367A (en) * | 2019-05-29 | 2019-08-23 | 南京工业职业技术学院 | A kind of aircraft main landing gear anti-impact force test device |
CN111693309A (en) * | 2020-05-13 | 2020-09-22 | 南京航空航天大学 | Suspension releasing device for observing landing attitude change of lander and test method |
US20230055684A1 (en) * | 2020-05-13 | 2023-02-23 | Nanjing University Of Aeronautics And Astronautics | Suspending release device for observing drop vibration attitude changes of lander and test method |
CN113049207A (en) * | 2021-03-30 | 2021-06-29 | 中国飞机强度研究所 | Drop test device and method thereof |
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