SU542926A1 - Intra-model aerodynamic scales - Google Patents
Intra-model aerodynamic scalesInfo
- Publication number
- SU542926A1 SU542926A1 SU2016005A SU2016005A SU542926A1 SU 542926 A1 SU542926 A1 SU 542926A1 SU 2016005 A SU2016005 A SU 2016005A SU 2016005 A SU2016005 A SU 2016005A SU 542926 A1 SU542926 A1 SU 542926A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- intra
- model aerodynamic
- aerodynamic scales
- scales
- model
- Prior art date
Links
Landscapes
- Measurement Of Force In General (AREA)
- Force Measurement Appropriate To Specific Purposes (AREA)
Description
ральный стержень 2 и через упругие шарниры 3, расположенные в горизонтальной плоскости (и имеющие в вертикальной плоскости большую жесткость), воспринимаютс измерительными элементами 4 и регистрируютс с помошью наклеенных на эти элементы тензодатчйков 6. При этом за счет малой жесткости шарниров 3 в горизонтальном и осевом направлении измерительные элементы 4 практически разгружены от действи осевой силы Р . , боковой силы Рг И моментз рыскань М„. Аналогично с помошью тензодатчиков 6, наклеенных на измерительные элементы 5, производ т регистрацию боковой силы Рг и момента рыскань М„.The pivot rod 2 and through the elastic hinges 3 located in the horizontal plane (and having a vertical rigidity) are perceived by the measuring elements 4 and are recorded using strain gages 6 glued to these elements 6. At the same time, due to the small rigidity of the hinges 3 in the horizontal and axial the direction of the measuring elements 4 is practically unloaded from the action of the axial force P. , lateral force of Pr And moment ysk M '. Similarly, with the aid of strain gauges 6, glued to the measuring elements 5, the lateral force Pg and the yaw moment Mn are registered.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU2016005A SU542926A1 (en) | 1974-04-12 | 1974-04-12 | Intra-model aerodynamic scales |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU2016005A SU542926A1 (en) | 1974-04-12 | 1974-04-12 | Intra-model aerodynamic scales |
Publications (1)
Publication Number | Publication Date |
---|---|
SU542926A1 true SU542926A1 (en) | 1977-01-15 |
Family
ID=20581952
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU2016005A SU542926A1 (en) | 1974-04-12 | 1974-04-12 | Intra-model aerodynamic scales |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU542926A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103323178A (en) * | 2013-05-29 | 2013-09-25 | 哈尔滨工业大学 | Attitude motion simulation device with two degrees of freedom |
CN113670560A (en) * | 2021-10-21 | 2021-11-19 | 中国空气动力研究与发展中心低速空气动力研究所 | Pneumatic load measuring device of horizontal tail |
-
1974
- 1974-04-12 SU SU2016005A patent/SU542926A1/en active
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103323178A (en) * | 2013-05-29 | 2013-09-25 | 哈尔滨工业大学 | Attitude motion simulation device with two degrees of freedom |
CN103323178B (en) * | 2013-05-29 | 2015-07-08 | 哈尔滨工业大学 | Attitude motion simulation device with two degrees of freedom |
CN113670560A (en) * | 2021-10-21 | 2021-11-19 | 中国空气动力研究与发展中心低速空气动力研究所 | Pneumatic load measuring device of horizontal tail |
CN113670560B (en) * | 2021-10-21 | 2022-02-11 | 中国空气动力研究与发展中心低速空气动力研究所 | Pneumatic load measuring device of horizontal tail |
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