SU542926A1 - Intra-model aerodynamic scales - Google Patents

Intra-model aerodynamic scales

Info

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
Application number
SU2016005A
Other languages
Russian (ru)
Inventor
Вячеслав Иванович Лагутин
Амирий Владимирович Тертерашвили
Виталий Степанович Трусов
Original Assignee
Предприятие П/Я М-5539
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Предприятие П/Я М-5539 filed Critical Предприятие П/Я М-5539
Priority to SU2016005A priority Critical patent/SU542926A1/en
Application granted granted Critical
Publication of SU542926A1 publication Critical patent/SU542926A1/en

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)

1. Авторское свидетельство 1. Copyright certificate 344313, М. Кл.2 G 01М 9/00, 1971 г. 344313, M. Kl.2 G 01M 9/00, 1971
SU2016005A 1974-04-12 1974-04-12 Intra-model aerodynamic scales SU542926A1 (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (4)

* Cited by examiner, † Cited by third party
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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