SU795150A3 - Bench for determining characteristics of dynamic rigidly of aircraft control actuators - Google Patents

Bench for determining characteristics of dynamic rigidly of aircraft control actuators

Info

Publication number
SU795150A3
SU795150A3 SU2712667/23A SU2712667A SU795150A3 SU 795150 A3 SU795150 A3 SU 795150A3 SU 2712667/23 A SU2712667/23 A SU 2712667/23A SU 2712667 A SU2712667 A SU 2712667A SU 795150 A3 SU795150 A3 SU 795150A3
Authority
SU
USSR - Soviet Union
Prior art keywords
bench
rigidly
dynamic
aircraft control
control actuators
Prior art date
Application number
SU2712667/23A
Other languages
Russian (ru)
Inventor
С.Ф. Алферов
Original Assignee
ЦАГИ им.профессора Н.Е.Жуковского
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 ЦАГИ им.профессора Н.Е.Жуковского filed Critical ЦАГИ им.профессора Н.Е.Жуковского
Priority to SU2712667/23A priority Critical patent/SU795150A3/en
Application granted granted Critical
Publication of SU795150A3 publication Critical patent/SU795150A3/en

Links

SU2712667/23A 1979-01-16 1979-01-16 Bench for determining characteristics of dynamic rigidly of aircraft control actuators SU795150A3 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU2712667/23A SU795150A3 (en) 1979-01-16 1979-01-16 Bench for determining characteristics of dynamic rigidly of aircraft control actuators

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU2712667/23A SU795150A3 (en) 1979-01-16 1979-01-16 Bench for determining characteristics of dynamic rigidly of aircraft control actuators

Publications (1)

Publication Number Publication Date
SU795150A3 true SU795150A3 (en) 1994-02-15

Family

ID=60523526

Family Applications (1)

Application Number Title Priority Date Filing Date
SU2712667/23A SU795150A3 (en) 1979-01-16 1979-01-16 Bench for determining characteristics of dynamic rigidly of aircraft control actuators

Country Status (1)

Country Link
SU (1) SU795150A3 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU191471U1 (en) * 2019-04-23 2019-08-07 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Aircraft dynamical load testing machine
CN111537170A (en) * 2020-05-21 2020-08-14 北京航空航天大学 Dynamic stiffness testing method for servo actuator

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU191471U1 (en) * 2019-04-23 2019-08-07 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Aircraft dynamical load testing machine
CN111537170A (en) * 2020-05-21 2020-08-14 北京航空航天大学 Dynamic stiffness testing method for servo actuator
CN111537170B (en) * 2020-05-21 2021-06-15 北京航空航天大学 Dynamic stiffness testing method for servo actuator

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