SU1522885A1 - Device for testing members for controlling wing - Google Patents

Device for testing members for controlling wing

Info

Publication number
SU1522885A1
SU1522885A1 SU4404332/23A SU4404332A SU1522885A1 SU 1522885 A1 SU1522885 A1 SU 1522885A1 SU 4404332/23 A SU4404332/23 A SU 4404332/23A SU 4404332 A SU4404332 A SU 4404332A SU 1522885 A1 SU1522885 A1 SU 1522885A1
Authority
SU
USSR - Soviet Union
Prior art keywords
leading
edge slat
base
tested
testing members
Prior art date
Application number
SU4404332/23A
Other languages
Russian (ru)
Inventor
В.А. Сумароков
Г.Е. Любимов
В.М. Курушин
Original Assignee
В.А. Сумароков
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 В.А. Сумароков filed Critical В.А. Сумароков
Priority to SU4404332/23A priority Critical patent/SU1522885A1/en
Application granted granted Critical
Publication of SU1522885A1 publication Critical patent/SU1522885A1/en

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  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)

Abstract

FIELD: aircraft engineering. SUBSTANCE: device has parallelogram mechanism and is coupled with leading-edge slat 10 to be tested through hydraulic cylinders 7,8 and with movable base 2 through rockers 4,5. One rotates base 2 synchronously with leading-edge slat 10 to be tested. In so doing axes of rotation of leading-edge slat 10 and base 2 are coincident. In addition rocker 4 reciprocates with respect to link 11 simultaneously. EFFECT: enhanced reliability. 3 dwg
SU4404332/23A 1988-04-05 1988-04-05 Device for testing members for controlling wing SU1522885A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4404332/23A SU1522885A1 (en) 1988-04-05 1988-04-05 Device for testing members for controlling wing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4404332/23A SU1522885A1 (en) 1988-04-05 1988-04-05 Device for testing members for controlling wing

Publications (1)

Publication Number Publication Date
SU1522885A1 true SU1522885A1 (en) 1994-12-15

Family

ID=60517741

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4404332/23A SU1522885A1 (en) 1988-04-05 1988-04-05 Device for testing members for controlling wing

Country Status (1)

Country Link
SU (1) SU1522885A1 (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103303493B (en) * 2013-01-05 2015-12-02 中国航空工业集团公司西安飞机设计研究所 A kind of large aircraft strength test wing loads bringing device
CN106017877A (en) * 2016-05-16 2016-10-12 中国航空工业集团公司西安飞机设计研究所 Loading method in movable surface limit load test
CN107010245A (en) * 2016-01-28 2017-08-04 陕西飞机工业（集团）有限公司 A kind of flap-type rudder surface servo load maintainer
CN109163961A (en) * 2018-08-22 2019-01-08 中国飞机强度研究所 A kind of loading device of big deformation wing

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103303493B (en) * 2013-01-05 2015-12-02 中国航空工业集团公司西安飞机设计研究所 A kind of large aircraft strength test wing loads bringing device
CN107010245A (en) * 2016-01-28 2017-08-04 陕西飞机工业（集团）有限公司 A kind of flap-type rudder surface servo load maintainer
CN106017877A (en) * 2016-05-16 2016-10-12 中国航空工业集团公司西安飞机设计研究所 Loading method in movable surface limit load test
CN106017877B (en) * 2016-05-16 2018-11-13 中国航空工业集团公司西安飞机设计研究所 A kind of load loading method in active face Ultimate load test
CN109163961A (en) * 2018-08-22 2019-01-08 中国飞机强度研究所 A kind of loading device of big deformation wing

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