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

Links

Landscapes

  • 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

Similar Documents

Publication Publication Date Title
ATE77488T1 (en) IN VITRO TEST PROCEDURE FOR DETECTING CELLULAR IMMUNE RESPONSES.
DE3465692D1 (en) Guar gum food bar
SU1522885A1 (en) Device for testing members for controlling wing
IT1235432B (en) FOUR-POINT DEAD POINT CRANK
PT95211A (en) METHOD FOR PREPARING COMPOSITIONS FOR TOPICAL USE CONTAINING DESOLIMIZED DEOXY-RIBONUCLEIC ACIDS TO REDUCE VISIBLE DEFECTS OF EPIDER FROM THE FACE AND SOME AREAS OF THE BODY'S SKIN
DE3773333D1 (en) DEVICE FOR STEP-BY-STEP TRANSPORTING AND POSITIONING OF OBJECTS.
DE3775843D1 (en) BELLOW GAS METER.
JPS57186010A (en) Valve moving mechanism for engine with overhead cam shafts
GB2242983A (en) Rheometer calibration
SU1607558A1 (en) Device for test strength of flap of aircraft
NO901499D0 (en) APPARATUS.
GB1267307A (en) Adjusting device for an artificial limb
Obiri et al. The role of thiols in lymphocyte responses: effect of 2-mercaptoethanol on interleukin 2 production
BR0013559A (en) Double mast system for simulation test
JPS541088A (en) Bond strength tester of laminated materials
SU1091701A1 (en) DEVICE FOR LOADING OF AERODYNAMIC SURFACE OF AIRCRAFT
SU678821A1 (en) DEVICE FOR DISCONNECTING THE WIRING OF THE MECHANICAL MANAGEMENT SYSTEM OF THE AIRCRAFT
IT8147852A0 (en) DISPERSANTS BASED ON SULPHONATED DERIVATIVES OF LIGIN METHOD FOR THEIR PREPARATION AND THEIR USE IN COLORING COMPOSITIONS
Lighthart et al. RPST: A ROM-based pseudo-exhaustive self-test approach.
ES128537U (en) Car-chair for children, perfected. (Machine-translation by Google Translate, not legally binding)
GRAY FOOLPROOF' METHOD PRODUCES LIQUID BRIGHT GOLD FOR DECALS
ES1008282U (en) Lounger chair. (Machine-translation by Google Translate, not legally binding)
JPS5739307A (en) Method and device for measuring crack length
LEMAY Fatigue damage mechanisms and short crack growth
COUEDOR Experimental setup of jet simulation in a wind tunnel(Wind tunnel simulation of jet exhaust in low speed testing of Franco-German Alpha-Jet trainer and fire support aircraft)