FIELD: testing equipment. SUBSTANCE: gear has driving hydraulic cylinders 2 and 3 hinged to driving levers 4 and 5 and loading hydraulic cylinders 10 and 11 each being hinged to proper driving 4 (5) and additional levers 6 (7) and coupled through strain-gauge dynamometers 8 and 9 lever systems 12 and 13 to tested diviated links 14 and 15. Each strain-gauge dynamometer is provided with position pickups 16 and 17 which output links 18 and 19 are also coupled to lever systems 12 and 13. Driving hydraulic cylinders 2 and 3, loading hydraulic cylinders 10 and 11, strain-gauge dynamometers 8 and 9 and positions pickups 16 and 17 are connected to program-time control device 22. EFFECT: enhanced testing authenticity. 3 dwg
Title | Year | Author | Number |
---|---|---|---|
DEVICE FOR TESTING AIRCRAFT FLAP | 1994 |
|
RU2078321C1 |
DEVICE FOR TESTING TWO-SECTIONAL CONTROL SURFACES OF AEROPLANE | 1990 |
|
RU1762621C |
BED TO TEST SUPPORTS OF LANDING GEAR OF AIRCRAFT | 1989 |
|
RU1658718C |
AIRCRAFT FLAPS CONTROL SYSTEM | 1992 |
|
RU2065377C1 |
SET FOR TESTING WING HIGH-LIFT DEVICES | 1996 |
|
RU2095775C1 |
FLYING VEHICLE CONTROL COLUMN | 1991 |
|
RU2018459C1 |
CARGO COMPARTMENT OF FLYING VEHICLE | 1995 |
|
RU2099240C1 |
DEVICE FOR TEST STRENGTH OF FLAP OF AIRCRAFT | 1989 |
|
SU1607558A1 |
AIRCRAFT ENGINE CONTROL SYSTEM | 1990 |
|
RU1707896C |
FUR SKIN DRYING DEVICE | 1990 |
|
RU2027768C1 |
Authors
Dates
1995-10-10—Published
1992-11-05—Filed