FIELD: equipment testing panels of flying vehicles and other structures for strength. SUBSTANCE: proposed gear for strength testing of panels includes rigid frame which carries two systems of compression force loading in mutually perpendicular directions with force-transmitting members and system of shear force loading. Gear is equipped with grippers 10 with grooves in working faces and wedge-shaped protrusions on opposite faces, bearings 11 positioned in of bearing casings 9, duct 12 hinged to panel in one point and resting against panel with the aid of rolling bearings 16 arranged on edges of duct with spacing determined from condition of avoidance of local loss of stability of sheathing between these bearings. Elastic shell 14 tightly attached to panel is put on outer surface of duct. EFFECT: increased operational reliability of gear. 2 dwg
Title | Year | Author | Number |
---|---|---|---|
DEVICE FOR PERFORMING STRENGTH TESTS | 1990 |
|
SU1840411A2 |
ADAPTIVE WING | 1990 |
|
SU1762488A1 |
SAMPLE FOR TESTING SUPPORTED PANEL | 1988 |
|
SU1840335A1 |
PNEUMATIC SUPPORT FOR SUPPORTING OF FLIGHT VEHICLES AT DYNAMIC LOAD TESTS | 1983 |
|
RU2129230C1 |
METHOD FOR FASTENING OF THERMOCOUPLES | 1982 |
|
RU2034246C1 |
MECHANIZED STOREHOUSE FOR LONG-MEASURE PRODUCTS | 1991 |
|
RU2041142C1 |
METHOD OF FORCE MEASUREMENT UNDER CLIMATIC TESTS OF STRUCTURE OF FLYING VEHICLE FOR STRENGTH AND GEAR FOR ITS REALIZATION | 1990 |
|
RU2085876C1 |
DEVICE MEASURING DEFORMATIONS OF FLEXIBLE ENVELOPES OF FLYING VEHICLES | 1994 |
|
RU2082082C1 |
RELOADING MACHINE | 1991 |
|
RU2009969C1 |
GEAR FOR ANGULAR AND LINEAR MOVEMENT OF MODEL OF AIRCRAFT IN WIND TUNNEL | 1994 |
|
RU2102714C1 |
Authors
Dates
1997-05-20—Published
1994-06-21—Filed