FIELD: test equipment.
SUBSTANCE: invention relates to testing facilities. Stand for development of aircraft separation units consists of housing, base, lock for attachment of test object, trapping device, control panel. Catching device is a rocker mechanism comprising a block suspension, a rope connected to the test object and the link. Link is equipped with a slider to rule out the rope sagging and one of the ends is hinged on the support. Total weight of link with slider exceeds weight of trapped object.
EFFECT: simplified design, integrity of test object.
1 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| TEST BENCH FOR INVESTIGATION OF AIRCRAFT SYSTEMS SERVICEABILITY UNDER VACUUM AND WEIGHTLESSNESS CONDITIONS | 2018 |
|
RU2688505C1 |
| BALLISTIC BENCH FOR HIGH-SPEED THROW OF SOLID BODIES WHEN TESTING POWER PLANTS OF AIRCRAFTS | 2019 |
|
RU2741779C1 |
| TEST RIG FOR DETERMINATION OF HYDRAULIC RESIDUES OF FUEL IN MISSILE TANK | 2013 |
|
RU2543703C1 |
| SPACE APPARATUS SEPARATION DEVICES TEST BENCH | 2012 |
|
RU2489331C1 |
| ALL-WELDED BULLET TRAP | 2010 |
|
RU2422755C1 |
| METHOD OF MEMBRANE DESTRUCTION | 2015 |
|
RU2599066C1 |
| METHOD AND TEST RIG FOR DETERMINATION OF HYDRAULIC RESIDUES OF FUEL IN MISSILE TANK | 2013 |
|
RU2543702C1 |
| ACOUSTIC TEST RIG FOR ELECTRICAL AND MECHANICAL POWER ASSIST SYSTEM FOR VEHICLE | 2015 |
|
RU2610846C1 |
| BENCH FOR TESTING AND DEMONSTRATING OF EMERGENT ESCAPE FROM HELICOPTER | 2014 |
|
RU2562469C1 |
| BED FOR TESTING PNEUMOHYDRAULIC PISTONS OF TENSIONING DEVICES FOR FLOATING DRILLING PLATFORMS | 0 |
|
SU1137180A1 |
Authors
Dates
2019-05-21—Published
2018-05-15—Filed