FIELD: aircraft engineering. SUBSTANCE: system for suspension of cargo 7 to helicopter 1 has grippers 4 and 5 with junctures 2 and 3, support 6, a cargo horizontal attitude unit made in the form of propulsion devices 9 and 10, a unit for controlling position of grippers 4 and 5 relative to cargo 7 which has four drives. Junctures 2 and 3 of grippers 4 and 5 are made from rigid collapsible sections. EFFECT: improved operating characteristics. 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| HELICOPTER EXTERNAL LOAD SLING SYSTEM | 1992 |
|
RU2030332C1 |
| TOWED TARGET FOR IMITATION OF FLYING VEHICLES | 0 |
|
SU1837036A1 |
| DEVICE FOR MEASURING FLOW PARAMETERS IN CLOUDS | 1992 |
|
RU2015072C1 |
| SYSTEM FOR CONTROLLING ATTITUDE OF CARGO SUSPENDED TO HELICOPTER ON FLEXIBLE LINK FOR ASSEMBLING WORKS | 1992 |
|
RU2015075C1 |
| DEVICE TO MEASURE MODULE AND DIRECTION OF FLOW SPEED VECTOR | 1992 |
|
RU2029958C1 |
| TOWED BODY ATTITUDE CONTROL DEVICE | 1992 |
|
RU2006429C1 |
| DEVICE FOR MEASURING CHARACTERISTICS OF AERIAL FIELD | 0 |
|
SU1810844A1 |
| TOWABLE PLANAR SYSTEM | 0 |
|
SU1835373A1 |
| ANTENNA FIELD PARAMETERS TESTER | 0 |
|
SU1737374A1 |
| SYSTEM FOR HANDLING CARGO SUSPENDED ON EXTERNAL STORE OF HELICOPTER | 1991 |
|
RU2005665C1 |
