FIELD: aeronautical engineering. SUBSTANCE: external load sling system for securing loads to helicopter 1 has slings 2 and 3 with grips 4 and 5, support 6, load-bearing beam 8 and unit 7 for orientation of load in horizontal plane. Support 6 and load-bearing beam 8 are secured to helicopter 1 and slings 2 and 3 are secured on load-bearing beam 8 which is made for rotation about support 6 in horizontal plane; unit 7 for orientation of load in horizontal plane is made in form of drive arranged on support 6 and kinematically linked with load-bearing beam 8. Besides that, drive is made in form of two winches 12 and 13 located on support 6 at diametrically opposite points and connected by means of two flexible couplings 14 and 15 with two sections of drum 16 secured axially on load-bearing beam 8. EFFECT: improved operational characteristics and ease in use through orientation of load in wide range of angles in horizontal plane. 2 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| HELICOPTER OUTER CARGO SUSPENSION SYSTEM | 1992 |
|
RU2015074C1 |
| TOWED BODY ATTITUDE CONTROL DEVICE | 1992 |
|
RU2006429C1 |
| SYSTEM FOR CONTROLLING ATTITUDE OF CARGO SUSPENDED TO HELICOPTER ON FLEXIBLE LINK FOR ASSEMBLING WORKS | 1992 |
|
RU2015075C1 |
| DEVICE FOR MEASURING FLOW PARAMETERS IN CLOUDS | 1992 |
|
RU2015072C1 |
| SYSTEM FOR HANDLING CARGO SUSPENDED ON EXTERNAL STORE OF HELICOPTER | 1991 |
|
RU2005665C1 |
| TOWED TARGET FOR IMITATION OF FLYING VEHICLES | 0 |
|
SU1837036A1 |
| ANTENNA FIELD PARAMETERS TESTER | 0 |
|
SU1737374A1 |
| DEVICE FOR MEASURING CHARACTERISTICS OF AERIAL FIELD | 0 |
|
SU1810844A1 |
| TOWABLE PLANAR SYSTEM | 0 |
|
SU1835372A1 |
| TOWABLE PLANAR SYSTEM | 0 |
|
SU1835373A1 |
