FIELD: in-flight refuelling.
SUBSTANCE: device for stabilizing the cone of the fuel refuelling unit in flight contains a supply hose (1), a rigid bushing (2), a stabilizing aerodynamic body (3), a receiving ball joint (4), a gyroscopic dynamically balanced bushing (5), bearings of the gyroscopic bushing (6), front pillar (7), rear pillar (8), pipes (9). The branch pipes, open on the side of the supply hose and closed on the other side, have opposite holes located so that some holes (10) are directed tangentially to the surface of the gyroscopic sleeve, and the opposite holes (11) are directed outward.
EFFECT: improved stabilization of the aerodynamic cone during refuelling.
1 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| IN-FLIGHT REFUELING CONE STABILIZATION DEVICE | 2022 |
|
RU2797452C1 |
| AIR REFUELING SYSTEM WITH AUTOMATIC CONTROL AND AUTO-STABILIZED REFUELING DEVICE | 2023 |
|
RU2809164C1 |
| IN-FLIGHT FUELING UNIT TAPER GAGE | 2012 |
|
RU2490179C1 |
| FUELING UNIT TAPER GAGE | 2010 |
|
RU2436713C1 |
| AIR REFUELLING SYSTEM CONE SENSOR | 2013 |
|
RU2538479C2 |
| IN-FLIGHT REFUELING SYSTEM CONE | 2021 |
|
RU2762185C1 |
| PARACHUTE SKIRT OF CONE-SENSOR OF SUSPENSION FUEL IN-FLIGHT UNIT | 2021 |
|
RU2753777C1 |
| FUEL CONE-SENSOR FOR FILLING SET | 1980 |
|
RU1778983C |
| FUEL HOSE OF THE IN-FLIGHT REFUELING UNIT | 2020 |
|
RU2749470C1 |
| TANKER AEROPLANE | 1994 |
|
RU2100257C1 |
