FIELD: aviation.
SUBSTANCE: invention relates to aerodrome equipment. Proposed method comprises starting device filling, aircraft and starting device mechanical connection. Horizontal component of mechanical loads is transmitted from launching device to aircraft so that total transmitted force coincides with aircraft motion vector. Vertical component of mechanical loads from aircraft to runway through launching device is transmitted to a lesser extent. Providing for movement of bundle aircraft - launching device by conversion of chemical energy stored in fuel, using aircraft propulsion device and accelerating jet propulsion unit of starting device in kinetic energy of translational movement to kinetic energy of value, which allows aircraft to take off due to traction of own propulsion plant. Aircraft and starting device mechanical disconnection is performed. Braking of starting device is ensured by reverse thrust of accelerating jet propulsion unit.
EFFECT: invention is aimed at improvement of energy-mass efficiency of take-off.
1 cl
Title | Year | Author | Number |
---|---|---|---|
MOBILE LAUNCHER UNIT | 2020 |
|
RU2739477C1 |
METHOD OF LAUNCHING FLYING VEHICLE WITH THE AID OF LAUNCHING TROLLEY WITH LIQUID-PROPELLANT ENGINE PLANT | 1991 |
|
RU2046071C1 |
METHOD OF LAUNCHING FLYING VEHICLE WITH THE AID OF LAUNCHING TROLLEY PROVIDED WITH ELECTROMAGNETIC DRIVE | 1991 |
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RU2238883C2 |
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ACCELERATING DEVICE FOR TAKEOFF OF SHIPBORNE AIRCRAFT | 2019 |
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RU2712407C1 |
METHOD AND DEVICE FOR LAUNCHING FLYING VEHICLE | 1992 |
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RU2005673C1 |
VERTICAL TAKEOFF AND VERTICAL SOFT LANDING FLYING VEHICLE WITH LESSER-THAN-WEIGHT THRUST | 1998 |
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RU2152892C1 |
Authors
Dates
2019-05-21—Published
2017-07-25—Filed