AIRCRAFT Russian patent published in 2016 - IPC B64G1/40 

FIELD: space.

SUBSTANCE: invention relates to aerospace engineering. Aircraft (A/C) comprises rigidly connected housing and cylinder, located in cylinder piston with a lobe, as well as two rigidly connected to the housing starting jet engines and placed in the end of the cylinder two shock-absorbing safety stops. Said airframe has recess to accommodated damper interacting with piston. A/C comprises solenoid power supply and cylindrical solenoid located inside the housing opening, rigidly connected to the housing. Solenoid power supply is rigidly connected to the housing and has the first and the second outputs, respectively connected to the first and second inputs of the cylindrical solenoid. Power supply unit supplies electric pulses for pulling piston lobe inside of solenoid before damping and pushing of a piston and the housing in opposite directions after damping. A/C comprises control unit with possibility of metering of fuel dispensing, rigidly connected to the housing and having hydraulic connection with jet engines.

EFFECT: technical result is increased lifting capacity without loss of the required acceleration of A/C.

1 cl, 1 dwg