AIRCRAFT GRAVITY LAUNCHER Russian patent published in 2014 - IPC B64F1/04 

Abstract RU 2537079 C2

FIELD: aircraft engineering.

SUBSTANCE: proposed device comprises swing including two supports, carriage and cables for carriage pendulum suspension, elevator to integrate said carriage and aircraft in single swinging unit and the drive of the latter. Note here that said elevator comprises winches with drums arranged at supports. Swinging unit drive comprises propulsor with aero- or gas-dynamic thrust and is fitted at swinging unit. Note also that said cables are secured at said drums to be wound thereon and secured at said carriage for at least one cable to be uncoupled therefrom extending from one support to another one.

EFFECT: simplified launching and landing device.

6 cl, 4 dwg

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RU 2 537 079 C2

Authors

Rednikov Valerij Vasil'Evich

Dates

2014-12-27Published

2013-12-20Filed