SUPERSONIC AIRCRAFT STREAMLINING CONTROL METHOD Russian patent published in 2017 - IPC B64C19/00 H05B6/10 

Abstract RU 2621195 C1

FIELD: aviation.

SUBSTANCE: streamlining control is based on changing the direction of the incoming airflow from the counter to the radial outflow relative to the aircraft (LA) using a heated, gas-permeable porous insert on the aircraft front end. The heating of the gas-permeable porous insert is carried out by means of electric induction heating.

EFFECT: simplification of the system of influencing the flow and increasing the speed of streamlining control.

1 dwg

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RU 2 621 195 C1

Authors

Mironov Sergej Grigorevich

Tsyryulnikov Ivan Sergeevich

Dates

2017-06-01Published

2015-12-16Filed