FLYING VEHICLE FUEL SYSTEM Russian patent published in 1995 - IPC

Abstract SU 1621359 A1

FIELD: manufacture of aircraft. SUBSTANCE: vertical partition 5 is tight in upper portion and is provided with holes 12 in its lower portion; hole 11 is provided in upper point of transfer chamber 4; upper point of feed chamber 3 is connected with tank 1 by means of venting pipe line 10. EFFECT: enhanced reliability. 1 dwg

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SU 1 621 359 A1

Authors

Borisov D.G.

Sidorov A.K.

Krasinskij M.B.

Dates

1995-11-27—Published

1989-04-11—Filed