AIRCRAFT ENGINE DRAINAGE SYSTEM Russian patent published in 2002 - IPC

Abstract RU 2190109 C2

FIELD: aircraft engines. SUBSTANCE: aircraft engine drainage system includes filter, check valve and drainage cavities. Drainage system is also provided with combined drainage pipe line and adjusting units and drainage valve for estimation of total leakage. Combined pipe line is connected with above-fuel portion of aircraft fuel tank. EFFECT: enhanced saving of fuel. 1 dwg

Similar patents RU2190109C2

Title Year Author Number
METHOD OF STORAGE OF AIRCRAFT ENGINE FILLED WITH FUEL IN AIRCRAFT 1999
  • Komarov V.M.
RU2198828C2
SLUSHING COMPOUND AND METHODS OF INTERNAL PRESERVATION AND DEPRESERVATION OF AIRCRAFT ENGINE WITH THIS SLUSHING COMPOUND 1999
  • Komarov V.M.
RU2201474C2
FUEL SYSTEM FOR GAS-TURBINE ENGINE 0
  • Komarov Vladimir Mikhajlovich
SU1793083A1
SEAPLANE FUEL TANK VENTING SYSTEM 1992
  • Vorob'Ev V.S.
RU2054361C1
FLYING VEHICLE FUEL TRANSFER SYSTEM 1994
  • Belov A.P.
  • Moiseev V.I.
  • Sjafukov A.Kh.
RU2081793C1
METHOD FOR TESTING AIRCRAFT SYSTEM OF NEUTRAL GAS FOR MINIMISATION OF FLAMMABLE FUEL VAPOURS GENERATION 2009
  • Koterev Vladislav Alekseevich
  • Frolkina Ljudmila Veniaminovna
RU2392197C1
HYPERSONIC AIRCRAFT AND ONBOARD COMBAT LASER 2008
  • Bolotin Nikolaj Borisovich
RU2380282C1
HYPERSONIC AIRPLANE WITH COMBAT AIR CRAFT LASER 2008
  • Bolotin Nikolaj Borisovich
RU2384473C2
SYSTEM AND METHOD FOR AIRCRAFTFUEL-TANK PRESSURISATION BY NEUTRAL GAS 2008
  • Trofimov Sergej Alekseevich
  • Stekol'Shchikova Marija Vladimirovna
  • Malyshev Valentin Vsevolodovich
  • Stepanenko Vladimir Aleksandrovich
  • Step Grigorij Khaimovich
  • Udut Vadim Nikolaevich
RU2376210C1
FUEL DRAINAGE SYSTEM OF DOUBLE-CONTOUR TURBOJET ENGINE 1983
  • Polushkin V.M.
  • Rubinov V.O.
  • Tsyrlin Eh.G.
  • Andrjukov N.A.
  • Nazarov V.G.
RU1132619C

RU 2 190 109 C2

Authors

Komarov V.M.

Dates

2002-09-27Published

2000-04-27Filed