METHOD OF WORK OF AIR-JET ENGINE AND DEVICE FOR ITS IMPLEMENTATION (OPTIONS) Russian patent published in 2018 - IPC F02K7/20 

Abstract RU 2654292 C2

FIELD: engines.

SUBSTANCE: invention relates to engine building, in particular to the organization of the cycle processes and systems for the preparation and supply of fuel and air to the combustion chamber of an air-jet engine as an oxidant by means of a shock wave generator. Pulsating detonation combustion engine with an inlet diffuser and a nozzle contains two combustion chambers. One of the combustion chambers works as a generator of detonation shock waves, whose impulses with the help of a detonation tube deliver air to the combustion chamber in which combustion of the fuel supplied into it occurs at a pressure close to the applied pulses of the shock wave generator, with further acceleration of the flow of total combustion products in the nozzle and the creation of engine thrust. When the shock wave generator is operating, the energy of the combustion products under high pressure at the end of cycle at the highest dead point is divided into two parts. One of the parts is fed into the detonation tube, and the second part is spent on compressing the newly supplied combustible mixture. In this case, two pistons with counter motion are operated, one of which is associated with gas storages of energy and controls the formation of impulses of shock waves, and the second, with a crank-and-rod mechanism and a flywheel, serves to compress a new portion of the fuel mixture.

EFFECT: invention is aimed at increasing the effectiveness and efficiency of the engine.

20 cl, 14 dwg

Similar patents RU2654292C2

Title Year Author Number
INTERMITTENT DETONATION ENGINE 2010
  • Petrienko Viktor Grigor'Evich
RU2435059C1
INTERMITTENT DETONATION ENGINE 2012
  • Petrienko Viktor Grigor'Evich
RU2490498C1
METHOD FOR OPERATION OF DETONATION TWO-STROKE INTERNAL COMBUSTION ENGINE (VERSION) 2013
  • Popovich Vladimir Andrianovich
RU2579287C2
METHOD OF AIR JET ENGINE OPERATION WITH THRUST MODULES OF PULSATION-DETONATION COMBUSTION AND DEVICE TO THIS END 2008
  • Lebedenko Igor' Sergeevich
  • Lebedenko Jurij Igorevich
  • Lebedenko Viktor Igorevich
RU2375601C2
DYNAMIC SUPPORT CRAFT 2001
  • Artamonov A.S.
RU2205119C2
VTOL AIRCRAFT 2014
  • Artamonov Aleksandr Sergeevich
  • Artamonov Evgenij Aleksandrovich
RU2546385C1
COMPLEX FOR REACTIVE FLIGHT 2008
  • Artamonov Aleksandr Sergeevich
  • Artamonov Evgenij Aleksandrovich
RU2387582C2
CHAMBER FOR PULS DETONATION ENGINE 1994
  • Porshnev V.A.
  • Fedorets N.V.
  • Sorokin V.N.
  • Ivanov S.S.
  • Kutajtsev V.V.
RU2084675C1
DIRECT FLOW TURBORETACTIVE DETONATION ENGINE (DFTDE) 2016
  • Kozhevnikov Dmitrij Dmitrievich
RU2638239C1
JET ENGINE 1997
  • Artamonov A.S.
RU2157907C2

RU 2 654 292 C2

Authors

Popovich Vladimir Andrianovich

Dates

2018-05-17Published

2016-03-30Filed