RU2015109986A - COMBINED AIR-REACTIVE ENGINE - Google Patents

COMBINED AIR-REACTIVE ENGINE Download PDF

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Publication number
RU2015109986A
RU2015109986A RU2015109986A RU2015109986A RU2015109986A RU 2015109986 A RU2015109986 A RU 2015109986A RU 2015109986 A RU2015109986 A RU 2015109986A RU 2015109986 A RU2015109986 A RU 2015109986A RU 2015109986 A RU2015109986 A RU 2015109986A
Authority
RU
Russia
Prior art keywords
engine
compressor
jet
gas turbine
combined air
Prior art date
Application number
RU2015109986A
Other languages
Russian (ru)
Other versions
RU2626278C2 (en
Inventor
Виктор Серафимович Бахирев
Original Assignee
Виктор Серафимович Бахирев
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Виктор Серафимович Бахирев filed Critical Виктор Серафимович Бахирев
Priority to RU2015109986A priority Critical patent/RU2626278C2/en
Publication of RU2015109986A publication Critical patent/RU2015109986A/en
Application granted granted Critical
Publication of RU2626278C2 publication Critical patent/RU2626278C2/en

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/16—Composite ram-jet/turbo-jet engines

Landscapes

  • Jet Pumps And Other Pumps (AREA)
  • Supercharger (AREA)

Abstract

Комбинированный авиационный двигатель, содержащий двухкаскадный газотурбинный двигатель с внутренним и внешним валами и двумя каскадами компрессора, основной камеры, к которой подведен топливный трубопровод от топливного насоса, турбину и реактивное сопло, отличающийся тем, что в предлагаемом воздушно-реактивном двигателе компрессор с механизмами, обеспечивающими его работу, вращает газотурбинный двигатель, а за ним расположены компрессорная и вокруг нее бескомпрессорная камеры сгорания, создающие реактивную тягу двигателя.A combined aircraft engine containing a two-stage gas turbine engine with internal and external shafts and two stages of a compressor, a main chamber, to which a fuel pipe from a fuel pump is connected, a turbine and a jet nozzle, characterized in that in the proposed air-jet engine there is a compressor with mechanisms providing its work is rotated by a gas turbine engine, and behind it are the compressor and around it uncompressed combustion chambers that create jet thrust of the engine.

Claims (1)

Комбинированный авиационный двигатель, содержащий двухкаскадный газотурбинный двигатель с внутренним и внешним валами и двумя каскадами компрессора, основной камеры, к которой подведен топливный трубопровод от топливного насоса, турбину и реактивное сопло, отличающийся тем, что в предлагаемом воздушно-реактивном двигателе компрессор с механизмами, обеспечивающими его работу, вращает газотурбинный двигатель, а за ним расположены компрессорная и вокруг нее бескомпрессорная камеры сгорания, создающие реактивную тягу двигателя. A combined aircraft engine containing a two-stage gas turbine engine with internal and external shafts and two stages of a compressor, a main chamber, to which a fuel pipe from a fuel pump is connected, a turbine and a jet nozzle, characterized in that in the proposed air-jet engine there is a compressor with mechanisms providing its work is rotated by a gas turbine engine, and behind it are the compressor and around it uncompressed combustion chambers that create jet thrust of the engine.
RU2015109986A 2015-03-20 2015-03-20 Hybrid air-breathing engine RU2626278C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2015109986A RU2626278C2 (en) 2015-03-20 2015-03-20 Hybrid air-breathing engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2015109986A RU2626278C2 (en) 2015-03-20 2015-03-20 Hybrid air-breathing engine

Publications (2)

Publication Number Publication Date
RU2015109986A true RU2015109986A (en) 2016-10-10
RU2626278C2 RU2626278C2 (en) 2017-07-25

Family

ID=57122252

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2015109986A RU2626278C2 (en) 2015-03-20 2015-03-20 Hybrid air-breathing engine

Country Status (1)

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RU (1) RU2626278C2 (en)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1747730A1 (en) * 1989-04-14 1992-07-15 Казанский Авиационный Институт Им.А.Н.Туполева Method and device for operation of hybrid air-jet engine
RU2125659C1 (en) * 1996-10-16 1999-01-27 Чвилев Виктор Андреевич Turboramjet engine
RU2166659C2 (en) * 1996-12-02 2001-05-10 Александр Евгеньевич Яшин Flying vehicle combination engine unit
RU2142058C1 (en) * 1997-11-18 1999-11-27 Ермишин Александр Викторович Detonation combustion pulse-jet engine
RU2162957C2 (en) * 1998-01-06 2001-02-10 Орловский государственный технический университет Aircraft gas-turbine engine
RU2278986C1 (en) * 2005-02-04 2006-06-27 Борис Федорович Кочетков Combination air-jet engine

Also Published As

Publication number Publication date
RU2626278C2 (en) 2017-07-25

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Legal Events

Date Code Title Description
FA92 Acknowledgement of application withdrawn (lack of supplementary materials submitted)

Effective date: 20161111

FZ9A Application not withdrawn (correction of the notice of withdrawal)

Effective date: 20161111

MM4A The patent is invalid due to non-payment of fees

Effective date: 20170930