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RU2014100575A - AIR REACTIVE ENGINE - Google Patents

AIR REACTIVE ENGINE Download PDF

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Publication number
RU2014100575A
RU2014100575A RU2014100575/06A RU2014100575A RU2014100575A RU 2014100575 A RU2014100575 A RU 2014100575A RU 2014100575/06 A RU2014100575/06 A RU 2014100575/06A RU 2014100575 A RU2014100575 A RU 2014100575A RU 2014100575 A RU2014100575 A RU 2014100575A
Authority
RU
Russia
Prior art keywords
air
engine
gas turbine
compressor
jet
Prior art date
Application number
RU2014100575/06A
Other languages
Russian (ru)
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 RU2014100575/06A priority Critical patent/RU2014100575A/en
Publication of RU2014100575A publication Critical patent/RU2014100575A/en

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  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Воздушно-реактивный дизельный двигатель с приводом компрессора, предусматривает его работу без участия газовой турбины и потери энергии на ее вращение, отличающийся тем, что в предлагаемом воздушно-реактивном двигателе, компрессор вращает пульсирующий газотурбинный двигатель, установленный между компрессором и камерой сгорания, что способствует использовать напорную линию воздуха для работы пульсирующего газотурбинного двигателя, а отработавшие газовые продукты удалять по выхлопным патрубкам в тяговую камеру сгорания, рабочая энергия которой свободно истекает, создавая реактивную тягу двигателя.An air-jet diesel engine with a compressor drive provides for its operation without the participation of a gas turbine and loss of energy for its rotation, characterized in that in the proposed air-jet engine, the compressor rotates a pulsating gas turbine engine installed between the compressor and the combustion chamber, which contributes to the use of the pressure line of air for the operation of a pulsating gas turbine engine, and the exhaust gas products to be removed through the exhaust pipes into the traction combustion chamber, working a Gia which expires freely, creating a jet engine thrust.

Claims (1)

Воздушно-реактивный дизельный двигатель с приводом компрессора, предусматривает его работу без участия газовой турбины и потери энергии на ее вращение, отличающийся тем, что в предлагаемом воздушно-реактивном двигателе, компрессор вращает пульсирующий газотурбинный двигатель, установленный между компрессором и камерой сгорания, что способствует использовать напорную линию воздуха для работы пульсирующего газотурбинного двигателя, а отработавшие газовые продукты удалять по выхлопным патрубкам в тяговую камеру сгорания, рабочая энергия которой свободно истекает, создавая реактивную тягу двигателя. An air-jet diesel engine with a compressor drive provides for its operation without the participation of a gas turbine and loss of energy for its rotation, characterized in that in the proposed air-jet engine, the compressor rotates a pulsating gas turbine engine installed between the compressor and the combustion chamber, which contributes to the use of the pressure line of air for the operation of a pulsating gas turbine engine, and the exhaust gas products to be removed through the exhaust pipes into the traction combustion chamber, working a Gia which expires freely, creating a jet engine thrust.
RU2014100575/06A 2014-01-09 2014-01-09 AIR REACTIVE ENGINE RU2014100575A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2014100575/06A RU2014100575A (en) 2014-01-09 2014-01-09 AIR REACTIVE ENGINE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2014100575/06A RU2014100575A (en) 2014-01-09 2014-01-09 AIR REACTIVE ENGINE

Publications (1)

Publication Number Publication Date
RU2014100575A true RU2014100575A (en) 2015-07-20

Family

ID=53611367

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2014100575/06A RU2014100575A (en) 2014-01-09 2014-01-09 AIR REACTIVE ENGINE

Country Status (1)

Country Link
RU (1) RU2014100575A (en)

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Legal Events

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

Effective date: 20151124