RU2011132566A - CLOSED AIRCRAFT GAS-TURBO-HYDRAULIC ENGINE - Google Patents

CLOSED AIRCRAFT GAS-TURBO-HYDRAULIC ENGINE Download PDF

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Publication number
RU2011132566A
RU2011132566A RU2011132566/06A RU2011132566A RU2011132566A RU 2011132566 A RU2011132566 A RU 2011132566A RU 2011132566/06 A RU2011132566/06 A RU 2011132566/06A RU 2011132566 A RU2011132566 A RU 2011132566A RU 2011132566 A RU2011132566 A RU 2011132566A
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RU
Russia
Prior art keywords
turbo
hydraulic engine
pressure pump
closed
water heater
Prior art date
Application number
RU2011132566/06A
Other languages
Russian (ru)
Inventor
Николай Павлович Иванников
Original Assignee
Николай Павлович Иванников
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Publication date
Application filed by Николай Павлович Иванников filed Critical Николай Павлович Иванников
Priority to RU2011132566/06A priority Critical patent/RU2011132566A/en
Publication of RU2011132566A publication Critical patent/RU2011132566A/en

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Abstract

Авиационный газотурбогидравлический двигатель замкнутого цикла, содержащий компрессор, камеру сгорания, газовую турбину, насос высокого давления, подогреватель воды, гидротурбины, воздушные винты, теплосъемник, реактивное сопло, магистраль рециркуляции, магистраль хим. очищенной воды, отличающийся тем, что насос высокого давления, подогреватель воды, гидротурбины образуют замкнутый цикл.Aircraft closed-circuit gas turbo-hydraulic engine containing a compressor, a combustion chamber, a gas turbine, a high pressure pump, a water heater, hydraulic turbines, propellers, a heat sink, a jet nozzle, a recirculation line, and a chemical line. purified water, characterized in that the high-pressure pump, water heater, turbines form a closed cycle.

Claims (1)

Авиационный газотурбогидравлический двигатель замкнутого цикла, содержащий компрессор, камеру сгорания, газовую турбину, насос высокого давления, подогреватель воды, гидротурбины, воздушные винты, теплосъемник, реактивное сопло, магистраль рециркуляции, магистраль хим. очищенной воды, отличающийся тем, что насос высокого давления, подогреватель воды, гидротурбины образуют замкнутый цикл. Aircraft closed-circuit gas turbo-hydraulic engine containing a compressor, a combustion chamber, a gas turbine, a high pressure pump, a water heater, hydraulic turbines, propellers, a heat sink, a jet nozzle, a recirculation line, and a chemical line. purified water, characterized in that the high-pressure pump, water heater, turbines form a closed cycle.
RU2011132566/06A 2011-08-02 2011-08-02 CLOSED AIRCRAFT GAS-TURBO-HYDRAULIC ENGINE RU2011132566A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2011132566/06A RU2011132566A (en) 2011-08-02 2011-08-02 CLOSED AIRCRAFT GAS-TURBO-HYDRAULIC ENGINE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2011132566/06A RU2011132566A (en) 2011-08-02 2011-08-02 CLOSED AIRCRAFT GAS-TURBO-HYDRAULIC ENGINE

Publications (1)

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RU2011132566A true RU2011132566A (en) 2013-02-10

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Family Applications (1)

Application Number Title Priority Date Filing Date
RU2011132566/06A RU2011132566A (en) 2011-08-02 2011-08-02 CLOSED AIRCRAFT GAS-TURBO-HYDRAULIC ENGINE

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RU (1) RU2011132566A (en)

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Legal Events

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

Effective date: 20130516