RU97114819A - AIRCRAFT POWER PLANT WITH ADDITIONAL GAS-TURBINE ENGINE FOR AIR STARTING SYSTEM AND VENTILATION AND AIR CONDITIONING SYSTEM - Google Patents

AIRCRAFT POWER PLANT WITH ADDITIONAL GAS-TURBINE ENGINE FOR AIR STARTING SYSTEM AND VENTILATION AND AIR CONDITIONING SYSTEM

Info

Publication number
RU97114819A
RU97114819A RU97114819/06A RU97114819A RU97114819A RU 97114819 A RU97114819 A RU 97114819A RU 97114819/06 A RU97114819/06 A RU 97114819/06A RU 97114819 A RU97114819 A RU 97114819A RU 97114819 A RU97114819 A RU 97114819A
Authority
RU
Russia
Prior art keywords
air
turbine engine
ventilation
power plant
aircraft power
Prior art date
Application number
RU97114819/06A
Other languages
Russian (ru)
Other versions
RU2133358C1 (en
Inventor
В.К. Кобченко
Б.И. Кузнецов
Original Assignee
Акционерное общество открытого типа Авиамоторный научно-технический комплекс "Союз"
Filing date
Publication date
Application filed by Акционерное общество открытого типа Авиамоторный научно-технический комплекс "Союз" filed Critical Акционерное общество открытого типа Авиамоторный научно-технический комплекс "Союз"
Priority to RU97114819/06A priority Critical patent/RU2133358C1/en
Priority claimed from RU97114819/06A external-priority patent/RU2133358C1/en
Publication of RU97114819A publication Critical patent/RU97114819A/en
Application granted granted Critical
Publication of RU2133358C1 publication Critical patent/RU2133358C1/en

Links

Claims (2)

1. Авиационная силовая установка с дополнительным газотурбинным двигателем для воздушной пусковой системы и системы вентиляции и кондиционирования, содержащая, по крайней мере, один основной маршевый газотурбинный двигатель, подключенный посредством трубопроводов с клапанами к воздушной пусковой системе и системе вентиляции и кондиционирования, отличающаяся тем, что она снабжена дополнительной воздушной турбиной, механически связанной с валом дополнительного газотурбинного двигателя и соединенной с воздушной пусковой системой трубопроводом с двухпозиционным клапаном и дросселирующим устройством между этим клапаном и дополнительной воздушной турбиной.1. An aircraft power plant with an additional gas turbine engine for an air starting system and a ventilation and air conditioning system, comprising at least one main marching gas turbine engine connected via pipelines with valves to the air starting system and a ventilation and air conditioning system, characterized in that it is equipped with an additional air turbine mechanically connected to the shaft of the additional gas turbine engine and connected to the air starting system a piping with a two-position valve and a throttling device between this valve and an additional air turbine. 2. Авиационная силовая установка по п. 1, отличающаяся тем, что упомянутая дополнительная воздушная турбина выполнена в виде рабочего радиального колеса с активными лопатками и радиального соплового аппарата. 2. The aircraft power plant according to claim 1, characterized in that the said additional air turbine is made in the form of a working radial wheel with active blades and a radial nozzle apparatus.
RU97114819/06A 1997-09-02 1997-09-02 Aircraft power plant with additional gas-turbine engine for air starting system and ventilation and air-conditioning system RU2133358C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU97114819/06A RU2133358C1 (en) 1997-09-02 1997-09-02 Aircraft power plant with additional gas-turbine engine for air starting system and ventilation and air-conditioning system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU97114819/06A RU2133358C1 (en) 1997-09-02 1997-09-02 Aircraft power plant with additional gas-turbine engine for air starting system and ventilation and air-conditioning system

Publications (2)

Publication Number Publication Date
RU97114819A true RU97114819A (en) 1999-06-27
RU2133358C1 RU2133358C1 (en) 1999-07-20

Family

ID=20196871

Family Applications (1)

Application Number Title Priority Date Filing Date
RU97114819/06A RU2133358C1 (en) 1997-09-02 1997-09-02 Aircraft power plant with additional gas-turbine engine for air starting system and ventilation and air-conditioning system

Country Status (1)

Country Link
RU (1) RU2133358C1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2689927C1 (en) * 2018-08-15 2019-05-29 Виктор Израилевич Думов Aircraft air conditioning system compressed air producer

Similar Documents

Publication Publication Date Title
US6012279A (en) Gas turbine engine with water injection
US5373707A (en) Air conditioning system
US5119624A (en) Gas turbine engine power unit
WO2002042623A3 (en) Fan-stator interaction tone reduction
CA2148059A1 (en) Steam cooling of gas turbine with backup air cooling
EP0586619A1 (en) Turbine bypass working fluid admission.
CA2358593A1 (en) Compressor bleeding using an uninterrupted annular slot
AU6563298A (en) Method and apparatus for enhancing gas turbo machinery flow
US6289665B1 (en) Aircraft air conditioner energy recovery method
CA2220172A1 (en) Control system for a ducted fan gas turbine engine
US8083467B2 (en) Apparatus and method for controlling a rotary machine using pressurized gas
WO2000020739A3 (en) Gas turbine engine
RU97114819A (en) AIRCRAFT POWER PLANT WITH ADDITIONAL GAS-TURBINE ENGINE FOR AIR STARTING SYSTEM AND VENTILATION AND AIR CONDITIONING SYSTEM
GB2063366A (en) Turbocharger and adaptions thereof
DE59712998D1 (en) Gas turbine arrangement for air conditioning
ATE388311T1 (en) CHARGED ENGINE WITH AT LEAST TWO STAGES OF TURBOCHARGER
RU2000131795A (en) POWER INSTALLATION OF THE AIRCRAFT
RU97111663A (en) AIRCRAFT POWER PLANT WITH ADDITIONAL GAS-TURBINE ENGINE FOR AIR STARTING SYSTEM AND AIR CONDITIONING SYSTEM
CA2199875A1 (en) Combined bleed valve and annular diffuser for gas turbine inter compressor duct
RU97121241A (en) METHOD OF WORK OF GAS-TURBINE INSTALLATION
RU2133358C1 (en) Aircraft power plant with additional gas-turbine engine for air starting system and ventilation and air-conditioning system
RU2123126C1 (en) Aircraft power plant with additional gas-turbine engine for air starting system and air conditioning system
RU96102064A (en) METHOD FOR WORKING HEAT TURBINE TURBINE ON HEAT GRAPHICS
RU2113631C1 (en) Method and device for operating diffuser
JPS6137767Y2 (en)