SU1475257A1 - HEATED AIR RECEIVING GAS TURBINE ENGINE - Google Patents

HEATED AIR RECEIVING GAS TURBINE ENGINE

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Publication number
SU1475257A1
SU1475257A1 SU4217231/06A SU4217231A SU1475257A1 SU 1475257 A1 SU1475257 A1 SU 1475257A1 SU 4217231/06 A SU4217231/06 A SU 4217231/06A SU 4217231 A SU4217231 A SU 4217231A SU 1475257 A1 SU1475257 A1 SU 1475257A1
Authority
SU
USSR - Soviet Union
Prior art keywords
gas turbine
turbine engine
heated air
cavity
air receiving
Prior art date
Application number
SU4217231/06A
Other languages
Russian (ru)
Inventor
С.Г. Бондарев
М.Д. Бройдо
Б.В. Захаренко
Г.П. Панасюк
О.Д. Сарбучев
И.А. Сорокин
Original Assignee
С.Г. Бондарев
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 С.Г. Бондарев filed Critical С.Г. Бондарев
Priority to SU4217231/06A priority Critical patent/SU1475257A1/en
Application granted granted Critical
Publication of SU1475257A1 publication Critical patent/SU1475257A1/en

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Abstract

Обогреваемое воздухоприемное устройство газотурбинного двигателя, содержащее двустенный корпус, межстеночная полость которого подключена к источнику греющего газа, размещенный на входе в устройство завихритель с полыми лопатками, имеющими впускные отверстия и выпускные щели, сообщенные с входом двигателя, отличающееся тем, что, с целью повышения эффективности обогрева, в межстеночной полости установлена перегородка с образованием отсека, подключенного к полости лопаток через отверстия в последней и дополнительно к источнику нагретого воздуха, а межстеночная полость соединена с атмосферой.Heated air-intake device of a gas turbine engine, comprising a double-walled case, the inter-wall cavity of which is connected to a source of heating gas placed at the entrance to the device a swirler with hollow blades having inlets and exhaust slots communicated with the engine inlet, characterized in that, in order to increase efficiency heating, a partition is installed in the inter-wall cavity with the formation of a compartment connected to the cavity of the blades through the holes in the latter and heated in addition to the source of air and interwalled cavity is connected with the atmosphere.

SU4217231/06A 1987-03-30 1987-03-30 HEATED AIR RECEIVING GAS TURBINE ENGINE SU1475257A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4217231/06A SU1475257A1 (en) 1987-03-30 1987-03-30 HEATED AIR RECEIVING GAS TURBINE ENGINE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4217231/06A SU1475257A1 (en) 1987-03-30 1987-03-30 HEATED AIR RECEIVING GAS TURBINE ENGINE

Publications (1)

Publication Number Publication Date
SU1475257A1 true SU1475257A1 (en) 1999-07-27

Family

ID=60526603

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4217231/06A SU1475257A1 (en) 1987-03-30 1987-03-30 HEATED AIR RECEIVING GAS TURBINE ENGINE

Country Status (1)

Country Link
SU (1) SU1475257A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2480598C2 (en) * 2008-02-27 2013-04-27 Эрсель Air intake for aircraft nacelle

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2480598C2 (en) * 2008-02-27 2013-04-27 Эрсель Air intake for aircraft nacelle

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