SU1121887A1 - ACCESSORY POWER INSTALLATION OF AIRCRAFT - Google Patents

ACCESSORY POWER INSTALLATION OF AIRCRAFT

Info

Publication number
SU1121887A1
SU1121887A1 SU3618142/23A SU3618142A SU1121887A1 SU 1121887 A1 SU1121887 A1 SU 1121887A1 SU 3618142/23 A SU3618142/23 A SU 3618142/23A SU 3618142 A SU3618142 A SU 3618142A SU 1121887 A1 SU1121887 A1 SU 1121887A1
Authority
SU
USSR - Soviet Union
Prior art keywords
fixed
aircraft
fuselage
accessory power
power installation
Prior art date
Application number
SU3618142/23A
Other languages
Russian (ru)
Inventor
К.Б. Гузов
В.В. Зюскин
Г.В. Степанов
Original Assignee
К.Б. Гузов
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 К.Б. Гузов filed Critical К.Б. Гузов
Priority to SU3618142/23A priority Critical patent/SU1121887A1/en
Application granted granted Critical
Publication of SU1121887A1 publication Critical patent/SU1121887A1/en

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Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Вспомогательная силовая установка летательного аппарата, содержащая закрепленный в отсеке газотурбинный двигатель, воздухозаборный канал, жестко закрепленный на фюзеляже, шарнирно закрепленную напорную створку, отличающаяся тем, что, с целью повышения экономичности путем уменьшения потерь на входе в двигатель в наземных условиях, воздухозаборный канал выполнен разъемным, состоящим из двух частей - неподвижной, жестко закрепленной на фюзеляже, и подвижной, снабженной приводом и шарнирно соединенной с неподвижной частью.An auxiliary power unit of the aircraft, containing a gas turbine engine fixed in the compartment, an air intake channel rigidly fixed to the fuselage, a hinged pressure head flap, characterized in that, in order to improve efficiency by reducing losses at the engine inlet in ground conditions, the air intake channel is detachable consisting of two parts - a fixed, rigidly fixed on the fuselage, and a mobile, equipped with a drive and pivotally connected to the fixed part.

SU3618142/23A 1983-07-08 1983-07-08 ACCESSORY POWER INSTALLATION OF AIRCRAFT SU1121887A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU3618142/23A SU1121887A1 (en) 1983-07-08 1983-07-08 ACCESSORY POWER INSTALLATION OF AIRCRAFT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU3618142/23A SU1121887A1 (en) 1983-07-08 1983-07-08 ACCESSORY POWER INSTALLATION OF AIRCRAFT

Publications (1)

Publication Number Publication Date
SU1121887A1 true SU1121887A1 (en) 2004-12-20

Family

ID=60542176

Family Applications (1)

Application Number Title Priority Date Filing Date
SU3618142/23A SU1121887A1 (en) 1983-07-08 1983-07-08 ACCESSORY POWER INSTALLATION OF AIRCRAFT

Country Status (1)

Country Link
SU (1) SU1121887A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2646695C2 (en) * 2013-01-29 2018-03-06 Микротурбо System for feeding air to an auxiliary power unit in an aircraft

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2646695C2 (en) * 2013-01-29 2018-03-06 Микротурбо System for feeding air to an auxiliary power unit in an aircraft

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