RU98118382A - MULTI-STAGE AXIAL COMPRESSOR OF THE AIRCRAFT ENGINE - Google Patents

MULTI-STAGE AXIAL COMPRESSOR OF THE AIRCRAFT ENGINE

Info

Publication number
RU98118382A
RU98118382A RU98118382/06A RU98118382A RU98118382A RU 98118382 A RU98118382 A RU 98118382A RU 98118382/06 A RU98118382/06 A RU 98118382/06A RU 98118382 A RU98118382 A RU 98118382A RU 98118382 A RU98118382 A RU 98118382A
Authority
RU
Russia
Prior art keywords
aircraft engine
axial compressor
stage axial
compressor
stages
Prior art date
Application number
RU98118382/06A
Other languages
Russian (ru)
Other versions
RU2165547C2 (en
Inventor
В.И. Белоус
Original Assignee
В.И. Белоус
Filing date
Publication date
Application filed by В.И. Белоус filed Critical В.И. Белоус
Publication of RU98118382A publication Critical patent/RU98118382A/en
Application granted granted Critical
Publication of RU2165547C2 publication Critical patent/RU2165547C2/en

Links

Claims (3)

1. Многоступенчатый осевой компрессор авиационного двигателя, содержащий две или более установленные последовательно ступени, отличающийся тем, что компрессор снабжен средством для отключения части ступеней.1. A multistage axial compressor of an aircraft engine, comprising two or more stages installed in series, characterized in that the compressor is equipped with means for shutting off part of the stages. 2. Компрессор по п. 1, отличающийся тем, что снабжен средством для отключения одной или более первых ступеней. 2. The compressor according to claim 1, characterized in that it is provided with means for disabling one or more of the first stages. 3. Компрессор по п. 1, или по пп.1-2, отличающийся тем, что снабжен средством для отключения одной или более последних ступеней. 3. The compressor according to claim 1, or according to claims 1 to 2, characterized in that it is equipped with means for shutting off one or more of the last stages.
RU98118382/06A 1998-03-17 1998-10-08 Aircraft engine multi-stage axial-flow compressor RU2165547C2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
BY19980250 1998-03-17
BY19980250 1998-03-17

Publications (2)

Publication Number Publication Date
RU98118382A true RU98118382A (en) 2000-09-10
RU2165547C2 RU2165547C2 (en) 2001-04-20

Family

ID=4083719

Family Applications (1)

Application Number Title Priority Date Filing Date
RU98118382/06A RU2165547C2 (en) 1998-03-17 1998-10-08 Aircraft engine multi-stage axial-flow compressor

Country Status (4)

Country Link
AU (1) AU2706699A (en)
RU (1) RU2165547C2 (en)
UA (1) UA40584C2 (en)
WO (1) WO1999047815A1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013109159A1 (en) * 2012-01-19 2013-07-25 Panchenko Vladimir Mitrofanovich Rotary screw engine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1389347A (en) * 1972-05-25 1975-04-03 Rolls Royce Gas turbine power plant
GB1415679A (en) * 1972-11-17 1975-11-26 Rolls Royce Gas turbine engine powerplant
US4587803A (en) * 1983-08-15 1986-05-13 Rolls-Royce Inc. Valve for diverting fluid flows in turbomachines
SU1394790A1 (en) * 1986-06-06 1996-03-10 В.П. Абруков Method of control of gas-turbine engine multi-stage compressor

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