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1. CN102272477 - Aircraft turbine engine and use of such a turbine engine

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Office China
Application Number 201080004111.X
Application Date 05.01.2010
Publication Number 102272477
Publication Date 07.12.2011
Grant Number 102272477
Grant Date 05.03.2014
Publication Kind B
IPC
F MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
02
COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
C
GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
6
Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
20
Adaptations of gas-turbine plants for driving vehicles
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
D
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS
27
Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
26
Aircraft characterised by construction of power-plant mounting
F02C 6/20
B64D 27/26
CPC
F02K 3/06
B64D 27/16
B64D 29/06
B64D 33/02
B64D 2033/0286
F02C 3/113
Applicants 空中客车运营简化股份公司
Inventors J.H.马尔什
Agents 中国专利代理(香港)有限公司 72001
Priority Data 0900032 07.01.2009 FR
Title
(EN) Aircraft turbine engine and use of such a turbine engine
(ZH) 飞行器涡轮发动机及该涡轮发动机的用途
Abstract
(EN)
The invention relates to an aircraft turbine engine and to the use of such a turbine engine. According to the invention, the turbine engine (1a) comprises a means for shifting the axis (la-la) of the blower (9a) transverse to the axis (La-La) of the hot flow generator (4a).

(ZH)

本发明涉及一种飞行器涡轮发动机及该涡轮发动机的用途。根据本发明,涡轮发动机(1a)包括能够使鼓风机(9a)的轴线(la-la)在横向于热气流发生器(4a)的轴线(La-La)的方向上发生偏移的装置。