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1. JP2016165950 - POWER GENERATION DEVICE FOR AIRCRAFT

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Office Japan
Application Number 2015046330
Application Date 09.03.2015
Publication Number 2016165950
Publication Date 15.09.2016
Grant Number 6343243
Grant Date 25.05.2018
Publication Kind B2
IPC
B64D 41/00
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
41Power installations for auxiliary purposes
F01D 15/10
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
DNON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
15Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
10Adaptations for driving, or combinations with, electric generators
F02C 7/00
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
7Features, component parts, details or accessories, not provided for in, or of interest apart from, groups F02C1/-F02C6/158; Air intakes for jet-propulsion plants
F02C 7/32
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
7Features, component parts, details or accessories, not provided for in, or of interest apart from, groups F02C1/-F02C6/158; Air intakes for jet-propulsion plants
32Arrangement, mounting, or driving, of auxiliaries
F02C 7/36
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
7Features, component parts, details or accessories, not provided for in, or of interest apart from, groups F02C1/-F02C6/158; Air intakes for jet-propulsion plants
36Power transmission between the different shafts of the gas-turbine plant, or between the gas-turbine plant and the power user
F16H 1/06
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
16ENGINEERING ELEMENTS OR UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
HGEARING
1Toothed gearings for conveying rotary motion
02without gears having orbital motion
04involving only two intermeshing members
06with parallel axes
CPC
B64D 41/00
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
41Power installations for auxiliary purposes
F02C 7/32
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
7Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
32Arrangement, mounting, or driving, of auxiliaries
F05D 2220/76
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
2220Application
70in combination with
76an electrical generator
F05D 2250/312
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
2250Geometry
30Arrangement of components
31according to the direction of their main axis or their axis of rotation
312the axes being parallel to each other
F05D 2250/36
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
2250Geometry
30Arrangement of components
36in inner-outer relationship, e.g. shaft-bearing arrangements
F05D 2260/39
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
2260Function
30Retaining components in desired mutual position
39by a V-shaped ring to join the flanges of two cylindrical sections, e.g. casing sections of a turbocharger
Applicants KAWASAKI HEAVY IND LTD
川崎重工業株式会社
Inventors TANAKA KENICHIRO
田中　謙一郎
IMAI HIDEYUKI
今井　秀幸
FUJII ISAO
藤井　勲
GOI TATSUHIKO
五井　龍彦
淵脇　彰悟
Agents 特許業務法人　有古特許事務所
Title
(EN) POWER GENERATION DEVICE FOR AIRCRAFT
(JA) 航空機用発電装置
Abstract
(EN)

PROBLEM TO BE SOLVED: To provide a power generation device for an aircraft, that is compact and is small in overhang moment.

SOLUTION: A power generation device 11 for an aircraft comprises an input shaft 14 to which driving force of an engine is transmitted, a transmission 15 provided parallel to the input shaft, a power generator 16 provided parallel to the input shaft and the transmission and driven by output of the transmission, a power transmission mechanism 17 arranged on one axial end side of the input shaft and transmitting output from the transmission to the power generator, and a casing 18 having a mount part 18a at the one axial end side 14a of the input shaft. The transmission has an input part provided on the other axial end side 14b of the input shaft and inputted with rotation drive force from the input shaft, and an output part provided on the one axial end side of the input shaft and outputting the speed-changed rotation drive force to the power transmission mechanism. The power transmission mechanism has an internal space S. The input shaft is inserted in the internal space.

SELECTED DRAWING: Figure 3

COPYRIGHT: (C)2016,JPO&INPIT

(JA)

【課題】コンパクト且つオーバーハングモーメントの小さい航空機用発電装置を提供する。
【解決手段】航空機用発電装置１１は、エンジンの駆動力が伝達される入力軸１４と、前記入力軸と並設された変速機１５と、前記入力軸及び前記変速機と並設されて前記変速機の出力により駆動される発電機１６と、前記入力軸の軸方向一端側に配置され、前記変速機からの出力を前記発電機に伝達する動力伝動機構１７と、前記入力軸の軸方向一端側１４ａに取付部１８ａを有するケーシング１８と、を備える。前記変速機は、前記入力軸の軸方向他端側１４ｂに設けられて前記入力軸からの回転駆動力が入力される入力部と、前記入力軸の軸方向一端側に設けられて変速された回転駆動力を前記動力伝動機構に出力する出力部とを有する。前記動力伝動機構は、内部空間Ｓを有する。前記内部空間には前記入力軸が挿通される。
【選択図】図３
Also published as
CN107406149
EP3269648
US20180237154
WO/2016/143331
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