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1. (WO2017094823) ELECTRICALLY POWERED TAXIING SYSTEM FOR AIRCRAFT AND METHOD FOR CONTROLLING SAID SYSTEM
Latest bibliographic data on file with the International Bureau

Pub. No.: WO/2017/094823 International Application No.: PCT/JP2016/085687
Publication Date: 08.06.2017 International Filing Date: 01.12.2016
IPC:
B64C 25/36 (2006.01) ,B60T 1/16 (2006.01) ,B64C 25/42 (2006.01) ,B64D 27/24 (2006.01) ,B64D 41/00 (2006.01) ,H02P 3/18 (2006.01) ,B60T 8/17 (2006.01)
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
25
Alighting gear
32
characterised by elements which contact the ground or similar surface
34
wheeled type, e.g. multi-wheeled bogies
36
Arrangements or adaptations of wheels, tyres, or axles in general
B PERFORMING OPERATIONS; TRANSPORTING
60
VEHICLES IN GENERAL
T
VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
1
Arrangements of braking elements, i.e. of those parts where braking effect occurs
12
acting otherwise than by retarding wheels, e.g. jet- action
16
by increasing air resistance, e.g. flaps
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
25
Alighting gear
32
characterised by elements which contact the ground or similar surface
42
Arrangement or adaptation of brakes
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
02
Aircraft characterised by the type or position of power plant
24
using steam, electricity, or spring force
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
41
Power installations for auxiliary purposes
H ELECTRICITY
02
GENERATION, CONVERSION, OR DISTRIBUTION OF ELECTRIC POWER
P
CONTROL OR REGULATION OF ELECTRIC MOTORS, GENERATORS, OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS OR REACTORS OR CHOKE COILS
3
Arrangements for stopping or slowing electric motors, generators, or dynamo-electric converters
06
for stopping or slowing an individual dynamo-electric motor or dynamo-electric converter
18
for stopping or slowing an ac motor
B PERFORMING OPERATIONS; TRANSPORTING
60
VEHICLES IN GENERAL
T
VEHICLE BRAKE CONTROL SYSTEMS OR PARTS THEREOF; BRAKE CONTROL SYSTEMS OR PARTS THEREOF, IN GENERAL; ARRANGEMENT OF BRAKING ELEMENTS ON VEHICLES IN GENERAL; PORTABLE DEVICES FOR PREVENTING UNWANTED MOVEMENT OF VEHICLES; VEHICLE MODIFICATIONS TO FACILITATE COOLING OF BRAKES
8
Arrangements for adjusting wheel-braking force to meet varying vehicular or ground-surface conditions, e.g. limiting or varying distribution of braking force
17
Using electrical or electronic regulation means to control braking
Applicants:
株式会社IHI IHI CORPORATION [JP/JP]; 東京都江東区豊洲三丁目1番1号 1-1, Toyosu 3-chome, Koto-ku, Tokyo 1358710, JP
Inventors:
森岡 典子 MORIOKA Noriko; JP
垣内 大紀 KAKIUCHI Daiki; JP
大依 仁 OYORI Hitoshi; JP
朝倉 博幸 ASAKURA Hiroyuki; JP
Agent:
三好 秀和 MIYOSHI Hidekazu; JP
高橋 俊一 TAKAHASHI Shunichi; JP
伊藤 正和 ITO Masakazu; JP
高松 俊雄 TAKAMATSU Toshio; JP
Priority Data:
2015-23553002.12.2015JP
Title (EN) ELECTRICALLY POWERED TAXIING SYSTEM FOR AIRCRAFT AND METHOD FOR CONTROLLING SAID SYSTEM
(FR) SYSTÈME DE ROULAGE ÉLECTRIQUE POUR AÉRONEF ET PROCÉDÉ DE COMMANDE DUDIT SYSTÈME
(JA) 航空機の電動タキシングシステム及びその制御方法
Abstract:
(EN) An electrically powered taxiing system for an aircraft (1), said system being provided with: wheels (5a, 7a) of the aircraft (1); taxiing motors (5b, 7b) that, when the aircraft (1) lands, apply a braking force to the wheels (5a, 7a) on being turned with the wheels (5a, 7a) and generate regenerative power corresponding to the braking force, and that, when the aircraft (1) is taxiing, cause the wheels (5a, 7a) to turn; and a power supply control unit (27) for feeding the regenerative power to electrically powered elements (9b, 11b, 13b, 15b, 29a, 31a) of the aircraft (1), which are driven for landing of the aircraft (1) or for performing a second takeoff in an aborted landing.
(FR) L'invention concerne un système de roulage électrique destiné à un aéronef (1), ledit système comprenant : les roues (5a, 7a) de l'aéronef (1) ; des moteurs (5b, 7b) de roulage qui, lorsque l'aéronef (1) atterrit, appliquent une force de freinage sur les roues (5a, 7a) pendant qu'ils tournent avec les roues (5a, 7a) et générent de l'énergie de récupération correspondant à la force de freinage, et qui, lorsque l'aéronef (1) roule, entraînent les roues (5a, 7a) en rotation ; et une unité de commande (27) d'alimentation, qui fournit l'énergie de récupération (27) à des éléments (9b, 11b, 13b, 15b, 29a, 31a) alimentés électriquement de l'aéronef (1), lesquels sont entraînés en vue de l'atterrissage de l'aéronef (1), ou de la mise en oeuvre d'un deuxième décollage lors d'un atterrissage interrompu.
(JA) 航空機(1)の車輪(5a,7a)と、航空機(1)の着陸時に車輪(5a,7a)と共に回転されて車輪(5a,7a)に制動力を付与すると共に該制動力に応じた回生電力を発生し、航空機(1)のタキシング時に車輪(5a,7a)を回転させるタキシング用モータ(5b,7b)と、回生電力を、航空機(1)の着陸又は着陸を中止して行われる再離陸のために駆動される航空機(1)の電動要素(9b,11b,13b,15b,29a,31a)に供給する電源制御ユニット(27)と、を備える航空機(1)の電動タキシングシステム。
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Designated States: AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, BN, BR, BW, BY, BZ, CA, CH, CL, CN, CO, CR, CU, CZ, DE, DJ, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IR, IS, KE, KG, KN, KP, KR, KW, KZ, LA, LC, LK, LR, LS, LU, LY, MA, MD, ME, MG, MK, MN, MW, MX, MY, MZ, NA, NG, NI, NO, NZ, OM, PA, PE, PG, PH, PL, PT, QA, RO, RS, RU, RW, SA, SC, SD, SE, SG, SK, SL, SM, ST, SV, SY, TH, TJ, TM, TN, TR, TT, TZ, UA, UG, US, UZ, VC, VN, ZA, ZM, ZW
African Regional Intellectual Property Organization (ARIPO) (BW, GH, GM, KE, LR, LS, MW, MZ, NA, RW, SD, SL, ST, SZ, TZ, UG, ZM, ZW)
Eurasian Patent Organization (AM, AZ, BY, KG, KZ, RU, TJ, TM)
European Patent Office (AL, AT, BE, BG, CH, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HR, HU, IE, IS, IT, LT, LU, LV, MC, MK, MT, NL, NO, PL, PT, RO, RS, SE, SI, SK, SM, TR)
African Intellectual Property Organization (BF, BJ, CF, CG, CI, CM, GA, GN, GQ, GW, KM, ML, MR, NE, SN, TD, TG)
Publication Language: Japanese (JA)
Filing Language: Japanese (JA)
Also published as:
CA2994666EP3312085CN107848620US20180370619BR112018010889RU0002690779