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1. WO2021064375 - SYSTEMS, ARRANGEMENTS, STRUCTURES AND METHODS FOR AIRCRAFT

Publication Number WO/2021/064375
Publication Date 08.04.2021
International Application No. PCT/GB2020/052374
International Filing Date 01.10.2020
IPC
B64C 3/18 2006.1
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
3Wings
18Spars; Ribs; Stringers
B64C 25/34 2006.1
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
25Alighting gear
32characterised by elements which contact the ground or similar surface
34wheeled type, e.g. multi-wheeled bogies
B64D 31/06 2006.1
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
31Power plant control; Arrangement thereof
02Initiating means
06actuated automatically
B64D 37/30 2006.1
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
37Arrangements in connection with fuel supply for power plant
30Fuel systems for specific fuels
CPC
B60L 1/02
BPERFORMING OPERATIONS; TRANSPORTING
60VEHICLES IN GENERAL
LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES
1Supplying electric power to auxiliary equipment of vehicles
02to electric heating circuits
B60L 1/20
BPERFORMING OPERATIONS; TRANSPORTING
60VEHICLES IN GENERAL
LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES
1Supplying electric power to auxiliary equipment of vehicles
20Energy regeneration from auxiliary equipment
B60L 2200/10
BPERFORMING OPERATIONS; TRANSPORTING
60VEHICLES IN GENERAL
LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES
2200Type of vehicles
10Air crafts
B60L 2240/36
BPERFORMING OPERATIONS; TRANSPORTING
60VEHICLES IN GENERAL
LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES
2240Control parameters of input or output; Target parameters
10Vehicle control parameters
36Temperature of vehicle components or parts
B60L 50/60
BPERFORMING OPERATIONS; TRANSPORTING
60VEHICLES IN GENERAL
LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES
50Electric propulsion with power supplied within the vehicle
50using propulsion power supplied by batteries or fuel cells
60using power supplied by batteries
B60L 50/61
BPERFORMING OPERATIONS; TRANSPORTING
60VEHICLES IN GENERAL
LPROPULSION OF ELECTRICALLY-PROPELLED VEHICLES
50Electric propulsion with power supplied within the vehicle
50using propulsion power supplied by batteries or fuel cells
60using power supplied by batteries
61by batteries charged by engine-driven generators, e.g. series hybrid electric vehicles
Applicants
  • ELECTRIC AVIATION GROUP LTD [GB]/[GB]
Inventors
  • WOOD, Norman
  • IQBAL, Kamran
Agents
  • BARKER BRETTELL LLP
Priority Data
1914219.902.10.2019GB
1914220.702.10.2019GB
1914223.102.10.2019GB
1914224.902.10.2019GB
1914225.602.10.2019GB
1914227.202.10.2019GB
1916136.306.11.2019GB
1916137.106.11.2019GB
1916138.906.11.2019GB
1916139.706.11.2019GB
1917074.522.11.2019GB
2003496.311.03.2020GB
2003497.111.03.2020GB
2003498.911.03.2020GB
2003500.211.03.2020GB
2003501.011.03.2020GB
2003502.811.03.2020GB
2003503.611.03.2020GB
2003504.411.03.2020GB
2003505.111.03.2020GB
2003509.311.03.2020GB
2003511.911.03.2020GB
2003512.711.03.2020GB
2003513.511.03.2020GB
Publication Language English (en)
Filing Language English (EN)
Designated States
Title
(EN) SYSTEMS, ARRANGEMENTS, STRUCTURES AND METHODS FOR AIRCRAFT
(FR) SYSTÈMES, AGENCEMENTS, STRUCTURES ET PROCÉDÉS POUR AÉRONEF
Abstract
(EN) According to the present disclosure there is provided a spar arrangement for segregating components installed in an aircraft, the spar arrangement being locatable between the components, to provide one or more voids therebetween. Additionally, the present disclosure provides a method of segregating components installed in an aircraft, the method comprising the steps of: providing one or more spar arrangements; and locating the one or more spar arrangements between the components to provide a void therebetween.
(FR) La présente invention concerne un agencement de longeron pour séparer des éléments installés dans un aéronef, l'agencement de longeron pouvant être positionné entre les éléments, pour ménager un ou plusieurs vides entre ceux-ci. De plus, la présente invention concerne un procédé de ségrégation d'éléments installés dans un aéronef, le procédé comprenant les étapes consistant à : fournir un ou plusieurs agencements de longeron ; et placer le ou les agencements de longeron entre les éléments pour ménager un vide entre ceux-ci.
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