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1. WO2020109740 - AIR MANAGEMENT SYSTEM, IN PARTICULAR FOR AN AIR CONDITIONING AND DE-ICING PACK

Publication Number WO/2020/109740
Publication Date 04.06.2020
International Application No. PCT/FR2019/052842
International Filing Date 29.11.2019
IPC
B64D 13/08 2006.01
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
13Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space
06the air being conditioned
08the air being heated or cooled
B64D 13/06 2006.01
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
13Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space
06the air being conditioned
B64D 15/04 2006.01
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
15De-icing or preventing icing on exterior surfaces of aircraft
02by ducted hot gas or liquid
04Hot gas application
CPC
B64D 13/08
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
13Arrangements or adaptations of air-treatment apparatus for aircraft crew or passenger, or freight space; ; or structural parts of the aircarft
06the air being conditioned
08the air being heated or cooled
B64D 15/04
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
15De-icing or preventing icing on exterior surfaces of aircraft
02by ducted hot gas or liquid
04Hot gas application
B64D 2013/0607
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
13Arrangements or adaptations of air-treatment apparatus for aircraft crew or passenger, or freight space; ; or structural parts of the aircarft
06the air being conditioned
0603Environmental Control Systems
0607providing hot air or liquid for deicing aircraft parts, e.g. aerodynamic surfaces or windows
B64D 2013/0614
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
13Arrangements or adaptations of air-treatment apparatus for aircraft crew or passenger, or freight space; ; or structural parts of the aircarft
06the air being conditioned
0603Environmental Control Systems
0614with subsystems for cooling avionics
Applicants
  • SAFRAN [FR]/[FR]
Inventors
  • JALJAL, Nawal
  • MAALOUF, Samer
Agents
  • REGIMBEAU
Priority Data
187207529.11.2018FR
Publication Language French (FR)
Filing Language French (FR)
Designated States
Title
(EN) AIR MANAGEMENT SYSTEM, IN PARTICULAR FOR AN AIR CONDITIONING AND DE-ICING PACK
(FR) SYSTÈME DE GESTION D'AIR NOTAMMENT POUR PACK DE CONDITIONNEMENT D'AIR ET DÉGIVRAGE
Abstract
(EN)
The invention relates to an air management system (10) for an ECS pack (20), comprising: - a leading edge (110, 210) of a turbomachine nacelle (100) or aircraft wing, - an air inlet (22), for example of an ECS pack (20), characterised in that the leading edge (110) comprises an exchanger (112), the exchanger (112) being connected to the air inlet (22) such that, during operation, the air inlet (22) is supplied with the air from the exchanger (112).
(FR)
L'invention concerne un système de gestion d'air (10) pour pack ECS (20), comprenant : -un bord d'attaque (110, 210) de nacelle de turbomachine (100) ou d'aile d'avion, -une entrée d'air (22), par exemple de pack ECS (20), caractérisé en ce que le bord d'attaque (110) comprend un échangeur (112), l'échangeur (112) étant connecté avec l'entrée d'air (22), de sorte qu'en fonctionnement, l'entrée d'air (22) est alimentée avec l'air issu de l'échangeur (112).
Latest bibliographic data on file with the International Bureau