FR3089204B1 - Air management system in particular for air conditioning and defrosting pack - Google Patents
Air management system in particular for air conditioning and defrosting pack Download PDFInfo
- Publication number
- FR3089204B1 FR3089204B1 FR1872075A FR1872075A FR3089204B1 FR 3089204 B1 FR3089204 B1 FR 3089204B1 FR 1872075 A FR1872075 A FR 1872075A FR 1872075 A FR1872075 A FR 1872075A FR 3089204 B1 FR3089204 B1 FR 3089204B1
- Authority
- FR
- France
- Prior art keywords
- air
- management system
- pack
- defrosting
- air conditioning
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
- B64D13/08—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned the air being heated or cooled
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
- B64D15/04—Hot gas application
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
- B64D2013/0603—Environmental Control Systems
- B64D2013/0607—Environmental Control Systems providing hot air or liquid for deicing aircraft parts, e.g. aerodynamic surfaces or windows
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
- B64D2013/0603—Environmental Control Systems
- B64D2013/0614—Environmental Control Systems with subsystems for cooling avionics
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Abstract
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). Figure pour l’abrégé : Fig. 2The invention relates to an air management system (10) for an ECS pack (20), comprising: - a leading edge (110, 210) of a turbine engine nacelle (100) or an aircraft wing, - an air inlet (22), for example an ECS pack (20), characterized in that the leading edge (110) comprises an exchanger (112), the exchanger (112) being connected with the inlet of air (22), so that in operation, the air inlet (22) is supplied with air from the exchanger (112). Figure for abstract: Fig. 2
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1872075A FR3089204B1 (en) | 2018-11-29 | 2018-11-29 | Air management system in particular for air conditioning and defrosting pack |
PCT/FR2019/052842 WO2020109740A1 (en) | 2018-11-29 | 2019-11-29 | Air management system, in particular for an air conditioning and de-icing pack |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1872075A FR3089204B1 (en) | 2018-11-29 | 2018-11-29 | Air management system in particular for air conditioning and defrosting pack |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3089204A1 FR3089204A1 (en) | 2020-06-05 |
FR3089204B1 true FR3089204B1 (en) | 2022-04-01 |
Family
ID=66530134
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1872075A Active FR3089204B1 (en) | 2018-11-29 | 2018-11-29 | Air management system in particular for air conditioning and defrosting pack |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR3089204B1 (en) |
WO (1) | WO2020109740A1 (en) |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3933327A (en) * | 1974-08-30 | 1976-01-20 | Rohr Industries, Inc. | Aircraft anti-icing plenum |
US3981466A (en) * | 1974-12-23 | 1976-09-21 | The Boeing Company | Integrated thermal anti-icing and environmental control system |
US4482114A (en) * | 1981-01-26 | 1984-11-13 | The Boeing Company | Integrated thermal anti-icing and environmental control system |
FR2998265B1 (en) * | 2012-11-19 | 2016-02-05 | Turbomeca | AIR CONDITIONING METHOD AND SYSTEM FOR AN AIRCRAFT |
US10823066B2 (en) * | 2015-12-09 | 2020-11-03 | General Electric Company | Thermal management system |
DE102016120682A1 (en) * | 2016-10-28 | 2018-05-03 | Rolls-Royce Deutschland Ltd & Co Kg | Aircraft bleed air system and method for providing bleed air in an aircraft engine |
US10407164B2 (en) * | 2016-10-28 | 2019-09-10 | Honeywell International Inc. | Air distribution system with drag reducing inlet |
-
2018
- 2018-11-29 FR FR1872075A patent/FR3089204B1/en active Active
-
2019
- 2019-11-29 WO PCT/FR2019/052842 patent/WO2020109740A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2020109740A1 (en) | 2020-06-04 |
FR3089204A1 (en) | 2020-06-05 |
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Effective date: 20200605 |
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Year of fee payment: 3 |
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PLFP | Fee payment |
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