ES2150372B1 - AIR CONDITIONING AIR CONDITIONING AIR RECOVERY DEVICE. - Google Patents
AIR CONDITIONING AIR CONDITIONING AIR RECOVERY DEVICE.Info
- Publication number
- ES2150372B1 ES2150372B1 ES009801535A ES9801535A ES2150372B1 ES 2150372 B1 ES2150372 B1 ES 2150372B1 ES 009801535 A ES009801535 A ES 009801535A ES 9801535 A ES9801535 A ES 9801535A ES 2150372 B1 ES2150372 B1 ES 2150372B1
- Authority
- ES
- Spain
- Prior art keywords
- air conditioning
- air
- conditioning air
- recovery device
- turbine
- 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.)
- Expired - Lifetime
Links
Classifications
-
- 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
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
Abstract
El dispositivo consiste en colocar la turbina de una bomba de aire y a la válvula de salida del flujo de aire del avión en un conducto por donde se hace pasar todo el flujo de aire, estando el eje de la turbina unido al eje de un generador eléctrico, al de una bomba hidráulica o a la caja de engranajes del N2 o de los accesorios en el interior del motor, el aire de salida del aire acondicionado también puede ser enviado por un conducto para hacerle incidir sobre los extremos de los álabes del fan y sobre los álabes de la primera etapa del compresor de baja velocidad del motor.The device consists in placing the turbine of an air pump and the airflow outlet valve of the aircraft in a conduit through which all the air flow is passed, the turbine axis being connected to the axis of an electric generator , to that of a hydraulic pump or to the gearbox of the N2 or of the accessories inside the engine, the exhaust air from the air conditioner can also be sent through a duct to make it impact on the ends of the fan blades and on the blades of the first stage of the low speed motor compressor.
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES009801535A ES2150372B1 (en) | 1998-07-20 | 1998-07-20 | AIR CONDITIONING AIR CONDITIONING AIR RECOVERY DEVICE. |
US09/138,551 US6128896A (en) | 1998-01-14 | 1998-08-24 | Aircraft air conditioner energy recovery device |
EP99500060A EP0974515A3 (en) | 1998-07-20 | 1999-04-15 | Aircraft airconditioning energy recovery device |
US09/643,369 US6289665B1 (en) | 1996-02-10 | 2000-08-22 | Aircraft air conditioner energy recovery method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES009801535A ES2150372B1 (en) | 1998-07-20 | 1998-07-20 | AIR CONDITIONING AIR CONDITIONING AIR RECOVERY DEVICE. |
Publications (2)
Publication Number | Publication Date |
---|---|
ES2150372A1 ES2150372A1 (en) | 2000-11-16 |
ES2150372B1 true ES2150372B1 (en) | 2001-06-01 |
Family
ID=8304576
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES009801535A Expired - Lifetime ES2150372B1 (en) | 1996-02-10 | 1998-07-20 | AIR CONDITIONING AIR CONDITIONING AIR RECOVERY DEVICE. |
Country Status (1)
Country | Link |
---|---|
ES (1) | ES2150372B1 (en) |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5137230A (en) * | 1991-06-04 | 1992-08-11 | General Electric Company | Aircraft gas turbine engine bleed air energy recovery apparatus |
DE4320302C2 (en) * | 1993-06-18 | 1996-09-12 | Daimler Benz Aerospace Airbus | Arrangement for energy generation on board an aircraft, in particular a passenger aircraft |
DE19542843C1 (en) * | 1995-11-17 | 1996-12-19 | Daimler Benz Aerospace Airbus | Reduction of structure heating in supersonic aircraft during flight |
US5721402A (en) * | 1996-09-09 | 1998-02-24 | Northrop Grumman Corporation | Noise suppression system for a jet engine |
-
1998
- 1998-07-20 ES ES009801535A patent/ES2150372B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
ES2150372A1 (en) | 2000-11-16 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EC2A | Search report published |
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