ES8703375A1 - Procedimiento para la produccion de energia y de aire acondicionado en aviones. - Google Patents
Procedimiento para la produccion de energia y de aire acondicionado en aviones.Info
- Publication number
- ES8703375A1 ES8703375A1 ES541772A ES541772A ES8703375A1 ES 8703375 A1 ES8703375 A1 ES 8703375A1 ES 541772 A ES541772 A ES 541772A ES 541772 A ES541772 A ES 541772A ES 8703375 A1 ES8703375 A1 ES 8703375A1
- Authority
- ES
- Spain
- Prior art keywords
- air
- aircraft
- power
- conditioning
- generation
- 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
Links
- 238000000034 method Methods 0.000 title abstract 2
- 238000004378 air conditioning Methods 0.000 abstract 3
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT 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
- B64D2013/0622—Environmental Control Systems used in combination with boundary layer control systems
-
- 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
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Pulmonology (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Jet Pumps And Other Pumps (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
- Air-Conditioning For Vehicles (AREA)
Abstract
PROCEDIMIENTO PARA LA PRODUCCION DE ENERGIA Y DE AIRE ACONDICIONADO EN AVIONES. CONSISTE EN: A) CONDUCIR EL AIRE DE LA CABINA A TRAVES DE UN TUBO DE CONDUCCION (5) A UN TUBO COLECTOR (6); B) SUCCIONAR EL AIRE FRESCO QUE PENETRA EN LA ENTRADA DE AIRE (4), A TRAVES DE UN CANAL DE ALIMENTACION (9) Y COMPRIMIRLO; CONDUCIRLO PARA SU POSTERIOR COMPRESION EN EL COMPRESOR DE AIRE ACONDICIONADO (2); D) CONDUCIR EL AIRE ACONDICIONADO COMPRIMIDO A TRAVES DE UN TUBO (15) Y UNA TUBERIA (13) AL INTERCAMBIADOR DE CALOR (11); Y E) CONDUCIR EL AIRE FRESCO DESPUES DE UN PRIMER ESCALONAMIENTO PARA SER USADO COMO AIRE FRESCO ACONDICIONADO. TIENE APLICACIONES EN AVIACION CIVIL Y DESTINADOS AL USO DE VIAJEROS.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3412101A DE3412101A1 (de) | 1984-03-31 | 1984-03-31 | Einbauanordnung eines hilfstriebwerkes im rumpfheck von transportflugzeugen zur wirtschaftlichen erzeugung von klimaluft und von vortriebsschub im flug |
Publications (2)
Publication Number | Publication Date |
---|---|
ES8703375A1 true ES8703375A1 (es) | 1987-02-16 |
ES541772A0 ES541772A0 (es) | 1987-02-16 |
Family
ID=6232270
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES541772A Expired ES8703375A1 (es) | 1984-03-31 | 1985-03-29 | Procedimiento para la produccion de energia y de aire acondicionado en aviones. |
Country Status (7)
Country | Link |
---|---|
US (1) | US4642997A (es) |
DE (1) | DE3412101A1 (es) |
ES (1) | ES8703375A1 (es) |
FR (1) | FR2563491B1 (es) |
GB (1) | GB2158937B (es) |
IT (1) | IT1183496B (es) |
NL (1) | NL8500916A (es) |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3633090A1 (de) * | 1986-09-29 | 1988-04-07 | Kloeckner Humboldt Deutz Ag | Hilfsgasturbinenanlage |
US5125597A (en) * | 1990-06-01 | 1992-06-30 | General Electric Company | Gas turbine engine powered aircraft environmental control system and boundary layer bleed with energy recovery system |
US5143329A (en) * | 1990-06-01 | 1992-09-01 | General Electric Company | Gas turbine engine powered aircraft environmental control system and boundary layer bleed |
US5123242A (en) * | 1990-07-30 | 1992-06-23 | General Electric Company | Precooling heat exchange arrangement integral with mounting structure fairing of gas turbine engine |
US5114103A (en) * | 1990-08-27 | 1992-05-19 | General Electric Company | Aircraft engine electrically powered boundary layer bleed system |
GB2248682B (en) * | 1990-09-28 | 1994-08-10 | Gilberts | Apparatus for controlling air flow in ductwork |
US5137230A (en) * | 1991-06-04 | 1992-08-11 | General Electric Company | Aircraft gas turbine engine bleed air energy recovery apparatus |
US6735953B1 (en) * | 1997-12-22 | 2004-05-18 | Allied Signal Inc. | Turbomachine-driven environmental control system |
FR2839948B1 (fr) * | 2002-05-22 | 2004-12-17 | Airbus France | Echangeur pour circuit de conditionnement d'air d'aeronef et ensemble de propulsion integrant un tel echangeur |
DE10361390B4 (de) | 2003-12-29 | 2008-05-08 | Airbus Deutschland Gmbh | Verfahren und Einrichtung zur Absaugung der Grenzschicht |
DE102004024016A1 (de) * | 2004-05-13 | 2005-12-22 | Airbus Deutschland Gmbh | Anordnung zur Grenzschichtabsaugung |
DE102004024057B3 (de) * | 2004-05-13 | 2005-09-15 | Airbus Deutschland Gmbh | Luftfahrzeug mit einem Fluidkanalsystem |
US7344107B2 (en) * | 2004-10-26 | 2008-03-18 | The Boeing Company | Dual flow APU inlet and associated systems and methods |
EP2572991B1 (en) * | 2011-09-26 | 2014-06-18 | Goodrich Lighting Systems GmbH | Aircraft light |
FR3012422B1 (fr) * | 2013-10-31 | 2016-12-09 | Microturbo | Procede et systeme de generation de puissance auxiliaire dans un aeronef |
EP3034395B1 (en) * | 2014-12-15 | 2018-06-27 | Rolls-Royce Corporation | Aircraft boundary layer removal with auxilliary power unit suction |
US10988262B2 (en) | 2018-03-14 | 2021-04-27 | Honeywell International Inc. | Cabin pressure control system architecture using cabin pressure air for inlet to APU core compressor |
US11273917B2 (en) | 2018-05-29 | 2022-03-15 | Honeywell International Inc. | Cabin discharge air management system and method for auxiliary power unit |
US11511865B2 (en) | 2018-05-29 | 2022-11-29 | Honeywell International Inc. | Air supply management system for auxiliary power unit |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2304151A (en) * | 1939-03-13 | 1942-12-08 | Robert B P Crawford | Air conditioning system |
US2697917A (en) * | 1951-09-15 | 1954-12-28 | Garrett Corp | Air conditioning apparatus for enclosures of aircraft |
BE535079A (es) * | 1954-01-25 | |||
US2829505A (en) * | 1955-04-27 | 1958-04-08 | Lockheed Aircraft Corp | Systems for preventing ice formation |
US2929224A (en) * | 1955-12-23 | 1960-03-22 | Garrett Corp | Gas turbine compressor driven air conditioning system |
US3052106A (en) * | 1960-05-19 | 1962-09-04 | Thompson Ramo Wooldridge Inc | Air cooling system |
US3247676A (en) * | 1965-01-14 | 1966-04-26 | Rosemount Eng Co Ltd | Aerodynamic cooling |
US3470703A (en) * | 1968-01-16 | 1969-10-07 | Lian Tong Wen | Hypersonic cooling device |
US3688770A (en) * | 1970-10-08 | 1972-09-05 | Westinghouse Electric Corp | High pressure gas pressurization system |
US3699777A (en) * | 1971-04-09 | 1972-10-24 | United Aircraft Corp | Capacity control for gas turbine powered air cycle refrigeration system |
US4014179A (en) * | 1975-08-29 | 1977-03-29 | The Garrett Corporation | Air conditioning system for aircraft |
US4374469A (en) * | 1980-12-24 | 1983-02-22 | United Technologies Corporation | Variable capacity air cycle refrigeration system |
-
1984
- 1984-03-31 DE DE3412101A patent/DE3412101A1/de not_active Withdrawn
-
1985
- 1985-03-27 IT IT20107/85A patent/IT1183496B/it active
- 1985-03-27 GB GB08508024A patent/GB2158937B/en not_active Expired
- 1985-03-28 FR FR858504694A patent/FR2563491B1/fr not_active Expired
- 1985-03-28 NL NL8500916A patent/NL8500916A/nl not_active Application Discontinuation
- 1985-03-29 ES ES541772A patent/ES8703375A1/es not_active Expired
- 1985-03-29 US US06/717,377 patent/US4642997A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
IT1183496B (it) | 1987-10-22 |
IT8520107A0 (it) | 1985-03-27 |
US4642997A (en) | 1987-02-17 |
GB2158937A (en) | 1985-11-20 |
FR2563491B1 (fr) | 1989-02-03 |
GB2158937B (en) | 1987-11-04 |
FR2563491A1 (fr) | 1985-10-31 |
DE3412101A1 (de) | 1985-10-10 |
NL8500916A (nl) | 1985-10-16 |
GB8508024D0 (en) | 1985-05-01 |
ES541772A0 (es) | 1987-02-16 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FD1A | Patent lapsed |
Effective date: 19971001 |