ES2172103T3 - Dispositivo de descongelacion para motor de entrada de aire de motor a reaccion. - Google Patents
Dispositivo de descongelacion para motor de entrada de aire de motor a reaccion.Info
- Publication number
- ES2172103T3 ES2172103T3 ES98402870T ES98402870T ES2172103T3 ES 2172103 T3 ES2172103 T3 ES 2172103T3 ES 98402870 T ES98402870 T ES 98402870T ES 98402870 T ES98402870 T ES 98402870T ES 2172103 T3 ES2172103 T3 ES 2172103T3
- Authority
- ES
- Spain
- Prior art keywords
- motor
- reaction
- air input
- defrosting device
- hot air
- 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
- 238000010257 thawing Methods 0.000 title abstract 2
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L27/00—Adjustable joints, Joints allowing movement
- F16L27/12—Adjustable joints, Joints allowing movement allowing substantial longitudinal adjustment or movement
- F16L27/125—Adjustable joints, Joints allowing movement allowing substantial longitudinal adjustment or movement having longitudinal and rotary movement
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/047—Heating to prevent icing
-
- 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
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0233—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
-
- 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
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Fuel-Injection Apparatus (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
- Motor Or Generator Cooling System (AREA)
Abstract
LA PRESENTE INVENCION SE REFIERE AL DESESCARCHE DEL BORDE DE ATAQUE DE LA CAPERUZA DE ENTRADA DE AIRE DE UN MOTOR A REACCION. SEGUN LA INVENCION, EL INYECTOR (12) ENCARGADO DE INYECTAR AIRE CALIENTE A PRESION EN EL INTERIOR DE DICHO BORDE DE ATAQUE ESTA CONECTADO A LA ENTRADA DE AIRE CALIENTE A PRESION MEDIANTE UNA JUNTA DE ROTULA.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9714611A FR2771452B1 (fr) | 1997-11-21 | 1997-11-21 | Dispositif de degivrage pour capot d'entree d'air de moteur a reaction |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2172103T3 true ES2172103T3 (es) | 2002-09-16 |
Family
ID=9513628
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES98402870T Expired - Lifetime ES2172103T3 (es) | 1997-11-21 | 1998-11-19 | Dispositivo de descongelacion para motor de entrada de aire de motor a reaccion. |
Country Status (5)
Country | Link |
---|---|
US (1) | US6193192B1 (es) |
EP (1) | EP0918150B1 (es) |
DE (1) | DE69803741T2 (es) |
ES (1) | ES2172103T3 (es) |
FR (1) | FR2771452B1 (es) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2424064A1 (es) * | 2012-03-23 | 2013-09-26 | Juan Francisco LÓPEZ GIL | Apertura de sobres con facilidad |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6709024B1 (en) | 2000-09-27 | 2004-03-23 | General Electric Company | Method and apparatus for assembling couplings for transferring fluids |
FR2886674B1 (fr) * | 2005-06-07 | 2007-08-03 | Airbus France Sas | Systeme pour le degivrage du bord d'attaque d'un capot d'entree d'air pour turbomoteur |
FR2887294B1 (fr) * | 2005-06-21 | 2007-08-10 | Airbus France Sas | Systeme pour le degivrage du bord d'attaque d'un capot d'entree d'air pour turbomoteur |
FR2898867B1 (fr) * | 2006-03-27 | 2008-12-19 | Airbus France Sas | Systeme pour le degivrage d'un capot d'entree d'air pour turbomoteur. |
GB2440133A (en) * | 2006-07-18 | 2008-01-23 | Gkn Aerospace Transparency Sys | A de-icing heated leading edge component of an aircraft |
FR2921901B1 (fr) * | 2007-10-08 | 2011-03-18 | Aircelle Sa | Structure d'entree d'air apte a etre montee en amont d'une structure mediane de nacelle pour moteur d'aeronef, et nacelle equipee d'une telle structure d'entree d'air |
US20090108134A1 (en) * | 2007-10-25 | 2009-04-30 | General Electric Company | Icing protection system and method for enhancing heat transfer |
US7975966B2 (en) * | 2008-02-04 | 2011-07-12 | Embraer - Empresa Brasileira De Aeronautica S.A. | Icing protection for aircraft air inlet scoops |
FR2927882B1 (fr) * | 2008-02-27 | 2010-02-12 | Aircelle Sa | Structure d'entree d'air pour une nacelle d'un aeronef |
FR2928695B1 (fr) * | 2008-03-13 | 2012-06-29 | Aircelle Sa | Dispositif d'acheminement d'air sous pression entre un moteur d'aeronef et un compartiment de degivrage d'une structure d'entree d'air de nacelle |
GB0812562D0 (en) * | 2008-07-10 | 2008-08-13 | Airbus Uk Ltd | A Connector for an aircraft fuel pipe |
FR2954279B1 (fr) * | 2009-12-18 | 2014-08-22 | Airbus Operations Sas | Entree d'air d'une nacelle d'aeronef integrant des moyens d'injection en air chaud pour le traitement du givre optimises |
FR2957586B1 (fr) * | 2010-03-18 | 2012-04-27 | Airbus Operations Sas | Dispositif de degivrage comprenant des moyens pour detecter une fuite au niveau d'une alimentation en air chaud |
FR2975435B1 (fr) | 2011-05-16 | 2016-09-02 | Snecma | Dispositif de degivrage d'un bec de separation de turbomachine |
US9528442B2 (en) * | 2013-08-21 | 2016-12-27 | The Boeing Company | Aircraft engine anti-icing (EAI) barrier assembly, system and method |
US10138811B2 (en) * | 2014-03-13 | 2018-11-27 | The Boeing Company | Enhanced temperature control anti-ice nozzle |
BE1023289B1 (fr) | 2015-07-17 | 2017-01-24 | Safran Aero Boosters S.A. | Bec de separation de compresseur basse pression de turbomachine axiale avec conduit annulaire de degivrage |
US10625871B1 (en) * | 2015-08-24 | 2020-04-21 | Roller Bearing Company Of America, Inc. | Dynamic movement tube connection system |
US10267334B2 (en) * | 2016-08-01 | 2019-04-23 | United Technologies Corporation | Annular heatshield |
US10708979B2 (en) | 2016-10-07 | 2020-07-07 | De-Ice Technologies | Heating a bulk medium |
RU177304U1 (ru) * | 2017-08-29 | 2018-02-15 | Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") | Труба подвода горячего воздуха к противообледенительной системе |
FR3072421B1 (fr) * | 2017-10-18 | 2019-09-27 | Airbus Operations | Levre d'entree d'air d'un moteur d'aeronef comportant un systeme de degivrage |
FR3087477A1 (fr) * | 2018-10-22 | 2020-04-24 | Safran Aircraft Engines | Dispositif de degivrage d'un bec de turbomachine |
US11220344B2 (en) * | 2018-12-17 | 2022-01-11 | Rohr, Inc. | Anti-ice double walled duct system |
US11325716B2 (en) * | 2019-05-24 | 2022-05-10 | Rohr, Inc. | Inlet bulkhead with ventilation groove |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2657076A (en) * | 1950-05-19 | 1953-10-27 | Ryan Aeronautical Co | Flexible joint for tubes |
US2836436A (en) * | 1955-01-24 | 1958-05-27 | R L A P I Soc | Coupling joined by fluid-pressure-deformed packing |
US2931672A (en) * | 1956-06-05 | 1960-04-05 | George W Merritt | Flexible duct mounting |
CH417245A (de) * | 1964-05-22 | 1966-07-15 | Jansen & Co Ag | Muffenverbindung für Rohre, insbesondere für Kunststoffrohre |
US3339832A (en) * | 1965-08-19 | 1967-09-05 | Gen Electric | Pipe connections for aircraft gas turbine engines |
US3502356A (en) * | 1967-11-02 | 1970-03-24 | Hancock Brick & Tile Co | Plain end sewer pipes and coupling for same |
US3596934A (en) * | 1969-05-06 | 1971-08-03 | Herbert A De Cenzo | Flexible fluidtight coupling for tubes |
US4522433A (en) * | 1982-05-14 | 1985-06-11 | Stanley Aviation Corporation | Spherical seat flexible O-ring coupling |
US4733890A (en) * | 1984-07-09 | 1988-03-29 | Stratoflex, Inc. | Formed fluid coupling apparatus |
AU581684B2 (en) * | 1984-10-08 | 1989-03-02 | Short Brothers Plc | Duct for hot air |
FR2621554B1 (fr) | 1987-10-07 | 1990-01-05 | Snecma | Capot d'entree non tournant de turboreacteur a fixation centrale et turboreacteur ainsi equipe |
US5106129A (en) * | 1990-10-09 | 1992-04-21 | Delaware Capital Formation, Inc. | Flexible coupling for transferring a fluid between two fluid conduits |
GB9120113D0 (en) * | 1991-09-20 | 1992-09-23 | Short Brothers Plc | Thermal antiicing of aircraft structures |
US5127681A (en) * | 1991-12-09 | 1992-07-07 | Aeroquip Corporation | Flexible connector |
US5772254A (en) * | 1995-12-20 | 1998-06-30 | Eg&G Pressure Science, Inc. | Modular joint, with a replaceable sealing sleeve |
-
1997
- 1997-11-21 FR FR9714611A patent/FR2771452B1/fr not_active Expired - Lifetime
-
1998
- 1998-11-12 US US09/190,105 patent/US6193192B1/en not_active Expired - Lifetime
- 1998-11-19 DE DE69803741T patent/DE69803741T2/de not_active Expired - Lifetime
- 1998-11-19 EP EP98402870A patent/EP0918150B1/fr not_active Expired - Lifetime
- 1998-11-19 ES ES98402870T patent/ES2172103T3/es not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2424064A1 (es) * | 2012-03-23 | 2013-09-26 | Juan Francisco LÓPEZ GIL | Apertura de sobres con facilidad |
Also Published As
Publication number | Publication date |
---|---|
DE69803741D1 (de) | 2002-03-21 |
US6193192B1 (en) | 2001-02-27 |
FR2771452A1 (fr) | 1999-05-28 |
DE69803741T2 (de) | 2002-09-26 |
EP0918150A1 (fr) | 1999-05-26 |
FR2771452B1 (fr) | 2000-04-14 |
EP0918150B1 (fr) | 2002-02-06 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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