FR2953254B1 - AIR INLET HOOD FOR REACTION ENGINE AND HOT AIR MIXER FOR SUCH HOOD - Google Patents

AIR INLET HOOD FOR REACTION ENGINE AND HOT AIR MIXER FOR SUCH HOOD

Info

Publication number
FR2953254B1
FR2953254B1 FR0905798A FR0905798A FR2953254B1 FR 2953254 B1 FR2953254 B1 FR 2953254B1 FR 0905798 A FR0905798 A FR 0905798A FR 0905798 A FR0905798 A FR 0905798A FR 2953254 B1 FR2953254 B1 FR 2953254B1
Authority
FR
France
Prior art keywords
hood
air inlet
reaction engine
hot air
mixer
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 - Fee Related
Application number
FR0905798A
Other languages
French (fr)
Other versions
FR2953254A1 (en
Inventor
Nicolas Boulet
Alain Porte
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR0905798A priority Critical patent/FR2953254B1/en
Publication of FR2953254A1 publication Critical patent/FR2953254A1/en
Application granted granted Critical
Publication of FR2953254B1 publication Critical patent/FR2953254B1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/25—Three-dimensional helical
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR0905798A 2009-12-01 2009-12-01 AIR INLET HOOD FOR REACTION ENGINE AND HOT AIR MIXER FOR SUCH HOOD Expired - Fee Related FR2953254B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0905798A FR2953254B1 (en) 2009-12-01 2009-12-01 AIR INLET HOOD FOR REACTION ENGINE AND HOT AIR MIXER FOR SUCH HOOD

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0905798A FR2953254B1 (en) 2009-12-01 2009-12-01 AIR INLET HOOD FOR REACTION ENGINE AND HOT AIR MIXER FOR SUCH HOOD

Publications (2)

Publication Number Publication Date
FR2953254A1 FR2953254A1 (en) 2011-06-03
FR2953254B1 true FR2953254B1 (en) 2012-01-20

Family

ID=42315735

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0905798A Expired - Fee Related FR2953254B1 (en) 2009-12-01 2009-12-01 AIR INLET HOOD FOR REACTION ENGINE AND HOT AIR MIXER FOR SUCH HOOD

Country Status (1)

Country Link
FR (1) FR2953254B1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105992867A (en) * 2013-10-25 2016-10-05 肖特兄弟公司 Anti-icing system for an aircraft
US11613373B2 (en) 2020-03-13 2023-03-28 Rohr, Inc. Nozzle for a thermal anti-icing system

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10167086B2 (en) 2013-10-25 2019-01-01 Short Brothers Plc Anti-icing system for an aircraft
CN104110308B (en) * 2014-05-08 2015-12-16 中国联合工程公司 A kind of inlet air heating structure for large-scale gas turbine
US10723464B2 (en) 2015-08-26 2020-07-28 Rohr, Inc. Injector nozzle configuration for swirl anti-icing system
US10393020B2 (en) 2015-08-26 2019-08-27 Rohr, Inc. Injector nozzle configuration for swirl anti-icing system
US10513978B2 (en) * 2016-05-02 2019-12-24 General Electric Company Directed flow nozzle swirl enhancer
US11279491B2 (en) 2019-04-30 2022-03-22 Rohr, Inc. Method and apparatus for aircraft anti-icing
US11465758B2 (en) * 2019-04-30 2022-10-11 Rohr, Inc. Method and apparatus for aircraft anti-icing
US11167855B2 (en) 2019-04-30 2021-11-09 Rohr, Inc. Method and apparatus for aircraft anti-icing
FR3140350A1 (en) * 2022-10-04 2024-04-05 Safran Nacelles Injector for a device for defrosting an air inlet of an aircraft turbojet nacelle and associated method

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL276188A (en) * 1966-09-19
US3590560A (en) * 1969-07-28 1971-07-06 David B Pall Tubular vortex air cleaner
US5257498A (en) * 1992-04-23 1993-11-02 United Technologies Corporation Efficient anti-ice exhaust vent
US6267328B1 (en) * 1999-10-21 2001-07-31 Rohr, Inc. Hot air injection for swirling rotational anti-icing system
US6354538B1 (en) * 1999-10-25 2002-03-12 Rohr, Inc. Passive control of hot air injection for swirling rotational type anti-icing system
FR2813581B1 (en) * 2000-09-06 2002-11-29 Aerospatiale Matra Airbus AIR INTAKE COVER FOR REACTION ENGINE PROVIDED WITH DEFROSTING MEANS

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105992867A (en) * 2013-10-25 2016-10-05 肖特兄弟公司 Anti-icing system for an aircraft
CN105992867B (en) * 2013-10-25 2018-01-30 肖特兄弟公司 Anti-icing system and its method for aircraft
US11613373B2 (en) 2020-03-13 2023-03-28 Rohr, Inc. Nozzle for a thermal anti-icing system

Also Published As

Publication number Publication date
FR2953254A1 (en) 2011-06-03

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