FR2950928B1 - Cone d'entree autodegivrant pour turbomachine d'aeronef - Google Patents

Cone d'entree autodegivrant pour turbomachine d'aeronef

Info

Publication number
FR2950928B1
FR2950928B1 FR0956890A FR0956890A FR2950928B1 FR 2950928 B1 FR2950928 B1 FR 2950928B1 FR 0956890 A FR0956890 A FR 0956890A FR 0956890 A FR0956890 A FR 0956890A FR 2950928 B1 FR2950928 B1 FR 2950928B1
Authority
FR
France
Prior art keywords
autosegiving
input cone
aircraft turbomachine
turbomachine
aircraft
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
Application number
FR0956890A
Other languages
English (en)
Other versions
FR2950928A1 (fr
Inventor
Francis Robert Forest
Florent Reboul
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA 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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR0956890A priority Critical patent/FR2950928B1/fr
Publication of FR2950928A1 publication Critical patent/FR2950928A1/fr
Application granted granted Critical
Publication of FR2950928B1 publication Critical patent/FR2950928B1/fr
Active 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/02—Hub construction
    • B64C11/14—Spinners
    • 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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/02—De-icing means for engines having icing phenomena
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0956890A 2009-10-02 2009-10-02 Cone d'entree autodegivrant pour turbomachine d'aeronef Active FR2950928B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0956890A FR2950928B1 (fr) 2009-10-02 2009-10-02 Cone d'entree autodegivrant pour turbomachine d'aeronef

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0956890A FR2950928B1 (fr) 2009-10-02 2009-10-02 Cone d'entree autodegivrant pour turbomachine d'aeronef

Publications (2)

Publication Number Publication Date
FR2950928A1 FR2950928A1 (fr) 2011-04-08
FR2950928B1 true FR2950928B1 (fr) 2011-12-09

Family

ID=42163809

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0956890A Active FR2950928B1 (fr) 2009-10-02 2009-10-02 Cone d'entree autodegivrant pour turbomachine d'aeronef

Country Status (1)

Country Link
FR (1) FR2950928B1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10087840B2 (en) 2013-04-03 2018-10-02 United Technologies Corporation Gas turbine engine de-icing system
EP3024729B1 (fr) 2013-07-26 2022-04-27 MRA Systems, LLC Mât d'accrochage de moteur pour aéronef

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB628191A (en) * 1947-02-06 1949-08-24 C S A Ind Ltd Improvements in or relating to de-icing means for spinners for aircraft screw propellers
US2812899A (en) * 1949-08-30 1957-11-12 A V Roe Canada Ltd Intake sprinkler for gas turbine engines
FR2168938B1 (fr) * 1972-01-27 1974-12-13 Snecma
FR2621554B1 (fr) * 1987-10-07 1990-01-05 Snecma Capot d'entree non tournant de turboreacteur a fixation centrale et turboreacteur ainsi equipe
GB2217393B (en) * 1988-04-14 1992-07-08 Rolls Royce Plc Nose bullet anti-icing for gas turbine engines
FR2912467B1 (fr) * 2007-02-14 2009-05-15 Snecma Sa Systeme de degivrage a l'huile du cone avant d'un turboreacteur d'avion.
US8210825B2 (en) * 2007-05-11 2012-07-03 Honeywell International Inc. Heated engine nose cone using spiral channels

Also Published As

Publication number Publication date
FR2950928A1 (fr) 2011-04-08

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