FR2993920B1 - Helice non carenee a pales a calage variable pour une turbomachine - Google Patents

Helice non carenee a pales a calage variable pour une turbomachine

Info

Publication number
FR2993920B1
FR2993920B1 FR1357289A FR1357289A FR2993920B1 FR 2993920 B1 FR2993920 B1 FR 2993920B1 FR 1357289 A FR1357289 A FR 1357289A FR 1357289 A FR1357289 A FR 1357289A FR 2993920 B1 FR2993920 B1 FR 2993920B1
Authority
FR
France
Prior art keywords
careed
turbomachine
propeller
variable shaft
variable
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
FR1357289A
Other languages
English (en)
Other versions
FR2993920A1 (fr
Inventor
Adrien Jacques Philippe Fabre
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 FR1357289A priority Critical patent/FR2993920B1/fr
Publication of FR2993920A1 publication Critical patent/FR2993920A1/fr
Application granted granted Critical
Publication of FR2993920B1 publication Critical patent/FR2993920B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • B64C11/04—Blade mountings
    • B64C11/06—Blade mountings for variable-pitch blades
    • 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
    • F01D7/00—Rotors with blades adjustable in operation; Control thereof
    • F01D7/02—Rotors with blades adjustable in operation; Control thereof having adjustment responsive to speed
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/20—Adaptations of gas-turbine plants for driving vehicles
    • F02C6/206—Adaptations of gas-turbine plants for driving vehicles the vehicles being airscrew driven
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D2027/005—Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR]
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/70—Adjusting of angle of incidence or attack of rotating blades
    • F05B2260/74—Adjusting of angle of incidence or attack of rotating blades by turning around an axis perpendicular the rotor centre line
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/325—Application in turbines in gas turbines to drive unshrouded, high solidity propeller
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Support Of The Bearing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1357289A 2012-07-25 2013-07-24 Helice non carenee a pales a calage variable pour une turbomachine Active FR2993920B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1357289A FR2993920B1 (fr) 2012-07-25 2013-07-24 Helice non carenee a pales a calage variable pour une turbomachine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1257207A FR2993919B1 (fr) 2012-07-25 2012-07-25 Helice non carenee a pales a calage variable pour une turbomachine
FR1357289A FR2993920B1 (fr) 2012-07-25 2013-07-24 Helice non carenee a pales a calage variable pour une turbomachine

Publications (2)

Publication Number Publication Date
FR2993920A1 FR2993920A1 (fr) 2014-01-31
FR2993920B1 true FR2993920B1 (fr) 2016-09-09

Family

ID=47022861

Family Applications (2)

Application Number Title Priority Date Filing Date
FR1257207A Expired - Fee Related FR2993919B1 (fr) 2012-07-25 2012-07-25 Helice non carenee a pales a calage variable pour une turbomachine
FR1357289A Active FR2993920B1 (fr) 2012-07-25 2013-07-24 Helice non carenee a pales a calage variable pour une turbomachine

Family Applications Before (1)

Application Number Title Priority Date Filing Date
FR1257207A Expired - Fee Related FR2993919B1 (fr) 2012-07-25 2012-07-25 Helice non carenee a pales a calage variable pour une turbomachine

Country Status (1)

Country Link
FR (2) FR2993919B1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3021295B1 (fr) 2014-05-21 2016-05-13 Snecma Moyeu raidi pour helice non carenee a pales a calage variable de turbomachine.
CN115885110A (zh) 2020-07-24 2023-03-31 赛峰飞机发动机公司 包括轮叶和轮叶桨距设置系统的组件
EP4185523B1 (fr) 2020-07-24 2024-06-26 Safran Aircraft Engines Système de commande du calage angulaire d'une aube d'helice pour une turbomachine d'aeronef

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3228673A (en) * 1963-08-26 1966-01-11 William L Hinks Laterally supported static load bearing
US3292711A (en) * 1965-03-30 1966-12-20 Lord Corp Blade pitch change bearing
US3297094A (en) * 1965-10-20 1967-01-10 Boeing Co Aircraft propelling assembly
US3511492A (en) * 1967-08-17 1970-05-12 Trw Inc Flexible laminated bearing stabilized against buckling
US3782854A (en) * 1972-07-05 1974-01-01 United Aircraft Corp Elastomeric bearing for a helicopter rotor
DE2643166A1 (de) * 1975-11-03 1977-05-12 United Technologies Corp Elastomeres lager fuer hubschrauberrotor
US4601591A (en) * 1984-05-14 1986-07-22 The Garrett Corporation Elastomeric bearing damper apparatus and associated methods
FR2943313B1 (fr) * 2009-03-23 2011-05-27 Snecma Helice non carenee a pales a calage variable pour une turbomachine
FR2943312B1 (fr) * 2009-03-23 2011-05-27 Snecma Helice non carenee a pales a calage variable pour une turbomachine

Also Published As

Publication number Publication date
FR2993920A1 (fr) 2014-01-31
FR2993919B1 (fr) 2014-07-11
FR2993919A1 (fr) 2014-01-31

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