JP6385951B2 - ターボ機械用プロペラブレード - Google Patents
ターボ機械用プロペラブレード Download PDFInfo
- Publication number
- JP6385951B2 JP6385951B2 JP2015546082A JP2015546082A JP6385951B2 JP 6385951 B2 JP6385951 B2 JP 6385951B2 JP 2015546082 A JP2015546082 A JP 2015546082A JP 2015546082 A JP2015546082 A JP 2015546082A JP 6385951 B2 JP6385951 B2 JP 6385951B2
- Authority
- JP
- Japan
- Prior art keywords
- blade
- height
- propeller
- vortex
- leading edge
- 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.)
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- 238000007373 indentation Methods 0.000 claims description 17
- 230000003993 interaction Effects 0.000 description 5
- 238000011144 upstream manufacturing Methods 0.000 description 4
- 238000002485 combustion reaction Methods 0.000 description 3
- 230000005855 radiation Effects 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 2
- 239000000567 combustion gas Substances 0.000 description 2
- 230000000368 destabilizing effect Effects 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 239000012530 fluid Substances 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Images
Classifications
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- 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
- B64C11/46—Arrangements of, or constructional features peculiar to, multiple propellers
- B64C11/48—Units of two or more coaxial propellers
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- 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
- B64C11/16—Blades
- B64C11/18—Aerodynamic features
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/467—Aerodynamic features
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- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/141—Shape, i.e. outer, aerodynamic form
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- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/141—Shape, i.e. outer, aerodynamic form
- F01D5/145—Means for influencing boundary layers or secondary circulations
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- 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]
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- 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
-
- 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
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
-
- 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
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05D2240/303—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the leading edge of a rotor blade
-
- 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
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05D2240/307—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the tip of a rotor blade
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- 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)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Description
Claims (8)
- プロペラのブレード(34)にして、ブレード根元部(38)からブレード先端(36)までの高さの方向を半径方向に伸び、前縁(40)および後縁(42)と共に、圧力側面と吸引側面とを有するブレード(34)であって、前縁(40)に沿って、ブレードが取り付けられるプロペラの半径方向に対応するブレードの半径方向と前縁の接線との間の角度(α)は、ブレード(34)の前記高さの60%〜80%の範囲に位置する極大点zmaxを通ること、およびブレード(34)の吸引側面は、ブレード(34)の半径方向に反転した湾曲を形成するように、前縁(40)から後縁に向かって軸方向に伸びて、ブレード(34)の前記高さに関して極大点zmaxとブレード先端(34)との間に位置する凹面のくぼみ(54)を含むことを特徴とする、ブレード(34)。
- 極大点が、ブレード(34)の前記高さの約75%に位置することを特徴とする、請求項1に記載のブレード。
- くぼみ(54)が、ブレード(34)の前記高さに沿って測定した場合に、ほぼ一定の幅を有することを特徴とする、請求項1または請求項2のいずれかに記載のブレード。
- くぼみ(54)が、ブレードの前記高さに沿って測定した場合に、ブレード(34)の前記高さの15%〜20%の範囲の幅を有することを特徴とする、請求項1〜請求項3のうちのいずれか一項に記載のブレード。
- くぼみ(54)の底部が、ブレード(34)の前記高さの75%〜90%に位置することを特徴とする、請求項1〜請求項4のうちのいずれか一項に記載のブレード。
- くぼみ(54)が、接線方向に測定した場合に、前縁(40)から後縁(42)に向かって増大する深さを有することを特徴とする、請求項1〜請求項5のうちのいずれか一項に記載のブレード。
- 請求項1〜請求項6のうちのいずれか一項に記載の複数のブレード(34)を備えることを特徴とする、タービンエンジン用アンダクテッドプロペラ。
- 航空機ターボジェットまたはターボプロップのようなタービンエンジンであって、請求項7に記載の少なくとも1つのアンダクテッドプロペラを含むことを特徴とするタービンエンジン。
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1261805A FR2999151B1 (fr) | 2012-12-07 | 2012-12-07 | Pale d'helice pour turbomachine |
FR1261805 | 2012-12-07 | ||
PCT/FR2013/052962 WO2014087109A1 (fr) | 2012-12-07 | 2013-12-05 | Pale d'helice pour turbomachine |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2016508094A JP2016508094A (ja) | 2016-03-17 |
JP6385951B2 true JP6385951B2 (ja) | 2018-09-05 |
Family
ID=47878223
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2015546082A Active JP6385951B2 (ja) | 2012-12-07 | 2013-12-05 | ターボ機械用プロペラブレード |
Country Status (9)
Country | Link |
---|---|
US (1) | US10035582B2 (ja) |
EP (1) | EP2928769B1 (ja) |
JP (1) | JP6385951B2 (ja) |
CN (1) | CN104837726B (ja) |
BR (1) | BR112015012502B1 (ja) |
CA (1) | CA2893254C (ja) |
FR (1) | FR2999151B1 (ja) |
RU (1) | RU2645180C2 (ja) |
WO (1) | WO2014087109A1 (ja) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2999151B1 (fr) * | 2012-12-07 | 2017-01-27 | Snecma | Pale d'helice pour turbomachine |
FR3030446B1 (fr) | 2014-12-17 | 2018-06-01 | Safran Aircraft Engines | Turbomachine a helice multi-diametres |
FR3038341B1 (fr) * | 2015-07-03 | 2017-07-28 | Snecma | Procede d'alteration de la loi de vrillage de la surface aerodynamique d'une pale de soufflante de moteur a turbine a gaz |
US10414486B2 (en) | 2015-11-30 | 2019-09-17 | General Electric Company | Airfoil for a rotary machine including a propellor assembly |
US20170152019A1 (en) * | 2015-11-30 | 2017-06-01 | General Electric Company | Airfoil for a rotary machine including a propellor assembly |
WO2019119379A1 (zh) * | 2017-12-21 | 2019-06-27 | 深圳市大疆创新科技有限公司 | 螺旋桨、动力组件及无人飞行器 |
FR3084693B1 (fr) * | 2018-08-03 | 2020-12-25 | Safran Aircraft Engines | Turbomachine a helices non carenees |
IT201900007935A1 (it) | 2019-06-04 | 2020-12-04 | R E M Holding S R L | Ventilatore con virola migliorata |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1153315A (fr) | 1956-05-15 | 1958-03-05 | Mach A Coudre Cosson | Perfectionnements aux machines à coudre |
US3467197A (en) * | 1968-05-07 | 1969-09-16 | Bell Aerospace Corp | Rotor blade |
US4012172A (en) * | 1975-09-10 | 1977-03-15 | Avco Corporation | Low noise blades for axial flow compressors |
US5190441A (en) * | 1990-08-13 | 1993-03-02 | General Electric Company | Noise reduction in aircraft propellers |
DE19812624A1 (de) * | 1998-03-23 | 1999-09-30 | Bmw Rolls Royce Gmbh | Rotor-Schaufelblatt einer Axialströmungsmaschine |
US6341942B1 (en) * | 1999-12-18 | 2002-01-29 | General Electric Company | Rotator member and method |
JP3960776B2 (ja) * | 2001-11-09 | 2007-08-15 | 松下電器産業株式会社 | 空調用送風機羽根車 |
RU2354854C1 (ru) * | 2007-12-20 | 2009-05-10 | Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" | Рабочее колесо высокооборотного осевого вентилятора или компрессора |
FR2935349B1 (fr) | 2008-08-29 | 2010-10-01 | Snecma | Turbomachine a helices non carenees |
FR2938502B1 (fr) * | 2008-11-14 | 2010-12-10 | Snecma | Turbomachine comportant une helice non carenee equipee de moyens de guidage d'air |
US8167567B2 (en) * | 2008-12-17 | 2012-05-01 | United Technologies Corporation | Gas turbine engine airfoil |
GB0914591D0 (en) | 2009-08-21 | 2009-09-30 | Rolls Royce Plc | Fluidfoil tip vortex disruption |
GB2483061A (en) * | 2010-08-23 | 2012-02-29 | Rolls Royce Plc | A method of damping aerofoil structure vibrations |
FR2964426B1 (fr) * | 2010-09-06 | 2014-02-14 | Snecma | Aube mobile en materiau composite |
FR2969230B1 (fr) | 2010-12-15 | 2014-11-21 | Snecma | Aube de compresseur a loi d'empilage amelioree |
EP2476862B1 (en) * | 2011-01-13 | 2013-11-20 | Alstom Technology Ltd | Vane for an axial flow turbomachine and corresponding turbomachine |
FR2974060B1 (fr) * | 2011-04-15 | 2013-11-22 | Snecma | Dispositif de propulsion a helices contrarotatives et coaxiales non-carenees |
FR2980818B1 (fr) * | 2011-09-29 | 2016-01-22 | Snecma | Pale pour une helice de turbomachine, notamment a soufflante non carenee, helice et turbomachine correspondantes. |
FR2999151B1 (fr) * | 2012-12-07 | 2017-01-27 | Snecma | Pale d'helice pour turbomachine |
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2012
- 2012-12-07 FR FR1261805A patent/FR2999151B1/fr active Active
-
2013
- 2013-12-05 BR BR112015012502-6A patent/BR112015012502B1/pt active IP Right Grant
- 2013-12-05 CA CA2893254A patent/CA2893254C/fr active Active
- 2013-12-05 US US14/649,736 patent/US10035582B2/en active Active
- 2013-12-05 JP JP2015546082A patent/JP6385951B2/ja active Active
- 2013-12-05 WO PCT/FR2013/052962 patent/WO2014087109A1/fr active Application Filing
- 2013-12-05 EP EP13815063.6A patent/EP2928769B1/fr active Active
- 2013-12-05 RU RU2015127099A patent/RU2645180C2/ru active
- 2013-12-05 CN CN201380063979.0A patent/CN104837726B/zh active Active
Also Published As
Publication number | Publication date |
---|---|
CN104837726A (zh) | 2015-08-12 |
EP2928769B1 (fr) | 2017-02-08 |
BR112015012502A2 (pt) | 2017-07-11 |
US20150315915A1 (en) | 2015-11-05 |
CN104837726B (zh) | 2017-03-08 |
CA2893254C (fr) | 2021-02-09 |
JP2016508094A (ja) | 2016-03-17 |
US10035582B2 (en) | 2018-07-31 |
WO2014087109A1 (fr) | 2014-06-12 |
EP2928769A1 (fr) | 2015-10-14 |
BR112015012502B1 (pt) | 2021-08-31 |
FR2999151B1 (fr) | 2017-01-27 |
CA2893254A1 (fr) | 2014-06-12 |
RU2015127099A (ru) | 2017-01-13 |
FR2999151A1 (fr) | 2014-06-13 |
RU2645180C2 (ru) | 2018-02-16 |
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