FR2935348B1 - Turbomachine a helices non carenees - Google Patents

Turbomachine a helices non carenees

Info

Publication number
FR2935348B1
FR2935348B1 FR0804748A FR0804748A FR2935348B1 FR 2935348 B1 FR2935348 B1 FR 2935348B1 FR 0804748 A FR0804748 A FR 0804748A FR 0804748 A FR0804748 A FR 0804748A FR 2935348 B1 FR2935348 B1 FR 2935348B1
Authority
FR
France
Prior art keywords
carineated
turbomachine
propellers
carineated propellers
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
FR0804748A
Other languages
English (en)
Other versions
FR2935348A1 (fr
Inventor
Benoit Guillaume Farvacque
Philippe Jacques Pierre Fessou
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 FR0804748A priority Critical patent/FR2935348B1/fr
Publication of FR2935348A1 publication Critical patent/FR2935348A1/fr
Application granted granted Critical
Publication of FR2935348B1 publication Critical patent/FR2935348B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/16Blades
    • B64C11/18Aerodynamic features
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/46Arrangements of, or constructional features peculiar to, multiple propellers
    • B64C11/48Units of two or more coaxial propellers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/02Multi-stage pumps
    • F04D19/024Multi-stage pumps with contrarotating parts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/08Sealings
    • F04D29/16Sealings between pressure and suction sides
    • F04D29/161Sealings between pressure and suction sides especially adapted for elastic fluid pumps
    • F04D29/164Sealings between pressure and suction sides especially adapted for elastic fluid pumps of an axial flow wheel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/68Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
    • F04D29/681Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/20Rotors
    • F05D2240/30Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
    • F05D2240/307Characteristics 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/10Two-dimensional
    • F05D2250/18Two-dimensional patterned
    • F05D2250/182Two-dimensional patterned crenellated, notched
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/10Two-dimensional
    • F05D2250/18Two-dimensional patterned
    • F05D2250/183Two-dimensional patterned zigzag
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0804748A 2008-08-28 2008-08-28 Turbomachine a helices non carenees Active FR2935348B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0804748A FR2935348B1 (fr) 2008-08-28 2008-08-28 Turbomachine a helices non carenees

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0804748A FR2935348B1 (fr) 2008-08-28 2008-08-28 Turbomachine a helices non carenees

Publications (2)

Publication Number Publication Date
FR2935348A1 FR2935348A1 (fr) 2010-03-05
FR2935348B1 true FR2935348B1 (fr) 2011-04-08

Family

ID=40433908

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0804748A Active FR2935348B1 (fr) 2008-08-28 2008-08-28 Turbomachine a helices non carenees

Country Status (1)

Country Link
FR (1) FR2935348B1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2538024B1 (fr) * 2011-06-24 2015-09-23 Alstom Technology Ltd Aube dans une turbomachine
US9102397B2 (en) * 2011-12-20 2015-08-11 General Electric Company Airfoils including tip profile for noise reduction and method for fabricating same
US10414486B2 (en) 2015-11-30 2019-09-17 General Electric Company Airfoil for a rotary machine including a propellor assembly
US11225874B2 (en) * 2019-12-20 2022-01-18 Raytheon Technologies Corporation Turbine engine rotor blade with castellated tip surface

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4883240A (en) * 1985-08-09 1989-11-28 General Electric Company Aircraft propeller noise reduction
GB2220712B (en) * 1988-07-13 1992-12-09 Rolls Royce Plc Open rotor blading
US5190441A (en) * 1990-08-13 1993-03-02 General Electric Company Noise reduction in aircraft propellers
JPH04314693A (ja) * 1991-04-11 1992-11-05 Mitsubishi Heavy Ind Ltd 回転翼
DE19706668A1 (de) * 1997-02-20 1998-09-10 Winfried Dipl Ing Bessler Multiwinglets für Fluggeräte und Modelle für: Flugzeuge, Ultraleichtflugzeuge, Hubschrauberpropeller, Flugdrachen + Gleitschirme, Luftkissenfahrzeuge und Modelle aller dieser Fluggeräte
FR2783885B1 (fr) * 1998-09-25 2001-07-27 Geco As Structure portante a tourbillon marginal reduit
US6578798B1 (en) * 2002-04-08 2003-06-17 Faruk Dizdarevic Airlifting surface division
US20050061921A1 (en) * 2003-09-19 2005-03-24 Egolf Thomas A. Aerodynamic tip protuberances for tip vortex intensity reduction

Also Published As

Publication number Publication date
FR2935348A1 (fr) 2010-03-05

Similar Documents

Publication Publication Date Title
FR2950381B1 (fr) Turbomachine a helices non carenees contrarotatives
FR2935349B1 (fr) Turbomachine a helices non carenees
BRPI1011134A2 (pt) turbomáquina.
BRPI1006029A2 (pt) um ventilador
DK2274514T3 (da) En vindmøllevinge
DK2138716T3 (da) Vingeindsats
IT1393131B1 (it) Controvento a ingobbamento limitato
DK2406492T3 (da) Vingemontering
BRPI0915524A2 (pt) conjunto de aerofólio
FR2962109B1 (fr) Turbomoteur a helices non carenees
BRPI0917179A2 (pt) turbina
DK2429882T3 (da) Forbindelsesanordning
BRPI0922070A2 (pt) turbina.
DK2295808T4 (da) Fiskevenlig pumpe eller turbine
FR2927605B1 (fr) Propulseur hydraulique a rotor peripherique ameliore.
DK2283215T3 (da) Honeycombkonstuktion med radialt forskelligt udførte forbindelsessteder
FR2935348B1 (fr) Turbomachine a helices non carenees
IT1397426B1 (it) Radiatore a segmenti
FR2937005B1 (fr) Planeur a propulsion eolienne
SE0801582A0 (sv) Framdrivningsanordning
BRPI0920293A2 (pt) nacela
BRPI0923233A2 (pt) combustor
BRPI0922853A2 (pt) combustor
FI20085942A0 (fi) Kaivo
IT1393434B1 (it) Radiatore a segmenti

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 10

CD Change of name or company name

Owner name: SNECMA, FR

Effective date: 20170713

PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13

PLFP Fee payment

Year of fee payment: 14

PLFP Fee payment

Year of fee payment: 15

PLFP Fee payment

Year of fee payment: 16