FR2576872B1 - Helice avec fleche en extremite de pale a stabilite amelioree - Google Patents

Helice avec fleche en extremite de pale a stabilite amelioree

Info

Publication number
FR2576872B1
FR2576872B1 FR8514818A FR8514818A FR2576872B1 FR 2576872 B1 FR2576872 B1 FR 2576872B1 FR 8514818 A FR8514818 A FR 8514818A FR 8514818 A FR8514818 A FR 8514818A FR 2576872 B1 FR2576872 B1 FR 2576872B1
Authority
FR
France
Prior art keywords
propeller
improved stability
boom end
end pole
pole
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
Application number
FR8514818A
Other languages
English (en)
Other versions
FR2576872A1 (fr
Inventor
Edward Allen Rothman
John Alfred Violette
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of FR2576872A1 publication Critical patent/FR2576872A1/fr
Application granted granted Critical
Publication of FR2576872B1 publication Critical patent/FR2576872B1/fr
Expired legal-status Critical Current

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
    • B64C11/16—Blades
    • B64C11/18—Aerodynamic features
    • 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

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Nitrogen And Oxygen Or Sulfur-Condensed Heterocyclic Ring Systems (AREA)
  • Percussion Or Vibration Massage (AREA)
FR8514818A 1985-02-07 1985-10-07 Helice avec fleche en extremite de pale a stabilite amelioree Expired FR2576872B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US69911985A 1985-02-07 1985-02-07

Publications (2)

Publication Number Publication Date
FR2576872A1 FR2576872A1 (fr) 1986-08-08
FR2576872B1 true FR2576872B1 (fr) 1987-07-24

Family

ID=24808020

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8514818A Expired FR2576872B1 (fr) 1985-02-07 1985-10-07 Helice avec fleche en extremite de pale a stabilite amelioree

Country Status (7)

Country Link
JP (1) JPS61181798A (fr)
BR (1) BR8504907A (fr)
CA (1) CA1270802A (fr)
DE (1) DE3535399A1 (fr)
FR (1) FR2576872B1 (fr)
GB (1) GB2170868B (fr)
IT (1) IT1185996B (fr)

Families Citing this family (34)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2605588B1 (fr) * 1986-10-24 1989-04-28 Onera (Off Nat Aerospatiale) Perfectionnements apportes aux helices aeriennes, notamment pour propulseurs d'aeronef
DE3738785A1 (de) * 1986-11-19 1988-05-26 Gen Electric Gegenlaeufig rotierende flugzeug-antriebsschaufeln
USRE34207E (en) * 1986-11-19 1993-03-30 General Electric Company Counterrotating aircraft propulsor blades
US5165856A (en) * 1988-06-02 1992-11-24 General Electric Company Fan blade mount
US5102302A (en) * 1988-06-02 1992-04-07 General Electric Company Fan blade mount
GB2220712B (en) * 1988-07-13 1992-12-09 Rolls Royce Plc Open rotor blading
US4971641A (en) * 1988-11-14 1990-11-20 General Electric Company Method of making counterrotating aircraft propeller blades
US6071077A (en) * 1996-04-09 2000-06-06 Rolls-Royce Plc Swept fan blade
GB2469516A (en) * 2009-04-17 2010-10-20 Insensys Ltd Rotor blade with optical strain sensors covered by erosion shield
US20130340406A1 (en) * 2012-01-31 2013-12-26 Edward J. Gallagher Fan stagger angle for geared gas turbine engine
EP3108106B1 (fr) 2014-02-19 2022-05-04 Raytheon Technologies Corporation Pale de moteur à turbine à gaz
EP3108104B1 (fr) 2014-02-19 2019-06-12 United Technologies Corporation Surface portante de moteur à turbine à gaz
WO2015126451A1 (fr) 2014-02-19 2015-08-27 United Technologies Corporation Surface portante de moteur à turbine à gaz
US10570915B2 (en) 2014-02-19 2020-02-25 United Technologies Corporation Gas turbine engine airfoil
WO2015127032A1 (fr) 2014-02-19 2015-08-27 United Technologies Corporation Surface portante pour turbine à gaz
EP3108109B1 (fr) 2014-02-19 2023-09-13 Raytheon Technologies Corporation Aube de soufflante de moteur à turbine à gaz
WO2015178974A2 (fr) 2014-02-19 2015-11-26 United Technologies Corporation Surface portante de moteur à turbine à gaz
US9567858B2 (en) 2014-02-19 2017-02-14 United Technologies Corporation Gas turbine engine airfoil
US10422226B2 (en) 2014-02-19 2019-09-24 United Technologies Corporation Gas turbine engine airfoil
WO2015175052A2 (fr) 2014-02-19 2015-11-19 United Technologies Corporation Profil aérodynamique de turbine à gaz
EP3108114B1 (fr) 2014-02-19 2021-12-08 Raytheon Technologies Corporation Profil d'aube pour moteur à turbine à gaz
WO2015126452A1 (fr) * 2014-02-19 2015-08-27 United Technologies Corporation Surface portante de moteur à turbine à gaz
WO2015175051A2 (fr) 2014-02-19 2015-11-19 United Technologies Corporation Profil aérodynamique de moteur à turbine à gaz
WO2015175058A2 (fr) 2014-02-19 2015-11-19 United Technologies Corporation Surface portante de moteur à turbine à gaz
EP3108100B1 (fr) 2014-02-19 2021-04-14 Raytheon Technologies Corporation Pale de soufflante de moteur à turbine à gaz
US10605259B2 (en) 2014-02-19 2020-03-31 United Technologies Corporation Gas turbine engine airfoil
EP3108118B1 (fr) 2014-02-19 2019-09-18 United Technologies Corporation Surface portante de moteur à turbine à gaz
EP3108116B1 (fr) 2014-02-19 2024-01-17 RTX Corporation Moteur à turbine à gaz
EP3114321B1 (fr) 2014-02-19 2019-04-17 United Technologies Corporation Profil aérodynamique de moteur à turbine à gaz
EP3108107B1 (fr) 2014-02-19 2023-10-11 Raytheon Technologies Corporation Moteur à double flux à engrenage avec aubes de compresseur basse pression
EP3108119B1 (fr) 2014-02-19 2023-10-04 RTX Corporation Moteur à double flux à engrenage avec aubes mobiles de compresseur basse pression
WO2015175056A2 (fr) 2014-02-19 2015-11-19 United Technologies Corporation Surface portante de moteur à turbine à gaz
FR3045565B1 (fr) 2015-12-21 2018-07-27 Airbus Helicopters Pale de rotor d'aeronef a geometrie adaptee pour l'ameloration acoustique lors d'un vol d'approche et l'amelioration des performances en vol d'avancement
FR3045564B1 (fr) * 2015-12-21 2018-08-17 Airbus Helicopters Pale de rotor d'aeronef a geometrie adaptee pour l'amelioration acoustique lors de vols d'approche et l'amelioration des performances en vols stationnaire et d'avancement

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3989406A (en) * 1974-11-26 1976-11-02 Bolt Beranek And Newman, Inc. Method of and apparatus for preventing leading edge shocks and shock-related noise in transonic and supersonic rotor blades and the like
US4171183A (en) * 1976-09-24 1979-10-16 United Technologies Corporation Multi-bladed, high speed prop-fan
US4358246A (en) * 1979-07-16 1982-11-09 United Technologies Corporation Noise reduction means for prop-fan and the construction thereof

Also Published As

Publication number Publication date
IT1185996B (it) 1987-11-18
BR8504907A (pt) 1986-12-16
GB2170868B (en) 1988-07-13
IT8522377A0 (it) 1985-10-07
CA1270802A (fr) 1990-06-26
JPS61181798A (ja) 1986-08-14
GB2170868A (en) 1986-08-13
FR2576872A1 (fr) 1986-08-08
DE3535399A1 (de) 1986-08-07
GB8524280D0 (en) 1985-11-06

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Legal Events

Date Code Title Description
ST Notification of lapse