FR2990718B1 - Helice pour moteur d'aeronef comprenant des moyens de reduction du bruit a moyennes et hautes frequences et amelioration de la perception acoustique. - Google Patents

Helice pour moteur d'aeronef comprenant des moyens de reduction du bruit a moyennes et hautes frequences et amelioration de la perception acoustique.

Info

Publication number
FR2990718B1
FR2990718B1 FR1254490A FR1254490A FR2990718B1 FR 2990718 B1 FR2990718 B1 FR 2990718B1 FR 1254490 A FR1254490 A FR 1254490A FR 1254490 A FR1254490 A FR 1254490A FR 2990718 B1 FR2990718 B1 FR 2990718B1
Authority
FR
France
Prior art keywords
medium
high frequencies
aircraft engine
reducing noise
engine propeller
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 - Fee Related
Application number
FR1254490A
Other languages
English (en)
Other versions
FR2990718A1 (fr
Inventor
Camil Negulescu
Magdi Omais
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations 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 Airbus Operations SAS filed Critical Airbus Operations SAS
Priority to FR1254490A priority Critical patent/FR2990718B1/fr
Priority to US13/894,076 priority patent/US9540094B2/en
Publication of FR2990718A1 publication Critical patent/FR2990718A1/fr
Application granted granted Critical
Publication of FR2990718B1 publication Critical patent/FR2990718B1/fr
Expired - Fee Related 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
    • B64C11/46—Arrangements of, or constructional features peculiar to, multiple propellers
    • B64C11/48—Units of two or more coaxial propellers
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D2027/005—Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR]
    • 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
FR1254490A 2012-05-16 2012-05-16 Helice pour moteur d'aeronef comprenant des moyens de reduction du bruit a moyennes et hautes frequences et amelioration de la perception acoustique. Expired - Fee Related FR2990718B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1254490A FR2990718B1 (fr) 2012-05-16 2012-05-16 Helice pour moteur d'aeronef comprenant des moyens de reduction du bruit a moyennes et hautes frequences et amelioration de la perception acoustique.
US13/894,076 US9540094B2 (en) 2012-05-16 2013-05-14 Propeller for an aircraft engine comprising means for reducing noise at middle and high frequencies and improving the acoustic perception

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1254490A FR2990718B1 (fr) 2012-05-16 2012-05-16 Helice pour moteur d'aeronef comprenant des moyens de reduction du bruit a moyennes et hautes frequences et amelioration de la perception acoustique.

Publications (2)

Publication Number Publication Date
FR2990718A1 FR2990718A1 (fr) 2013-11-22
FR2990718B1 true FR2990718B1 (fr) 2016-12-09

Family

ID=46514642

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1254490A Expired - Fee Related FR2990718B1 (fr) 2012-05-16 2012-05-16 Helice pour moteur d'aeronef comprenant des moyens de reduction du bruit a moyennes et hautes frequences et amelioration de la perception acoustique.

Country Status (2)

Country Link
US (1) US9540094B2 (fr)
FR (1) FR2990718B1 (fr)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9714575B2 (en) * 2013-11-27 2017-07-25 Hamilton Sundstrand Corporation Differential blade design for propeller noise reduction
US10137982B1 (en) 2014-05-11 2018-11-27 Wing Aviation Llc Propeller units
FR3029576B1 (fr) * 2014-12-04 2016-12-30 Snecma Procede pour reduire le niveau de bruit d'une soufflante de turbomachine
EP3241743B1 (fr) * 2016-05-02 2018-12-26 Ratier-Figeac SAS Commande de pas de pale
US10604245B2 (en) 2016-12-30 2020-03-31 Wing Aviation Llc Rotor units having asymmetric rotor blades
CA3063192A1 (fr) 2017-05-10 2018-11-15 Embry-Riddle Aeronautical University, Inc. Systemes et procedes d'attenuation du bruit pour aeronef hybride et electrique
US11401824B2 (en) 2019-10-15 2022-08-02 General Electric Company Gas turbine engine outlet guide vane assembly
US11286795B2 (en) 2019-10-15 2022-03-29 General Electric Company Mount for an airfoil
US20210108595A1 (en) 2019-10-15 2021-04-15 General Electric Company Unducted single rotor engine and method for operation
CN112660396A (zh) 2019-10-15 2021-04-16 通用电气公司 用于飞行器的可去除机身护罩
US11506067B2 (en) 2019-10-15 2022-11-22 General Electric Company Gas turbine engine with clutch assembly
US11655768B2 (en) 2021-07-26 2023-05-23 General Electric Company High fan up speed engine
US11739689B2 (en) 2021-08-23 2023-08-29 General Electric Company Ice reduction mechanism for turbofan engine
US11767790B2 (en) 2021-08-23 2023-09-26 General Electric Company Object direction mechanism for turbofan engine
US11480063B1 (en) 2021-09-27 2022-10-25 General Electric Company Gas turbine engine with inlet pre-swirl features
US11788465B2 (en) 2022-01-19 2023-10-17 General Electric Company Bleed flow assembly for a gas turbine engine
US11808281B2 (en) 2022-03-04 2023-11-07 General Electric Company Gas turbine engine with variable pitch inlet pre-swirl features
US11725526B1 (en) 2022-03-08 2023-08-15 General Electric Company Turbofan engine having nacelle with non-annular inlet

Family Cites Families (7)

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Publication number Priority date Publication date Assignee Title
DE1503520A1 (de) * 1965-09-22 1970-02-26 Daimler Benz Ag Schaufelrad von Axial- oder Radialverdichtern
US4784575A (en) * 1986-11-19 1988-11-15 General Electric Company Counterrotating aircraft propulsor blades
JP2662838B2 (ja) * 1992-03-24 1997-10-15 川崎重工業株式会社 回転翼航空機の尾部回転翼
US5667361A (en) * 1995-09-14 1997-09-16 United Technologies Corporation Flutter resistant blades, vanes and arrays thereof for a turbomachine
US5966525A (en) * 1997-04-09 1999-10-12 United Technologies Corporation Acoustically improved gas turbine blade array
US7234914B2 (en) * 2002-11-12 2007-06-26 Continum Dynamics, Inc. Apparatus and method for enhancing lift produced by an airfoil
DE102009007013A1 (de) * 2009-01-31 2010-08-12 Deutsches Zentrum für Luft- und Raumfahrt e.V. Triebwerk, insbesondere CROR-Antrieb, für ein Flugzeug

Also Published As

Publication number Publication date
US20140064968A1 (en) 2014-03-06
FR2990718A1 (fr) 2013-11-22
US9540094B2 (en) 2017-01-10

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