BR112015018470A2 - anel de suporte híbrido para um motor de aeronave - Google Patents

anel de suporte híbrido para um motor de aeronave

Info

Publication number
BR112015018470A2
BR112015018470A2 BR112015018470A BR112015018470A BR112015018470A2 BR 112015018470 A2 BR112015018470 A2 BR 112015018470A2 BR 112015018470 A BR112015018470 A BR 112015018470A BR 112015018470 A BR112015018470 A BR 112015018470A BR 112015018470 A2 BR112015018470 A2 BR 112015018470A2
Authority
BR
Brazil
Prior art keywords
support ring
aircraft engine
hybrid support
hanger
belt
Prior art date
Application number
BR112015018470A
Other languages
English (en)
Inventor
James Roby Benjamin
Jason Bishop Michael
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of BR112015018470A2 publication Critical patent/BR112015018470A2/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
    • F01D5/066—Connecting means for joining rotor-discs or rotor-elements together, e.g. by a central bolt, by clamps
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/243—Flange connections; Bolting arrangements
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/02—Selection of particular materials
    • F04D29/023—Selection of particular materials especially adapted for elastic fluid pumps
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • 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
    • F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • F05D2300/12—Light metals
    • F05D2300/121—Aluminium
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • F05D2300/13—Refractory metals, i.e. Ti, V, Cr, Zr, Nb, Mo, Hf, Ta, W
    • F05D2300/133—Titanium
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • F05D2300/17—Alloys
    • F05D2300/171—Steel alloys
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Clamps And Clips (AREA)

Abstract

resumo “anel de suporte híbrido para um motor de aeronave” trata-se de um anel de suporte híbrido que compreende um suspensor e uma correia, sendo que o suspensor é definido por um flange e uma perna que se estende para trás que tem um ressalto, sendo que o suspensor também se estende circunferencialmente, sendo que o suspensor é feito de um primeiro material, a correia se estende circunferencialmente e está disposta no ressalto, sendo que a correia é feita de um segundo material.
BR112015018470A 2013-02-08 2014-01-21 anel de suporte híbrido para um motor de aeronave BR112015018470A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US13/763,228 US9969489B2 (en) 2013-02-08 2013-02-08 Hybrid spinner support
PCT/US2014/012233 WO2014123685A1 (en) 2013-02-08 2014-01-21 Hybrid spinner support

Publications (1)

Publication Number Publication Date
BR112015018470A2 true BR112015018470A2 (pt) 2017-07-18

Family

ID=50033843

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015018470A BR112015018470A2 (pt) 2013-02-08 2014-01-21 anel de suporte híbrido para um motor de aeronave

Country Status (7)

Country Link
US (1) US9969489B2 (pt)
EP (1) EP2954166A1 (pt)
JP (1) JP2016515176A (pt)
CN (1) CN104968892B (pt)
BR (1) BR112015018470A2 (pt)
CA (1) CA2899913C (pt)
WO (1) WO2014123685A1 (pt)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2986580B1 (fr) * 2012-02-08 2014-02-28 Safran Piece de revolution de rotor de turbomachine aeronautique
US9149997B2 (en) * 2012-09-14 2015-10-06 United Technologies Composite flange from braided preform
US10156427B2 (en) * 2014-12-11 2018-12-18 Stanislaw Litwin Multi-spectral camouflage device and method
CN106555675B (zh) * 2015-09-30 2018-07-10 中国航发商用航空发动机有限责任公司 风扇进气锥及航空涡扇发动机进气系统
US10167088B2 (en) * 2015-10-19 2019-01-01 General Electric Company Crosswind performance aircraft engine spinner
US10583913B2 (en) * 2017-03-14 2020-03-10 General Electric Company Stud push out mount for a turbine engine spinner assembly having a spinner push out stud joint connecting through a counterbore of a spinner bolt hole
JP6971864B2 (ja) * 2018-01-15 2021-11-24 オムロン株式会社 ベルトの製造方法
US11725525B2 (en) * 2022-01-19 2023-08-15 Rolls-Royce North American Technologies Inc. Engine section stator vane assembly with band stiffness features for turbine engines

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2346680A (en) * 1941-07-03 1944-04-18 Harper Elwood Propeller spinner
US2401247A (en) * 1941-09-20 1946-05-28 Goodrich Co B F Spinner assembly
US3990814A (en) * 1975-06-25 1976-11-09 United Technologies Corporation Spinner
US4699568A (en) * 1984-06-25 1987-10-13 Hartzell Propeller Inc. Aircraft propeller with improved spinner assembly
FR2642396B1 (fr) * 1989-01-30 1991-10-11 Messier Hispano Sa Roue d'avion en materiau composite
US5833435A (en) * 1996-12-24 1998-11-10 United Technologies Corporation Inlet nose cone assembly and method for repairing the assembly
US6059524A (en) * 1998-04-20 2000-05-09 United Technologies Corporation Penetration resistant fan casing for a turbine engine
GB2363170A (en) 2000-06-08 2001-12-12 Rolls Royce Plc Attaching a nose cone to a gas turbine engine rotor
GB0102169D0 (en) 2001-01-27 2001-03-14 Rolls Royce Plc A gas turbine engine nose cone
DE10259943A1 (de) * 2002-12-20 2004-07-01 Rolls-Royce Deutschland Ltd & Co Kg Schutzring für das Fan-Schutzgehäuse eines Gasturbinentriebswerks
GB2398353B (en) * 2003-02-14 2006-02-15 Rolls Royce Plc A gas turbine engine nose cone
US7254934B2 (en) * 2005-03-24 2007-08-14 The Gates Corporation Endless belt with improved load carrying cord
DE102006011513A1 (de) 2006-03-10 2007-09-13 Rolls-Royce Deutschland Ltd & Co Kg Einlaufkonus aus einem Faserverbundwerkstoff für ein Gasturbinentriebwerk und Verfahren zu dessen Herstellung
FR2930595B1 (fr) 2008-04-24 2011-10-14 Snecma Rotor de soufflante d'une turbomachine ou d'un moteur d'essai
US20100051157A1 (en) * 2008-08-29 2010-03-04 Bina Patel Botts Insert and belt overlay containing chopped carbon fibers
DE102008045546A1 (de) 2008-09-03 2010-03-04 Rolls-Royce Deutschland Ltd & Co Kg Fluggasturbinen-Einlaufkonus
FR2943726B1 (fr) * 2009-03-31 2014-04-25 Snecma Capot d'entree tournant pour turbomachine, comprenant une extremite avant excentree
DE102009016802A1 (de) * 2009-04-09 2010-10-14 Rolls-Royce Deutschland Ltd & Co Kg Einlaufkonus aus Faserverbundmaterial für ein Gasturbinentriebwerk
US8449260B2 (en) * 2009-10-30 2013-05-28 General Electric Company Composite load-bearing rotating ring and process therefor
DE102009053000B4 (de) 2009-11-16 2014-01-02 Rolls-Royce Deutschland Ltd & Co Kg Fanrückhaltescheibe für ein Strahltriebwerk
US8876042B2 (en) 2009-12-21 2014-11-04 General Electric Company Integrated nacelle assembly
US8807931B2 (en) 2010-01-04 2014-08-19 General Electric Company System for impact zone reinforcement
GB201020230D0 (en) 2010-11-30 2011-01-12 Rolls Royce Plc Nose cone assembly

Also Published As

Publication number Publication date
US20140255203A1 (en) 2014-09-11
CA2899913A1 (en) 2014-08-14
CA2899913C (en) 2018-08-07
CN104968892A (zh) 2015-10-07
EP2954166A1 (en) 2015-12-16
CN104968892B (zh) 2017-12-05
US9969489B2 (en) 2018-05-15
JP2016515176A (ja) 2016-05-26
WO2014123685A1 (en) 2014-08-14

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B11B Dismissal acc. art. 36, par 1 of ipl - no reply within 90 days to fullfil the necessary requirements