DE60130824T2 - Nasenhaube aus Faserverbundwerkstoff und Verfahren zu ihrer Herstellung - Google Patents

Nasenhaube aus Faserverbundwerkstoff und Verfahren zu ihrer Herstellung Download PDF

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Publication number
DE60130824T2
DE60130824T2 DE60130824T DE60130824T DE60130824T2 DE 60130824 T2 DE60130824 T2 DE 60130824T2 DE 60130824 T DE60130824 T DE 60130824T DE 60130824 T DE60130824 T DE 60130824T DE 60130824 T2 DE60130824 T2 DE 60130824T2
Authority
DE
Germany
Prior art keywords
preform
nose
axial
mold
rib
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 - Lifetime
Application number
DE60130824T
Other languages
German (de)
English (en)
Other versions
DE60130824D1 (de
Inventor
Chen-Yu Jack Cincinnati Chou
Gerald Alexander Hamilton Pauley
Yiping West Chester Xu
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of DE60130824D1 publication Critical patent/DE60130824D1/de
Application granted granted Critical
Publication of DE60130824T2 publication Critical patent/DE60130824T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • B64C11/02—Hub construction
    • B64C11/14—Spinners
    • 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
    • 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
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • 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
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/23—Three-dimensional prismatic
    • F05D2250/232—Three-dimensional prismatic conical
    • 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
    • F05D2300/20—Oxide or non-oxide ceramics
    • F05D2300/21—Oxide ceramics
    • F05D2300/2102—Glass
    • 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
    • F05D2300/20—Oxide or non-oxide ceramics
    • F05D2300/22—Non-oxide ceramics
    • F05D2300/224—Carbon, e.g. graphite
    • 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
    • F05D2300/30—Inorganic materials other than provided for in groups F05D2300/10 - F05D2300/2291
    • 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
    • F05D2300/40—Organic materials
    • F05D2300/44—Resins
    • 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
    • F05D2300/601—Fabrics
    • F05D2300/6012—Woven fabrics
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49318—Repairing or disassembling

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Woven Fabrics (AREA)
  • Laminated Bodies (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
DE60130824T 2000-03-24 2001-03-19 Nasenhaube aus Faserverbundwerkstoff und Verfahren zu ihrer Herstellung Expired - Lifetime DE60130824T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US535923 2000-03-24
US09/535,923 US6358014B1 (en) 2000-03-24 2000-03-24 Composite spinner and method of making the same

Publications (2)

Publication Number Publication Date
DE60130824D1 DE60130824D1 (de) 2007-11-22
DE60130824T2 true DE60130824T2 (de) 2008-07-17

Family

ID=24136357

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60130824T Expired - Lifetime DE60130824T2 (de) 2000-03-24 2001-03-19 Nasenhaube aus Faserverbundwerkstoff und Verfahren zu ihrer Herstellung

Country Status (4)

Country Link
US (1) US6358014B1 (enExample)
EP (1) EP1136353B1 (enExample)
JP (1) JP2001349248A (enExample)
DE (1) DE60130824T2 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010030550A1 (de) * 2010-06-25 2011-12-29 Technische Universität Dresden Verbundbauteil mit einem Gewebe mit integrierten Profilen

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US6887043B2 (en) * 2003-03-28 2005-05-03 General Electric Company Methods and apparatus for assembling gas turbine engines
WO2007001371A2 (en) * 2004-09-17 2007-01-04 Aurora Flight Sciences Vibration isolation engine mount system and method for ducted fan aircraft
WO2007001372A2 (en) 2004-09-17 2007-01-04 Aurora Flight Sciences Ducted spinner for engine cooling
US7441724B2 (en) * 2004-09-17 2008-10-28 Aurora Flight Sciences Corporation System and method for controlling a roll rate of a torsionally-disconnected freewing aircraft
GB2418333A (en) * 2004-09-17 2006-03-22 Pranil Ram Tabbed user interface for stock trading
WO2007001369A2 (en) * 2004-09-17 2007-01-04 Aurora Flight Sciences System and method for controlling engine rpm of a ducted fan aircraft
WO2007001373A2 (en) * 2004-09-17 2007-01-04 Aurora Flight Sciences Inbound transition control for a trail-sitting vertical take off and landing aircraft
US7774025B2 (en) * 2005-09-19 2010-08-10 Silverbrook Research Pty Ltd Printing content on a reverse side of a coded surface
US7419556B2 (en) * 2005-10-11 2008-09-02 United Technologies Corporation Method of repair for inlet caps of turbine engines
US7997529B2 (en) * 2006-01-19 2011-08-16 The Boeing Company Compliant panel for aircraft
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
US8017188B2 (en) * 2007-04-17 2011-09-13 General Electric Company Methods of making articles having toughened and untoughened regions
DE602007003971D1 (de) * 2007-07-09 2010-02-04 Agusta Spa Vorrichtung und Verfahren zum Schutz eines Flugzeugbauteils vor Kollisionen mit fliegenden Objekten
US8287243B2 (en) * 2008-01-24 2012-10-16 General Electric Company Spinner of a wind turbine
US8363356B2 (en) * 2008-07-28 2013-01-29 Hgst, Netherlands B.V. High bandwidth and mechanical strength between a disk drive flexible circuit and a read write head suspension
DE102009016802A1 (de) * 2009-04-09 2010-10-14 Rolls-Royce Deutschland Ltd & Co Kg Einlaufkonus aus Faserverbundmaterial für ein Gasturbinentriebwerk
US9186850B2 (en) * 2009-10-28 2015-11-17 Albany Engineered Composites, Inc. Fiber preform, fiber reinforced composite, and method of making thereof
US9429029B2 (en) 2010-09-30 2016-08-30 Pratt & Whitney Canada Corp. Gas turbine blade and method of protecting same
US9587645B2 (en) 2010-09-30 2017-03-07 Pratt & Whitney Canada Corp. Airfoil blade
GB201020230D0 (en) * 2010-11-30 2011-01-12 Rolls Royce Plc Nose cone assembly
US9140272B2 (en) * 2011-10-24 2015-09-22 Hamilton Sundstrand Corporation Ram air fan outer housing
US9427835B2 (en) 2012-02-29 2016-08-30 Pratt & Whitney Canada Corp. Nano-metal coated vane component for gas turbine engines and method of manufacturing same
CN102678333A (zh) * 2012-05-23 2012-09-19 哈尔滨工程大学 一种进口防护网罩
US9353685B2 (en) * 2012-12-21 2016-05-31 United Technologies Corporation Turbine engine nosecone with deformation region
US10823058B2 (en) * 2013-01-29 2020-11-03 Raytheon Technologies Corporation Thermoplastic nosecone for a turbine engine
ES2635122T3 (es) * 2013-03-04 2017-10-02 Airbus Defence And Space Sa Capot monolítico mejorado de un motor de aeronave y método de fabricación
US9481448B2 (en) 2013-03-11 2016-11-01 Rolls-Royce Corporation Aerodynamic fairings secondarily attached to nosecone
CA2917884A1 (en) 2013-07-09 2015-01-15 United Technologies Corporation Plated polymer fan
CA2917967A1 (en) 2013-07-09 2015-01-15 United Technologies Corporation Plated polymer compressor
CA2917916A1 (en) * 2013-07-09 2015-02-05 United Technologies Corporation Plated polymer nosecone
WO2015006406A1 (en) 2013-07-09 2015-01-15 United Technologies Corporation Plated tubular lattice structure
EP3063391B1 (en) * 2013-10-30 2019-09-04 United Technologies Corporation Nosecap
US9249776B2 (en) * 2014-02-19 2016-02-02 General Electric Company Wind turbine dome and method of assembly
US10392949B2 (en) * 2014-03-03 2019-08-27 United Technologies Corporation Gas turbine engine with reinforced spinner
US10100644B2 (en) 2014-03-03 2018-10-16 Rolls-Royce Corporation Spinner for a gas turbine engine
US10094282B2 (en) * 2014-07-30 2018-10-09 United Technologies Corporation Spinner aft-extended forward return flange
US10507902B2 (en) 2015-04-21 2019-12-17 General Electric Company Wind turbine dome and method of assembly
US10167088B2 (en) 2015-10-19 2019-01-01 General Electric Company Crosswind performance aircraft engine spinner
US10519965B2 (en) * 2016-01-15 2019-12-31 General Electric Company Method and system for fiber reinforced composite panels
US10753277B2 (en) 2016-07-27 2020-08-25 Raytheon Technologies Corporation Inlet cap of an engine
US10703452B2 (en) * 2016-10-17 2020-07-07 General Electric Company Apparatus and system for propeller blade aft retention
US10746031B2 (en) 2017-07-18 2020-08-18 Rolls-Royce Corporation Annulus filler
US11078839B2 (en) * 2018-01-22 2021-08-03 Rolls-Royce Corporation Composite nosecone
US11254418B2 (en) * 2019-03-29 2022-02-22 Textron Innovations Inc. Tiltrotor controls shield
US11421538B2 (en) 2020-05-12 2022-08-23 Rolls-Royce Corporation Composite aerofoils
US11506083B2 (en) 2020-06-03 2022-11-22 Rolls-Royce Corporalion Composite liners for turbofan engines

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010030550A1 (de) * 2010-06-25 2011-12-29 Technische Universität Dresden Verbundbauteil mit einem Gewebe mit integrierten Profilen
DE102010030550B4 (de) * 2010-06-25 2017-06-22 Technische Universität Dresden Verbundbauteil mit einem Gewebe mit integrierten Profilen

Also Published As

Publication number Publication date
EP1136353A2 (en) 2001-09-26
DE60130824D1 (de) 2007-11-22
EP1136353A3 (en) 2003-01-15
US6358014B1 (en) 2002-03-19
JP2001349248A (ja) 2001-12-21
EP1136353B1 (en) 2007-10-10

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