JP2001349248A5 - - Google Patents

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Publication number
JP2001349248A5
JP2001349248A5 JP2001083943A JP2001083943A JP2001349248A5 JP 2001349248 A5 JP2001349248 A5 JP 2001349248A5 JP 2001083943 A JP2001083943 A JP 2001083943A JP 2001083943 A JP2001083943 A JP 2001083943A JP 2001349248 A5 JP2001349248 A5 JP 2001349248A5
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JP
Japan
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.)
Pending
Application number
JP2001083943A
Other versions
JP2001349248A (ja
Filing date
Publication date
Priority claimed from US09/535,923 external-priority patent/US6358014B1/en
Application filed filed Critical
Publication of JP2001349248A publication Critical patent/JP2001349248A/ja
Publication of JP2001349248A5 publication Critical patent/JP2001349248A5/ja
Pending legal-status Critical Current

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JP2001083943A 2000-03-24 2001-03-23 複合スピナ及びその製造方法 Pending JP2001349248A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/535,923 US6358014B1 (en) 2000-03-24 2000-03-24 Composite spinner and method of making the same
US09/535923 2000-03-24

Publications (2)

Publication Number Publication Date
JP2001349248A JP2001349248A (ja) 2001-12-21
JP2001349248A5 true JP2001349248A5 (ja) 2008-05-08

Family

ID=24136357

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2001083943A Pending JP2001349248A (ja) 2000-03-24 2001-03-23 複合スピナ及びその製造方法

Country Status (4)

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

Families Citing this family (46)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6887043B2 (en) * 2003-03-28 2005-05-03 General Electric Company Methods and apparatus for assembling gas turbine engines
US8001764B2 (en) * 2004-09-17 2011-08-23 Aurora Flight Sciences Corporation Vibration isolation engine mount system and method for ducted fans
US7506837B2 (en) * 2004-09-17 2009-03-24 Aurora Flight Sciences Corporation Inbound transition control for a tail-sitting vertical take off and landing aircraft
US7364115B2 (en) * 2004-09-17 2008-04-29 Aurora Flight Sciences Corporation System and method for controlling engine RPM of a ducted fan aircraft
US20070221783A1 (en) * 2004-09-17 2007-09-27 Robert Parks Adaptive landing gear
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
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
PL2014551T3 (pl) * 2007-07-09 2010-06-30 Agusta Spa Urządzenie i sposób ochrony części składowej samolotu przed zderzeniem z obiektami latającymi
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
DE102010030550B4 (de) * 2010-06-25 2017-06-22 Technische Universität Dresden Verbundbauteil mit einem Gewebe mit integrierten Profilen
US9587645B2 (en) 2010-09-30 2017-03-07 Pratt & Whitney Canada Corp. Airfoil blade
US9429029B2 (en) 2010-09-30 2016-08-30 Pratt & Whitney Canada Corp. Gas turbine blade and method of protecting same
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
WO2014120123A2 (en) * 2013-01-29 2014-08-07 United 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
CA2917916A1 (en) * 2013-07-09 2015-02-05 United Technologies Corporation Plated polymer nosecone
WO2015006433A2 (en) 2013-07-09 2015-01-15 United Technologies Corporation Plated polymer fan
WO2015006421A1 (en) 2013-07-09 2015-01-15 United Technologies Corporation Metal-encapsulated polymeric article
EP3019723A4 (en) 2013-07-09 2017-05-10 United Technologies Corporation Plated polymer compressor
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
EP2915953B1 (en) 2014-03-03 2019-01-16 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

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB251753A (en) * 1925-04-14 1926-05-13 Armstrong Whitworth Co Eng Improvements in air screws
GB547433A (en) * 1941-02-25 1942-08-27 Robert Henry Coverley Improvements in or relating to spinners for airscrew hubs
US4147822A (en) * 1976-06-24 1979-04-03 Mcdonnell Douglas Corporation Composite structure and process and apparatus for making the same
US4471609A (en) * 1982-08-23 1984-09-18 The Boeing Company Apparatus and method for minimizing engine backbone bending
GB2160467B (en) * 1984-06-22 1987-09-23 Rolls Royce Moulding of composite materials
US4699568A (en) * 1984-06-25 1987-10-13 Hartzell Propeller Inc. Aircraft propeller with improved spinner assembly
US4957415A (en) 1986-04-14 1990-09-18 United Technologies Corporation Polyester composite propeller spinner and method of making same
FR2612950B1 (fr) * 1987-03-25 1989-06-09 Aerospatiale Procede de fabrication d'elements d'armature composites tisses en trois dimensions, machine pour sa mise en oeuvre et produit obtenu
DE3719098A1 (de) * 1987-06-06 1988-12-22 Mtu Muenchen Gmbh Nasenhaube aus faserverbundwerkstoffen
US5182906A (en) 1990-10-22 1993-02-02 General Electric Company Hybrid spinner nose configuration in a gas turbine engine having a bypass duct
US5252160A (en) * 1990-11-15 1993-10-12 Auto Air Composites, Inc. Method of manufacturing a metal/composite spinner cone
US5149251A (en) * 1990-11-15 1992-09-22 Auto Air Composites, Inc. Metal/composite spinner cone
US5279892A (en) 1992-06-26 1994-01-18 General Electric Company Composite airfoil with woven insert
US5833435A (en) * 1996-12-24 1998-11-10 United Technologies Corporation Inlet nose cone assembly and method for repairing the assembly

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