JP2002256807A5 - - Google Patents

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Publication number
JP2002256807A5
JP2002256807A5 JP2001388706A JP2001388706A JP2002256807A5 JP 2002256807 A5 JP2002256807 A5 JP 2002256807A5 JP 2001388706 A JP2001388706 A JP 2001388706A JP 2001388706 A JP2001388706 A JP 2001388706A JP 2002256807 A5 JP2002256807 A5 JP 2002256807A5
Authority
JP
Japan
Prior art keywords
bolt
passage
abutment member
nut
rotor disk
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.)
Granted
Application number
JP2001388706A
Other languages
English (en)
Japanese (ja)
Other versions
JP4100903B2 (ja
JP2002256807A (ja
Filing date
Publication date
Priority claimed from US09/747,873 external-priority patent/US6422812B1/en
Application filed filed Critical
Publication of JP2002256807A publication Critical patent/JP2002256807A/ja
Publication of JP2002256807A5 publication Critical patent/JP2002256807A5/ja
Application granted granted Critical
Publication of JP4100903B2 publication Critical patent/JP4100903B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

JP2001388706A 2000-12-22 2001-12-21 ロータディスク用のボルト継手及びその中の熱勾配を減少させる方法 Expired - Fee Related JP4100903B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/747873 2000-12-22
US09/747,873 US6422812B1 (en) 2000-12-22 2000-12-22 Bolted joint for rotor disks and method of reducing thermal gradients therein

Publications (3)

Publication Number Publication Date
JP2002256807A JP2002256807A (ja) 2002-09-11
JP2002256807A5 true JP2002256807A5 (enExample) 2005-05-19
JP4100903B2 JP4100903B2 (ja) 2008-06-11

Family

ID=25007019

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2001388706A Expired - Fee Related JP4100903B2 (ja) 2000-12-22 2001-12-21 ロータディスク用のボルト継手及びその中の熱勾配を減少させる方法

Country Status (6)

Country Link
US (1) US6422812B1 (enExample)
EP (1) EP1217231B1 (enExample)
JP (1) JP4100903B2 (enExample)
BR (1) BR0106233B1 (enExample)
CA (1) CA2364931C (enExample)
DE (1) DE60140170D1 (enExample)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8186939B2 (en) * 2009-08-25 2012-05-29 Pratt & Whitney Canada Corp. Turbine disc and retaining nut arrangement
FR2961250B1 (fr) * 2010-06-14 2012-07-20 Snecma Dispositif de refroidissement des alveoles d'un disque de rotor de turbomachine a l'aval du cone d'entrainement
US9004871B2 (en) * 2012-08-17 2015-04-14 General Electric Company Stacked wheel assembly for a turbine system and method of assembling
GB2505475B (en) * 2012-08-31 2015-11-18 Lappeenranta University Of Technology Compressing a laminated stack in an electrical machine
WO2014189589A2 (en) 2013-03-06 2014-11-27 Rolls-Royce North American Technologies, Inc. Gas turbine engine with soft mounted pre-swirl nozzle
US9951621B2 (en) * 2013-06-05 2018-04-24 Siemens Aktiengesellschaft Rotor disc with fluid removal channels to enhance life of spindle bolt
US9816387B2 (en) 2014-09-09 2017-11-14 United Technologies Corporation Attachment faces for clamped turbine stator of a gas turbine engine
JP6702542B2 (ja) * 2016-04-14 2020-06-03 株式会社東芝 カップリング構造およびカップリング構造用ナット
US11428104B2 (en) 2019-07-29 2022-08-30 Pratt & Whitney Canada Corp. Partition arrangement for gas turbine engine and method
CN115614324B (zh) * 2022-11-22 2023-05-05 中国航发四川燃气涡轮研究院 基于变截面螺栓连接的压气机转子多级轮盘连接结构

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH171459A (de) 1933-02-15 1934-08-31 Sulzer Ag Flanschverbindung, insbesondere für Hohlkörper, welche ein unter hoher Temperatur stehendes Druckmittel enthalten.
DE1218800B (de) * 1961-04-25 1966-06-08 M A N Turbo Ges Mit Beschraenk Gasturbine, insbesondere Kleingasturbine
US3561516A (en) * 1967-02-28 1971-02-09 Robert R Reddy Safety bolt
US4309145A (en) * 1978-10-30 1982-01-05 General Electric Company Cooling air seal
US4247248A (en) * 1978-12-20 1981-01-27 United Technologies Corporation Outer air seal support structure for gas turbine engine
US4887949A (en) * 1988-03-30 1989-12-19 United Technologies Corporation Bolt retention apparatus
US4991390A (en) * 1988-09-26 1991-02-12 Sundstrand Corporation Mounting and cooling turbine nozzle vanes
US5052891A (en) * 1990-03-12 1991-10-01 General Motors Corporation Connection for gas turbine engine rotor elements
US5072785A (en) * 1990-06-12 1991-12-17 United Technologies Corporation Convectively cooled bolt assembly
US5226788A (en) * 1991-12-23 1993-07-13 General Electric Company Turbine heat shield and bolt retainer assembly
US5350278A (en) * 1993-06-28 1994-09-27 The United States Of America As Represented By The Secretary Of The Air Force Joining means for rotor discs
US5511941A (en) * 1995-01-30 1996-04-30 Brandon; Ronald E. Steam turbine shell disassembly method
US5848874A (en) * 1997-05-13 1998-12-15 United Technologies Corporation Gas turbine stator vane assembly

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