DE602005004072D1 - Sicherungsanordnung - Google Patents

Sicherungsanordnung

Info

Publication number
DE602005004072D1
DE602005004072D1 DE602005004072T DE602005004072T DE602005004072D1 DE 602005004072 D1 DE602005004072 D1 DE 602005004072D1 DE 602005004072 T DE602005004072 T DE 602005004072T DE 602005004072 T DE602005004072 T DE 602005004072T DE 602005004072 D1 DE602005004072 D1 DE 602005004072D1
Authority
DE
Germany
Prior art keywords
fuse assembly
fuse
assembly
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.)
Active
Application number
DE602005004072T
Other languages
English (en)
Other versions
DE602005004072T2 (de
Inventor
Kamaljit Kaur Dhaliwal
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of DE602005004072D1 publication Critical patent/DE602005004072D1/de
Application granted granted Critical
Publication of DE602005004072T2 publication Critical patent/DE602005004072T2/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/20—Actively adjusting tip-clearance
    • F01D11/24—Actively adjusting tip-clearance by selectively cooling-heating stator or rotor components
    • 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
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/12—Cooling

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Clamps And Clips (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DE602005004072T 2004-06-23 2005-05-25 Sicherungsanordnung Active DE602005004072T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB0414043.0A GB0414043D0 (en) 2004-06-23 2004-06-23 Securing arrangement
GB0414043 2004-06-23

Publications (2)

Publication Number Publication Date
DE602005004072D1 true DE602005004072D1 (de) 2008-02-14
DE602005004072T2 DE602005004072T2 (de) 2008-04-10

Family

ID=32800016

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005004072T Active DE602005004072T2 (de) 2004-06-23 2005-05-25 Sicherungsanordnung

Country Status (4)

Country Link
US (1) US7857585B2 (de)
EP (1) EP1609954B1 (de)
DE (1) DE602005004072T2 (de)
GB (1) GB0414043D0 (de)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060032974A1 (en) * 2004-08-16 2006-02-16 Honeywell International Inc. Modular installation kit for auxiliary power unit
EP1701095B1 (de) * 2005-02-07 2012-01-18 Siemens Aktiengesellschaft Hitzeschild
US7540157B2 (en) * 2005-06-14 2009-06-02 Pratt & Whitney Canada Corp. Internally mounted fuel manifold with support pins
US7805924B2 (en) * 2006-11-30 2010-10-05 United Technologies Corporation Thermally decoupled mixer
GB2449477B (en) * 2007-05-24 2009-05-13 Rolls Royce Plc A duct installation
GB2469490B (en) 2009-04-16 2012-03-07 Rolls Royce Plc Turbine casing cooling
US8473242B1 (en) 2010-04-12 2013-06-25 Jason R. Hubbard System and method for race participant tracking and reporting of associated data
GB201013723D0 (en) 2010-08-17 2010-09-29 Rolls Royce Plc Manifold mounting arrangement
US9869196B2 (en) 2014-06-24 2018-01-16 General Electric Company Gas turbine engine spring mounted manifold
US20170114667A1 (en) * 2015-10-23 2017-04-27 General Electric Company Active clearance control with integral double wall heat shielding
US10458281B2 (en) 2017-06-12 2019-10-29 United Technologies Corporation Resilient mounting assembly for a turbine engine
US10941706B2 (en) 2018-02-13 2021-03-09 General Electric Company Closed cycle heat engine for a gas turbine engine
US11143104B2 (en) 2018-02-20 2021-10-12 General Electric Company Thermal management system
US11015534B2 (en) 2018-11-28 2021-05-25 General Electric Company Thermal management system
US11118473B2 (en) * 2019-04-11 2021-09-14 Raytheon Technologies Corporation Vibration isolator assembly
FR3099799B1 (fr) * 2019-08-09 2021-12-03 Safran Aircraft Engines Ensemble pour une turbine de turbomachine
FR3112808B1 (fr) * 2020-07-22 2022-10-07 Safran Aircraft Engines Mexico Sa De C V Procédé de montage de supports externes sur un carter de turbine
US11713715B2 (en) 2021-06-30 2023-08-01 Unison Industries, Llc Additive heat exchanger and method of forming

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB726072A (en) 1953-01-29 1955-03-16 Parsons & Marine Eng Turbine Improvements in and relating to elastic fluid turbines
US2878041A (en) 1954-09-30 1959-03-17 James C Hobbs Clamped flange joint with means for maintaining a fluid seal under varying temperature conditions
US3027715A (en) * 1956-10-22 1962-04-03 Morris Victor Sidney Radially free support for combustion chamber fuel manifold
US4023919A (en) * 1974-12-19 1977-05-17 General Electric Company Thermal actuated valve for clearance control
US4715565A (en) * 1986-05-27 1987-12-29 Hughes Aircraft Company Clamping connection assembly for spacecraft
FR2604750B1 (fr) * 1986-10-01 1988-12-02 Snecma Turbomachine munie d'un dispositif de commande automatique des debits de ventilation de turbine
US4859142A (en) * 1988-02-01 1989-08-22 United Technologies Corporation Turbine clearance control duct arrangement
US4840026A (en) 1988-02-24 1989-06-20 The United States Of America As Represented By The Secretary Of The Air Force Band clamp apparatus
US4826397A (en) * 1988-06-29 1989-05-02 United Technologies Corporation Stator assembly for a gas turbine engine
US5088279A (en) 1990-03-30 1992-02-18 General Electric Company Duct support assembly
US5127224A (en) * 1991-03-25 1992-07-07 United Technologies Corporation Spray-ring mounting assembly
US5205115A (en) * 1991-11-04 1993-04-27 General Electric Company Gas turbine engine case counterflow thermal control
US5205708A (en) * 1992-02-07 1993-04-27 General Electric Company High pressure turbine component interference fit up
US5271218A (en) * 1992-05-28 1993-12-21 Gerneral Electric Company Off-engine mounting system for steam and gaseous fuel manifolds of marine and industrial gas turbine engines
US5277382A (en) * 1992-10-13 1994-01-11 General Electric Company Aircraft engine forward mount
DE4432073C2 (de) 1994-09-09 2002-11-28 Abb Turbo Systems Ag Baden Vorrichtung zur Befestigung von Turboladern
US6357220B1 (en) * 1998-12-22 2002-03-19 United Technologies Corporation Gearbox accessory mount
DE10150527A1 (de) 2000-11-27 2002-06-20 Abb Turbo Systems Ag Baden Stützfuss für einen Turbolader
US6487860B2 (en) * 2000-12-08 2002-12-03 General Electric Company Turbine engine fuel supply system
FR2828167B1 (fr) * 2001-07-31 2003-11-21 Airbus France Dispositif d'accrochage d'un moteur sur un aeronef

Also Published As

Publication number Publication date
EP1609954B1 (de) 2008-01-02
US20060016173A1 (en) 2006-01-26
US7857585B2 (en) 2010-12-28
EP1609954A1 (de) 2005-12-28
GB0414043D0 (en) 2004-07-28
DE602005004072T2 (de) 2008-04-10

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition