CH501828A - Turbine à gaz ou compresseur - Google Patents

Turbine à gaz ou compresseur

Info

Publication number
CH501828A
CH501828A CH1388669A CH1388669A CH501828A CH 501828 A CH501828 A CH 501828A CH 1388669 A CH1388669 A CH 1388669A CH 1388669 A CH1388669 A CH 1388669A CH 501828 A CH501828 A CH 501828A
Authority
CH
Switzerland
Prior art keywords
compressor
gas turbine
turbine
gas
Prior art date
Application number
CH1388669A
Other languages
English (en)
Inventor
Thomas Mottram Antony William
William Stansbury Eric
Original Assignee
Rolls Royce
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 filed Critical Rolls Royce
Publication of CH501828A publication Critical patent/CH501828A/fr

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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CH1388669A 1968-09-13 1969-09-15 Turbine à gaz ou compresseur CH501828A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4356668A GB1245415A (en) 1968-09-13 1968-09-13 Improvements in or relating to fluid flow machines

Publications (1)

Publication Number Publication Date
CH501828A true CH501828A (fr) 1971-01-15

Family

ID=10429328

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1388669A CH501828A (fr) 1968-09-13 1969-09-15 Turbine à gaz ou compresseur

Country Status (4)

Country Link
CH (1) CH501828A (fr)
DE (1) DE1946085A1 (fr)
FR (1) FR2018042A1 (fr)
GB (1) GB1245415A (fr)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1291939A (en) * 1970-11-30 1972-10-04 Rolls Royce Flame shield for a gas turbine engine
FR2406074A1 (fr) * 1977-10-11 1979-05-11 Snecma Dispositif de securite pour machine tournante axiale
FR2467977A1 (fr) * 1979-10-19 1981-04-30 Snecma Dispositif de securite en cas de rupture d'element rotatif de turbomachine
FR2467978A1 (fr) * 1979-10-23 1981-04-30 Snecma Dispositif de retention pour carter de compresseur d'une turbomachine
US4598449A (en) * 1981-12-21 1986-07-08 United Technologies Corporation Beam for a containment structure
US4718818A (en) * 1981-12-21 1988-01-12 United Technologies Corporation Containment structure
US4934899A (en) * 1981-12-21 1990-06-19 United Technologies Corporation Method for containing particles in a rotary machine
US4490092A (en) * 1981-12-21 1984-12-25 United Technologies Corporation Containment structure
SE436399B (sv) * 1983-06-09 1984-12-10 Nitro Nobel Ab Skarvforband for sammanfogning av tva rorendar
US5163809A (en) * 1991-04-29 1992-11-17 Pratt & Whitney Canada, Inc. Spiral wound containment ring
DE19704842A1 (de) * 1997-02-08 1998-08-13 Bayerische Motoren Werke Ag Sicherheitsgehäuse für einen Rotationsenergiespeicher
US6059523A (en) * 1998-04-20 2000-05-09 Pratt & Whitney Canada Inc. Containment system for containing blade burst
DE102007042767A1 (de) * 2007-09-07 2009-03-12 Mtu Aero Engines Gmbh Mehrschichtiger Abschirmungsring für einen Flugantrieb
US8858156B2 (en) * 2010-08-12 2014-10-14 General Electric Company Fragment containment assembly and method for adding a fragment containment assembly to a turbine
US9109462B2 (en) 2011-12-15 2015-08-18 United Technologies Corporation Energy-absorbing fan case for a gas turbine engine
PL421648A1 (pl) 2017-05-19 2018-12-03 General Electric Company Usuwanie owinięcia z kevlaru z obudowy wentylatora
US20230340890A1 (en) * 2022-04-21 2023-10-26 Pratt & Whitney Canada Corp. Multi-layered containment structure for a bladed rotor of a gas turbine engine

Also Published As

Publication number Publication date
GB1245415A (en) 1971-09-08
DE1946085A1 (de) 1970-03-26
FR2018042A1 (fr) 1970-05-29

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Legal Events

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