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GB1245415A - Improvements in or relating to fluid flow machines - Google Patents

Improvements in or relating to fluid flow machines

Info

Publication number
GB1245415A
GB1245415A GB4356668A GB4356668A GB1245415A GB 1245415 A GB1245415 A GB 1245415A GB 4356668 A GB4356668 A GB 4356668A GB 4356668 A GB4356668 A GB 4356668A GB 1245415 A GB1245415 A GB 1245415A
Authority
GB
United Kingdom
Prior art keywords
casing
members
relating
sept
fluid flow
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
Application number
GB4356668A
Inventor
Anthony William Thomas Mottram
Eric William Stansbury
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
Priority to GB4356668A priority Critical patent/GB1245415A/en
Priority to FR6930773A priority patent/FR2018042A1/fr
Priority to DE19691946085 priority patent/DE1946085A1/en
Priority to CH1388669A priority patent/CH501828A/en
Publication of GB1245415A publication Critical patent/GB1245415A/en
Expired legal-status Critical Current

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)

Abstract

1,245,415. Turbines; axial-flow compressors. ROLLS-ROYCE Ltd. Sept.11, 1969 [Sept.13, 1968], No.43566/68. Headings F1C and F1T. [Also in Division F2] A gas turbine, compressor or like machine has its casing 11 surrounded by at least two helically wound metal strip members 24, 26 of sufficient strength to contain fragments in the event of rotor disintegration, the members 24, 26 being wound as a multi-start helix in a direction opposite to the direction of rotation Y of the rotor. The radially inner ends of the members 24, 26 may be welded to the casing 11 while the outer ends extend tangentially of the casing and are secured to fixed mounting structure.
GB4356668A 1968-09-13 1968-09-13 Improvements in or relating to fluid flow machines Expired GB1245415A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GB4356668A GB1245415A (en) 1968-09-13 1968-09-13 Improvements in or relating to fluid flow machines
FR6930773A FR2018042A1 (en) 1968-09-13 1969-09-10
DE19691946085 DE1946085A1 (en) 1968-09-13 1969-09-11 Flow machine, in particular gas turbine jet engine
CH1388669A CH501828A (en) 1968-09-13 1969-09-15 Gas turbine or compressor

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
GB1245415A true GB1245415A (en) 1971-09-08

Family

ID=10429328

Family Applications (1)

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

Country Status (4)

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

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3243887A1 (en) * 1981-12-21 1983-06-30 United Technologies Corp., 06101 Hartford, Conn. MANUFACTURING METHOD FOR A PARTICLE COLLECTOR, ESPECIALLY A PROTECTIVE HOUSING, PROTECTIVE COATING APPLICATION PROCESS AND PROTECTIVE DEVICE
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
US4746150A (en) * 1983-06-09 1988-05-24 Nitro Nobel Ab Joint for joining together two pipe ends
US4934899A (en) * 1981-12-21 1990-06-19 United Technologies Corporation Method for containing particles in a rotary machine
US5163809A (en) * 1991-04-29 1992-11-17 Pratt & Whitney Canada, Inc. Spiral wound containment ring
US6059523A (en) * 1998-04-20 2000-05-09 Pratt & Whitney Canada Inc. Containment system for containing blade burst
WO2009030197A1 (en) * 2007-09-07 2009-03-12 Mtu Aero Engines Gmbh Multilayer shielding ring for a flight driving mechanism
WO2012021203A1 (en) * 2010-08-12 2012-02-16 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
US10913256B2 (en) 2017-05-19 2021-02-09 General Electric Company Kevlar wrap removal from fan casing
EP4265889A1 (en) * 2022-04-21 2023-10-25 Pratt & Whitney Canada Corp. Multi-layered containment structure for a bladed rotor of a gas turbine engine

Families Citing this family (5)

* 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 (en) * 1977-10-11 1979-05-11 Snecma SAFETY DEVICE FOR AXIAL ROTATING MACHINE
FR2467977A1 (en) * 1979-10-19 1981-04-30 Snecma SAFETY DEVICE IN THE EVENT OF TURBOMACHINE ROTATING ELEMENT BREAK
FR2467978A1 (en) * 1979-10-23 1981-04-30 Snecma RETENTION DEVICE FOR A COMPRESSOR CASE OF A TURBOMACHINE
DE19704842A1 (en) * 1997-02-08 1998-08-13 Bayerische Motoren Werke Ag Safety housing for energy storage flywheel

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3243887A1 (en) * 1981-12-21 1983-06-30 United Technologies Corp., 06101 Hartford, Conn. MANUFACTURING METHOD FOR A PARTICLE COLLECTOR, ESPECIALLY A PROTECTIVE HOUSING, PROTECTIVE COATING APPLICATION PROCESS AND PROTECTIVE DEVICE
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
US4746150A (en) * 1983-06-09 1988-05-24 Nitro Nobel Ab Joint for joining together two pipe ends
US5163809A (en) * 1991-04-29 1992-11-17 Pratt & Whitney Canada, Inc. Spiral wound containment ring
US6059523A (en) * 1998-04-20 2000-05-09 Pratt & Whitney Canada Inc. Containment system for containing blade burst
WO2009030197A1 (en) * 2007-09-07 2009-03-12 Mtu Aero Engines Gmbh Multilayer shielding ring for a flight driving mechanism
WO2012021203A1 (en) * 2010-08-12 2012-02-16 General Electric Company Fragment containment assembly and method for adding a fragment containment assembly to a turbine
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
GB2513545A (en) * 2010-08-12 2014-11-05 Gen Electric Fragment containment assembly and method for adding a fragment containment assembly to a turbine
GB2513545B (en) * 2010-08-12 2017-10-11 Gen Electric 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
US10913256B2 (en) 2017-05-19 2021-02-09 General Electric Company Kevlar wrap removal from fan casing
EP4265889A1 (en) * 2022-04-21 2023-10-25 Pratt & Whitney Canada Corp. Multi-layered containment structure for a bladed rotor of a gas turbine engine
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
CH501828A (en) 1971-01-15
FR2018042A1 (en) 1970-05-29
DE1946085A1 (en) 1970-03-26

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