JPS5026904A - - Google Patents

Info

Publication number
JPS5026904A
JPS5026904A JP5217174A JP5217174A JPS5026904A JP S5026904 A JPS5026904 A JP S5026904A JP 5217174 A JP5217174 A JP 5217174A JP 5217174 A JP5217174 A JP 5217174A JP S5026904 A JPS5026904 A JP S5026904A
Authority
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
JP5217174A
Other languages
Japanese (ja)
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 filed Critical
Publication of JPS5026904A publication Critical patent/JPS5026904A/ja
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • F01D11/14Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
    • F01D11/16Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means
    • F01D11/18Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing by self-adjusting means using stator or rotor components with predetermined thermal response, e.g. selective insulation, thermal inertia, differential expansion

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)
JP5217174A 1973-05-12 1974-05-10 Pending JPS5026904A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2271173 1973-05-12

Publications (1)

Publication Number Publication Date
JPS5026904A true JPS5026904A (en) 1975-03-20

Family

ID=10183878

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5217174A Pending JPS5026904A (en) 1973-05-12 1974-05-10

Country Status (3)

Country Link
JP (1) JPS5026904A (en)
DE (1) DE2422533A1 (en)
FR (1) FR2228967A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS55500212A (en) * 1978-05-01 1980-04-10
JPS58500489A (en) * 1981-04-10 1983-03-31 キヤタピラ− トラクタ− コンパニ− floating inflation control ring

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3986720A (en) * 1975-04-14 1976-10-19 General Electric Company Turbine shroud structure
FR2455674A1 (en) * 1979-05-02 1980-11-28 Snecma SEALING DEVICE BETWEEN TWO TURBOMACHINE ELEMENTS
GB2087979B (en) * 1980-11-22 1984-02-22 Rolls Royce Gas turbine engine blade tip seal
FR2548733B1 (en) * 1983-07-07 1987-07-10 Snecma DEVICE FOR SEALING MOBILE BLADES OF A TURBOMACHINE
FR2559834B1 (en) * 1984-02-22 1988-04-08 Snecma TURBINE RING
GB2165590B (en) * 1984-10-09 1988-05-05 Rolls Royce Improvements in or relating to rotor tip clearance control devices
FR2577281B1 (en) * 1985-02-13 1987-03-20 Snecma TURBOMACHINE HOUSING ASSOCIATED WITH A DEVICE FOR ADJUSTING THE GAP BETWEEN MOBILE BLADES AND HOUSING
FR2580033A1 (en) * 1985-04-03 1986-10-10 Snecma Elastically suspended turbine ring for a turbine machine
DE69002064T2 (en) * 1989-01-09 1993-12-23 Northern Eng Ind Fastening and arrangement of segment-shaped elements in turbomachinery.
GB8903000D0 (en) * 1989-02-10 1989-03-30 Rolls Royce Plc A blade tip clearance control arrangement for a gas turbine engine
DE10251468A1 (en) * 2002-11-05 2004-05-19 Rolls-Royce Deutschland Ltd & Co Kg Fastening for compressor and turbine shroud ring segment on housing via bearing element with variable shape dependent upon temperature differentials, to vary relative radial distance
FR3044411B1 (en) 2015-11-27 2018-10-26 Safran Aircraft Engines TURBUMACHINE MODULE OR COMBUSTION CHAMBER TEST BENCH

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS55500212A (en) * 1978-05-01 1980-04-10
JPS58500489A (en) * 1981-04-10 1983-03-31 キヤタピラ− トラクタ− コンパニ− floating inflation control ring
JPH0423087B2 (en) * 1981-04-10 1992-04-21 Caterpillar Inc

Also Published As

Publication number Publication date
DE2422533A1 (en) 1974-12-12
FR2228967A1 (en) 1974-12-06

Similar Documents

Publication Publication Date Title
AU476761B2 (en)
AU465372B2 (en)
AR201235Q (en)
AU474593B2 (en)
AU474511B2 (en)
AU474838B2 (en)
AU471343B2 (en)
AU465453B2 (en)
AU465434B2 (en)
JPS5026904A (en)
AU450229B2 (en)
AU476714B2 (en)
AU472848B2 (en)
AU466283B2 (en)
AU476696B2 (en)
AU477823B2 (en)
AU477824B2 (en)
AU447540B2 (en)
AU471461B2 (en)
AU461342B2 (en)
AU476873B1 (en)
AU1891376A (en)
BG19245A1 (en)
AU470923A (en)
BG19016A1 (en)