JPS5716205A - Partly segmented support/seal construction body for guide wing array of gas turbine engine - Google Patents

Partly segmented support/seal construction body for guide wing array of gas turbine engine

Info

Publication number
JPS5716205A
JPS5716205A JP7433881A JP7433881A JPS5716205A JP S5716205 A JPS5716205 A JP S5716205A JP 7433881 A JP7433881 A JP 7433881A JP 7433881 A JP7433881 A JP 7433881A JP S5716205 A JPS5716205 A JP S5716205A
Authority
JP
Japan
Prior art keywords
gas turbine
turbine engine
construction body
seal construction
guide wing
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
JP7433881A
Other languages
English (en)
Japanese (ja)
Other versions
JPS6153521B2 (enrdf_load_stackoverflow
Inventor
Deii Baakunaa Hoosuto
Shii Manente Jiyunia Jiyozefu
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.)
Avco Corp
Original Assignee
Avco Corp
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 Avco Corp filed Critical Avco Corp
Publication of JPS5716205A publication Critical patent/JPS5716205A/ja
Publication of JPS6153521B2 publication Critical patent/JPS6153521B2/ja
Granted 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
JP7433881A 1980-05-19 1981-05-19 Partly segmented support/seal construction body for guide wing array of gas turbine engine Granted JPS5716205A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US15104780A 1980-05-19 1980-05-19

Publications (2)

Publication Number Publication Date
JPS5716205A true JPS5716205A (en) 1982-01-27
JPS6153521B2 JPS6153521B2 (enrdf_load_stackoverflow) 1986-11-18

Family

ID=22537110

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7433881A Granted JPS5716205A (en) 1980-05-19 1981-05-19 Partly segmented support/seal construction body for guide wing array of gas turbine engine

Country Status (8)

Country Link
JP (1) JPS5716205A (enrdf_load_stackoverflow)
BR (1) BR8102869A (enrdf_load_stackoverflow)
CA (1) CA1135195A (enrdf_load_stackoverflow)
DE (1) DE3108319C2 (enrdf_load_stackoverflow)
FR (1) FR2482657A1 (enrdf_load_stackoverflow)
GB (1) GB2076069B (enrdf_load_stackoverflow)
IT (1) IT1137478B (enrdf_load_stackoverflow)
SE (1) SE448757B (enrdf_load_stackoverflow)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3631271B2 (ja) * 1993-11-19 2005-03-23 ユナイテッド テクノロジーズ コーポレイション インナーシュラウド一体型ステータベーン構造
US6722848B1 (en) * 2002-10-31 2004-04-20 General Electric Company Turbine nozzle retention apparatus at the carrier horizontal joint face
GB2434182A (en) * 2006-01-11 2007-07-18 Rolls Royce Plc Guide vane arrangement for a gas turbine engine

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB589541A (en) * 1941-09-22 1947-06-24 Hayne Constant Improvements in axial flow turbines, compressors and the like
FR954577A (enrdf_load_stackoverflow) * 1947-09-02 1950-01-03
GB816288A (en) * 1957-03-25 1959-07-08 Gen Motors Corp Improvements relating to labyrinth seals in turbines or compressors
US3552753A (en) * 1968-06-26 1971-01-05 Westinghouse Electric Corp High efficiency static seal assembly
US3529906A (en) * 1968-10-30 1970-09-22 Westinghouse Electric Corp Static seal structure
US3647311A (en) * 1970-04-23 1972-03-07 Westinghouse Electric Corp Turbine interstage seal assembly
US3829233A (en) * 1973-06-27 1974-08-13 Westinghouse Electric Corp Turbine diaphragm seal structure
US4011718A (en) * 1975-08-01 1977-03-15 United Technologies Corporation Gas turbine construction
SE398659B (sv) * 1976-05-05 1978-01-09 Stal Laval Turbin Ab Tetningsanordning i en gasturbin

Also Published As

Publication number Publication date
GB2076069A (en) 1981-11-25
DE3108319A1 (de) 1982-01-28
SE448757B (sv) 1987-03-16
JPS6153521B2 (enrdf_load_stackoverflow) 1986-11-18
FR2482657A1 (fr) 1981-11-20
DE3108319C2 (de) 1986-12-18
IT1137478B (it) 1986-09-10
SE8101236L (sv) 1981-11-20
GB2076069B (en) 1983-12-21
IT8121699A0 (it) 1981-05-14
CA1135195A (en) 1982-11-09
FR2482657B1 (enrdf_load_stackoverflow) 1985-03-22
BR8102869A (pt) 1982-02-02

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