NO123552B - - Google Patents

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Publication number
NO123552B
NO123552B NO5037/68A NO503768A NO123552B NO 123552 B NO123552 B NO 123552B NO 5037/68 A NO5037/68 A NO 5037/68A NO 503768 A NO503768 A NO 503768A NO 123552 B NO123552 B NO 123552B
Authority
NO
Norway
Prior art keywords
segments
segment
screen
turbine
inner edge
Prior art date
Application number
NO5037/68A
Other languages
English (en)
Norwegian (no)
Inventor
T Westrum
Original Assignee
Kongsberg Vapenfab As
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 Kongsberg Vapenfab As filed Critical Kongsberg Vapenfab As
Priority to NO5037/68A priority Critical patent/NO123552B/no
Priority to DE19691960693 priority patent/DE1960693C/de
Priority to US885139A priority patent/US3661477A/en
Priority to JP44101580A priority patent/JPS4825683B1/ja
Priority to GB61557/69A priority patent/GB1294675A/en
Publication of NO123552B publication Critical patent/NO123552B/no

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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/26Double casings; Measures against temperature strain in casings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/24Heat or noise insulation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2230/00Manufacture
    • F05B2230/60Assembly methods
    • F05B2230/604Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins
    • F05B2230/606Assembly methods using positioning or alignment devices for aligning or centering, e.g. pins using maintaining alignment while permitting differential dilatation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/60Assembly methods
    • F05D2230/64Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F05D2230/642Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
NO5037/68A 1968-12-17 1968-12-17 NO123552B (de)

Priority Applications (5)

Application Number Priority Date Filing Date Title
NO5037/68A NO123552B (de) 1968-12-17 1968-12-17
DE19691960693 DE1960693C (de) 1968-12-17 1969-12-03 Einrichtung zur Verringerung des Wärmedurchgangs zwischen dem Radialturbinen- und dem Radialverdichterschaufelrad einer Gasturbinenanlage
US885139A US3661477A (en) 1968-12-17 1969-12-15 Heat shield
JP44101580A JPS4825683B1 (de) 1968-12-17 1969-12-17
GB61557/69A GB1294675A (en) 1968-12-17 1969-12-17 Heat shield

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
NO5037/68A NO123552B (de) 1968-12-17 1968-12-17

Publications (1)

Publication Number Publication Date
NO123552B true NO123552B (de) 1971-12-06

Family

ID=19880777

Family Applications (1)

Application Number Title Priority Date Filing Date
NO5037/68A NO123552B (de) 1968-12-17 1968-12-17

Country Status (4)

Country Link
US (1) US3661477A (de)
JP (1) JPS4825683B1 (de)
GB (1) GB1294675A (de)
NO (1) NO123552B (de)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4688988A (en) * 1984-12-17 1987-08-25 United Technologies Corporation Coolable stator assembly for a gas turbine engine
US4987736A (en) * 1988-12-14 1991-01-29 General Electric Company Lightweight gas turbine engine frame with free-floating heat shield
US5655876A (en) * 1996-01-02 1997-08-12 General Electric Company Low leakage turbine nozzle
DE19623300A1 (de) * 1996-06-11 1997-12-18 Siemens Ag Hitzeschildanordnung, insbesondere für Strukturteile von Gasturbinenanlagen, mit geschichtetem Aufbau
KR101091892B1 (ko) * 2004-07-16 2011-12-08 삼성테크윈 주식회사 열 차단 부재 및, 열 차단 부재를 구비하는 실링 조립체
US7631497B2 (en) * 2005-04-21 2009-12-15 Borgwarner Inc. Turbine heat shield with ribs
DE102007057309A1 (de) * 2007-11-28 2009-06-10 Continental Automotive Gmbh Hitzeschild und Turbolader mit einem Hitzeschild
EP2194234A1 (de) * 2008-12-03 2010-06-09 Siemens Aktiengesellschaft Wärmeisolationsring zur passiven Spaltkontrolle in einer Gasturbine

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2296701A (en) * 1939-01-21 1942-09-22 Bristol Aeroplane Co Ltd Gas turbine
DE726510C (de) * 1940-01-25 1942-10-15 Aeg Trag- und Zentriereinrichtung fuer in der Teilfuge des Gehaeuses unterteilte Leitraeder von Dampf- oder Gasturbinen
GB542197A (en) * 1940-01-25 1941-12-30 British Thomson Houston Co Ltd Improved supporting arrangement for elastic fluid turbine diaphragms
US2440069A (en) * 1944-08-26 1948-04-20 Gen Electric High-temperature elastic fluid turbine
GB679916A (en) * 1949-04-29 1952-09-24 Geoffrey Bertram Robert Feilde Improvements in gas turbines
US3352105A (en) * 1964-12-14 1967-11-14 United Aircraft Canada Firewall attachment
US3263424A (en) * 1965-03-25 1966-08-02 Birmann Rudolph Turbine-compressor unit

Also Published As

Publication number Publication date
JPS4825683B1 (de) 1973-07-31
DE1960693B2 (de) 1973-02-15
US3661477A (en) 1972-05-09
GB1294675A (en) 1972-11-01
DE1960693A1 (de) 1970-07-02

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