IT1186038B - Complesso di statore raffreddabile per una macchina rotativa - Google Patents

Complesso di statore raffreddabile per una macchina rotativa

Info

Publication number
IT1186038B
IT1186038B IT8522685A IT2268585A IT1186038B IT 1186038 B IT1186038 B IT 1186038B IT 8522685 A IT8522685 A IT 8522685A IT 2268585 A IT2268585 A IT 2268585A IT 1186038 B IT1186038 B IT 1186038B
Authority
IT
Italy
Prior art keywords
rotary machine
cooling stator
stator complex
complex
cooling
Prior art date
Application number
IT8522685A
Other languages
English (en)
Other versions
IT8522685A0 (it
Inventor
Robert H Weidner
Original Assignee
United Technologies 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 United Technologies Corp filed Critical United Technologies Corp
Publication of IT8522685A0 publication Critical patent/IT8522685A0/it
Application granted granted Critical
Publication of IT1186038B publication Critical patent/IT1186038B/it

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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/14—Casings modified therefor
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
IT8522685A 1984-12-05 1985-10-31 Complesso di statore raffreddabile per una macchina rotativa IT1186038B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/678,518 US4642024A (en) 1984-12-05 1984-12-05 Coolable stator assembly for a rotary machine

Publications (2)

Publication Number Publication Date
IT8522685A0 IT8522685A0 (it) 1985-10-31
IT1186038B true IT1186038B (it) 1987-11-18

Family

ID=24723129

Family Applications (1)

Application Number Title Priority Date Filing Date
IT8522685A IT1186038B (it) 1984-12-05 1985-10-31 Complesso di statore raffreddabile per una macchina rotativa

Country Status (10)

Country Link
US (1) US4642024A (it)
JP (1) JPH0756202B2 (it)
CA (1) CA1212047A (it)
CH (1) CH681243A5 (it)
DE (1) DE3537043C2 (it)
FR (1) FR2574115B1 (it)
GB (1) GB2168110B (it)
IL (1) IL76659A (it)
IT (1) IT1186038B (it)
SE (1) SE458545B (it)

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US8439629B2 (en) * 2007-03-01 2013-05-14 United Technologies Corporation Blade outer air seal
US8123466B2 (en) * 2007-03-01 2012-02-28 United Technologies Corporation Blade outer air seal
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US10145308B2 (en) * 2014-02-10 2018-12-04 United Technologies Corporation Gas turbine engine ring seal
US10590785B2 (en) * 2014-09-09 2020-03-17 United Technologies Corporation Beveled coverplate
US10301956B2 (en) 2014-09-25 2019-05-28 United Technologies Corporation Seal assembly for sealing an axial gap between components
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US10385718B2 (en) 2015-06-29 2019-08-20 Rolls-Royce North American Technologies, Inc. Turbine shroud segment with side perimeter seal
US10047624B2 (en) * 2015-06-29 2018-08-14 Rolls-Royce North American Technologies Inc. Turbine shroud segment with flange-facing perimeter seal
US10094234B2 (en) 2015-06-29 2018-10-09 Rolls-Royce North America Technologies Inc. Turbine shroud segment with buffer air seal system
US10196919B2 (en) 2015-06-29 2019-02-05 Rolls-Royce North American Technologies Inc. Turbine shroud segment with load distribution springs
US10767863B2 (en) * 2015-07-22 2020-09-08 Rolls-Royce North American Technologies, Inc. Combustor tile with monolithic inserts
JP6546481B2 (ja) * 2015-08-31 2019-07-17 川崎重工業株式会社 排気ディフューザ
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US10329941B2 (en) 2016-05-06 2019-06-25 United Technologies Corporation Impingement manifold
DE102016217320A1 (de) * 2016-09-12 2018-03-15 Siemens Aktiengesellschaft Gasturbine mit getrennter Kühlung für Turbine und Abgasgehäuse
US10533446B2 (en) * 2017-05-15 2020-01-14 United Technologies Corporation Alternative W-seal groove arrangement
US11903101B2 (en) 2019-12-13 2024-02-13 Goodrich Corporation Internal heating trace assembly

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Also Published As

Publication number Publication date
DE3537043A1 (de) 1986-06-05
IL76659A0 (en) 1986-02-28
DE3537043C2 (de) 1997-06-19
GB8524590D0 (en) 1985-11-06
US4642024A (en) 1987-02-10
GB2168110B (en) 1988-06-08
IT8522685A0 (it) 1985-10-31
JPS61135904A (ja) 1986-06-23
CH681243A5 (it) 1993-02-15
CA1212047A (en) 1986-09-30
FR2574115A1 (fr) 1986-06-06
FR2574115B1 (fr) 1992-04-24
SE8505155L (sv) 1986-06-06
JPH0756202B2 (ja) 1995-06-14
GB2168110A (en) 1986-06-11
SE8505155D0 (sv) 1985-10-31
IL76659A (en) 1994-11-28
SE458545B (sv) 1989-04-10

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