GB802166A - Improvements in counter-flow heat exchangers for gas turbines and gas turbine installations incorporating the same - Google Patents

Improvements in counter-flow heat exchangers for gas turbines and gas turbine installations incorporating the same

Info

Publication number
GB802166A
GB802166A GB26010/55A GB2601055A GB802166A GB 802166 A GB802166 A GB 802166A GB 26010/55 A GB26010/55 A GB 26010/55A GB 2601055 A GB2601055 A GB 2601055A GB 802166 A GB802166 A GB 802166A
Authority
GB
United Kingdom
Prior art keywords
gas
counter
same
heat exchangers
turbine
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
GB26010/55A
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.)
Henschel and Sohn GmbH
Original Assignee
Henschel and Sohn GmbH
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 Henschel and Sohn GmbH filed Critical Henschel and Sohn GmbH
Publication of GB802166A publication Critical patent/GB802166A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, 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
    • F02C7/08—Heating air supply before combustion, e.g. by exhaust gases

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

802,166. Gas-turbine plant. HENSCHEL & SOHN G.m.b.H. Sept. 12, 1955 [Sept. 10, 1954], No. 26010/55. Class 110 (3). [Also in Group XIII] In a gas turbine installation, a tubular air preheater 23 (see Group XIII) is mounted vertically above the exhaust outlet 29 of the turbine 28, and the air supply pipe 22 from the compressor 20 to the heat exchanger and also the lead-off pipe 24 for conducting heated air from the heat exchanger to the combustion chamber 25 extend at right angles to the vertical axis of the heat exchanger. In the form shown, the combustion chamber is located vertically above the inlet connecting pipe 27 of the turbine.
GB26010/55A 1954-09-10 1955-09-12 Improvements in counter-flow heat exchangers for gas turbines and gas turbine installations incorporating the same Expired GB802166A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE802166X 1954-09-10

Publications (1)

Publication Number Publication Date
GB802166A true GB802166A (en) 1958-10-01

Family

ID=6717991

Family Applications (1)

Application Number Title Priority Date Filing Date
GB26010/55A Expired GB802166A (en) 1954-09-10 1955-09-12 Improvements in counter-flow heat exchangers for gas turbines and gas turbine installations incorporating the same

Country Status (1)

Country Link
GB (1) GB802166A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4660377A (en) * 1985-02-21 1987-04-28 Fern Engineering, Inc. Regenerative system for a gas turbine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4660377A (en) * 1985-02-21 1987-04-28 Fern Engineering, Inc. Regenerative system for a gas turbine

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