GB145568A - Improvements in and relating to cooling of gas turbines - Google Patents

Improvements in and relating to cooling of gas turbines

Info

Publication number
GB145568A
GB145568A GB17692/20A GB1769220A GB145568A GB 145568 A GB145568 A GB 145568A GB 17692/20 A GB17692/20 A GB 17692/20A GB 1769220 A GB1769220 A GB 1769220A GB 145568 A GB145568 A GB 145568A
Authority
GB
United Kingdom
Prior art keywords
cooling
gas turbines
relating
explosion chambers
ring
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
GB17692/20A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB145568A publication Critical patent/GB145568A/en
Expired 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08—Cooling; Heating; Heat-insulation
    • F01D25/12—Cooling

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

145,568. Holzwarth, H. Sept. 5, 1918, [Convention date]. Cooling parts.-In gas turbines having several explosion chambers the gases are discharged from the last ring of rotor blades through an annular' extaust a so so as to take with them a stream of cooling or scavenging air which is drawn by induction through the explosion chambers and a passage 5 formed between a ring 4 and the casing. An exhaust fan or blower is thereby dispensed with, and the waste gases of the turbine can be used in other ways.
GB17692/20A 1918-09-05 1920-06-29 Improvements in and relating to cooling of gas turbines Expired GB145568A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE145568X 1918-09-05

Publications (1)

Publication Number Publication Date
GB145568A true GB145568A (en) 1920-12-16

Family

ID=5670846

Family Applications (1)

Application Number Title Priority Date Filing Date
GB17692/20A Expired GB145568A (en) 1918-09-05 1920-06-29 Improvements in and relating to cooling of gas turbines

Country Status (1)

Country Link
GB (1) GB145568A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2429990A (en) * 1944-07-17 1947-11-04 Gen Electric Gas turbine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2429990A (en) * 1944-07-17 1947-11-04 Gen Electric Gas turbine

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