GB145570A - Improvements in and relating to cooling of gas turbines - Google Patents

Improvements in and relating to cooling of gas turbines

Info

Publication number
GB145570A
GB145570A GB17694/20A GB1769420A GB145570A GB 145570 A GB145570 A GB 145570A GB 17694/20 A GB17694/20 A GB 17694/20A GB 1769420 A GB1769420 A GB 1769420A GB 145570 A GB145570 A GB 145570A
Authority
GB
United Kingdom
Prior art keywords
cooling
exhaust
slot
rotor
relating
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
GB17694/20A
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 GB145570A publication Critical patent/GB145570A/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

145,570. Holzwarth, H. Nov. 5, 1918, [Convention date]. Addition to 145,568. Cooling parts.-Relates to the circular exhaust nozzle a described in the parent Specification, through which the exhaust gases from the gas turbine are discharged, drawing with them a stream of cooling and scavenging air induced round the rotor. According to the present invention, the exhaust gases suck the cooling air not only through the outer slot e, but also through an inner slot f by way of a channel g round the exhaust chamber, thereby cooling the exhaust side of the rotor. The relative proportions of the slots e, f may be varied to suit requirements, and the slot e may be dispensed with altogether.
GB17694/20A 1918-11-05 1920-06-29 Improvements in and relating to cooling of gas turbines Expired GB145570A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE145570X 1918-11-05

Publications (1)

Publication Number Publication Date
GB145570A true GB145570A (en) 1920-12-16

Family

ID=5670848

Family Applications (1)

Application Number Title Priority Date Filing Date
GB17694/20A Expired GB145570A (en) 1918-11-05 1920-06-29 Improvements in and relating to cooling of gas turbines

Country Status (1)

Country Link
GB (1) GB145570A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2772455A1 (en) 2013-02-27 2014-09-03 Veyance Technologies, Inc. Method of manufacturing a fabric reinforcement for a conveyor belt
WO2017186630A1 (en) 2016-04-29 2017-11-02 Contitech Transportbandsysteme Gmbh Method of manufacturing a multi ply thermoplastic conveyor belt

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2772455A1 (en) 2013-02-27 2014-09-03 Veyance Technologies, Inc. Method of manufacturing a fabric reinforcement for a conveyor belt
WO2017186630A1 (en) 2016-04-29 2017-11-02 Contitech Transportbandsysteme Gmbh Method of manufacturing a multi ply thermoplastic conveyor belt

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