GB411787A - Improvements in gas turbine plant - Google Patents

Improvements in gas turbine plant

Info

Publication number
GB411787A
GB411787A GB3143/34A GB314334A GB411787A GB 411787 A GB411787 A GB 411787A GB 3143/34 A GB3143/34 A GB 3143/34A GB 314334 A GB314334 A GB 314334A GB 411787 A GB411787 A GB 411787A
Authority
GB
United Kingdom
Prior art keywords
turbine
compressor
plant
gas
compressors
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
GB3143/34A
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.)
Milo AB
Original Assignee
Milo AB
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 Milo AB filed Critical Milo AB
Publication of GB411787A publication Critical patent/GB411787A/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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages

Landscapes

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

Abstract

411,787. Gas-turbine plant. AKTIEBOLAGET MILO, 32, Kungsgatan, Stockholm. Jan. 30, 1934, No. 3143. Convention date, Feb. 1, 1933. [Class 110 (iii).] In a gas-turbine plant in which a powergenerating turbine 1 exhausts into a turbine 6 driving compressors 12, 14, for the charge air, a further compressor 16 is arranged to be driven by the power turbine. Conduits and valves are arranged so that at low-load or noload on the turbine 1, the compressor-driving turbine 6 may be cut out, the work of compression then being done by the compressor 16 acting alone. During normal working the compressor 16 may be in series or in parallel with the compressors 12, 14, or may be rendered inoperative by a clutch 39. The plant comprises a cooler 18 in the compressed air pipe into which water is sprayed, a regenerator 8 heated by exhaust gases, and a combustion chamber 23. In a modification the exhaust of the turbine 1 is reheated on its passage to the turbine 6.
GB3143/34A 1933-02-01 1934-01-30 Improvements in gas turbine plant Expired GB411787A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE411787X 1933-02-01

Publications (1)

Publication Number Publication Date
GB411787A true GB411787A (en) 1934-06-14

Family

ID=6432894

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3143/34A Expired GB411787A (en) 1933-02-01 1934-01-30 Improvements in gas turbine plant

Country Status (1)

Country Link
GB (1) GB411787A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2473356A (en) * 1942-04-18 1949-06-14 Turbo Engineering Corp Combustion gas turbine arrangement
US2779159A (en) * 1952-05-01 1957-01-29 Tech Studien Ag Thermal power installation for utilising waste heat
US2787886A (en) * 1951-11-17 1957-04-09 Garrett Corp Aircraft auxiliary power device using compounded gas turbo-compressor units

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2473356A (en) * 1942-04-18 1949-06-14 Turbo Engineering Corp Combustion gas turbine arrangement
US2787886A (en) * 1951-11-17 1957-04-09 Garrett Corp Aircraft auxiliary power device using compounded gas turbo-compressor units
US2779159A (en) * 1952-05-01 1957-01-29 Tech Studien Ag Thermal power installation for utilising waste heat

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