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GB400894A - Improvements in gas turbine aggregates - Google Patents

Improvements in gas turbine aggregates

Info

Publication number
GB400894A
GB400894A GB19200/33A GB1920033A GB400894A GB 400894 A GB400894 A GB 400894A GB 19200/33 A GB19200/33 A GB 19200/33A GB 1920033 A GB1920033 A GB 1920033A GB 400894 A GB400894 A GB 400894A
Authority
GB
United Kingdom
Prior art keywords
turbine
flow turbine
turbines
axial flow
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
GB19200/33A
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 GB400894A publication Critical patent/GB400894A/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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/003—Gas-turbine plants with heaters between turbine stages

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

400,894. Gas turbines. AKTIEBOLAGET MILO, 32, Kungsgatan, Stockholm. July 6, 1933, No. 19200. Convention date, July 7, 1932. [Class 110 (iii).] A gas turbine plant comprises a highpressure radial flow turbine, and a lowpressure axial flow turbine arranged separately from it, a reheating apparatus being arranged between them. In Fig. 3 the power unit driving the generators 33, 34 consists of a high-pressure double-rotation radial-flow turbine 23 and two low-pressure axial flow turbines 28, 29. The air for combustion is drawn in at 10 and passes in series through compressors 11, 13, 15 to a fuel burner 17. The products are first used in a double-rotation radial flow turbine 20 which drives the compressors 13, 15, and then pass to a reheater 21 after which they are used in the main turbine 23. The exhaust from this turbine is reheated at 24 and divided into three parts ; two parts are used in the turbines 28, 29 and the third part in an axial flow turbine 26 which drives the compressor 11. Simplified modifications are described. 400,894.
GB19200/33A 1932-07-07 1933-07-06 Improvements in gas turbine aggregates Expired GB400894A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE400894X 1932-07-07

Publications (1)

Publication Number Publication Date
GB400894A true GB400894A (en) 1933-11-02

Family

ID=6402650

Family Applications (1)

Application Number Title Priority Date Filing Date
GB19200/33A Expired GB400894A (en) 1932-07-07 1933-07-06 Improvements in gas turbine aggregates

Country Status (1)

Country Link
GB (1) GB400894A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2628473A (en) * 1948-05-03 1953-02-17 Frye Jack Stationary power plant having radially and axially displaced jet engines
DE965613C (en) * 1954-09-11 1957-06-13 Henschel & Sohn G M B H Small gas turbine with tubular combustion chamber
DE1101864B (en) * 1958-04-24 1961-03-09 Motoren Werke Mannheim Ag Gas turbine with circulation atomization of the fuel
US5709076A (en) * 1992-09-14 1998-01-20 Lawlor; Shawn P. Method and apparatus for power generation using rotating ramjet which compresses inlet air and expands exhaust gas against stationary peripheral wall
US6298653B1 (en) 1996-12-16 2001-10-09 Ramgen Power Systems, Inc. Ramjet engine for power generation
US6347507B1 (en) 1992-09-14 2002-02-19 Ramgen Power Systems, Inc. Method and apparatus for power generation using rotating ramjets
US6446425B1 (en) 1998-06-17 2002-09-10 Ramgen Power Systems, Inc. Ramjet engine for power generation

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2628473A (en) * 1948-05-03 1953-02-17 Frye Jack Stationary power plant having radially and axially displaced jet engines
DE965613C (en) * 1954-09-11 1957-06-13 Henschel & Sohn G M B H Small gas turbine with tubular combustion chamber
DE1101864B (en) * 1958-04-24 1961-03-09 Motoren Werke Mannheim Ag Gas turbine with circulation atomization of the fuel
US5709076A (en) * 1992-09-14 1998-01-20 Lawlor; Shawn P. Method and apparatus for power generation using rotating ramjet which compresses inlet air and expands exhaust gas against stationary peripheral wall
US6347507B1 (en) 1992-09-14 2002-02-19 Ramgen Power Systems, Inc. Method and apparatus for power generation using rotating ramjets
US6298653B1 (en) 1996-12-16 2001-10-09 Ramgen Power Systems, Inc. Ramjet engine for power generation
US6334299B1 (en) 1996-12-16 2002-01-01 Ramgen Power Systems, Inc. Ramjet engine for power generation
US6434924B1 (en) 1996-12-16 2002-08-20 Ramgen Power Systems, Inc. Ramjet engine for power generation
US6446425B1 (en) 1998-06-17 2002-09-10 Ramgen Power Systems, Inc. Ramjet engine for power generation

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