GB697119A - Generator of compressed air - Google Patents

Generator of compressed air

Info

Publication number
GB697119A
GB697119A GB3854/51A GB385451A GB697119A GB 697119 A GB697119 A GB 697119A GB 3854/51 A GB3854/51 A GB 3854/51A GB 385451 A GB385451 A GB 385451A GB 697119 A GB697119 A GB 697119A
Authority
GB
United Kingdom
Prior art keywords
compressed air
combustion chamber
turbine
feb
generator
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
GB3854/51A
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 GB697119A publication Critical patent/GB697119A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/02Units comprising pumps and their driving means
    • F04D25/04Units comprising pumps and their driving means the pump being fluid-driven
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/04Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
    • F02C6/06Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas
    • F02C6/08Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output providing compressed gas the gas being bled from the gas-turbine compressor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/4206Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/50Inlet or outlet
    • F05D2250/52Outlet
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

697,119. Gas turbine plant. SZYDLOWSKI, J. Feb. 16, 1951 [Feb. 22, 1950], No. 3854/51. Class 110(iii) A compressed air generator set comprises a combustion chamber 6 as described in Specification 686,908 and a radial-flow compressor 1 driven by a turbine 7 not adapted to provide excess power wherein the compressed air additional to that required in the combustion chamber is collected in an annular chamber 5 which surrounds the casing of the combustion chamber and communicates therewith through ports. The annular chamber 5 constitutes a volute having a tapping 11. The turbine 7 may be of the multi- or single-stage type.
GB3854/51A 1950-02-22 1951-02-16 Generator of compressed air Expired GB697119A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR899588X 1950-02-22

Publications (1)

Publication Number Publication Date
GB697119A true GB697119A (en) 1953-09-16

Family

ID=9392350

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3854/51A Expired GB697119A (en) 1950-02-22 1951-02-16 Generator of compressed air

Country Status (3)

Country Link
DE (1) DE899588C (en)
FR (1) FR1013172A (en)
GB (1) GB697119A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2673845A1 (en) * 1991-03-13 1992-09-18 Drecq Daniel Autonomous device for generating compressed air, and recompression casing incorporating it
EP2362079A3 (en) * 2010-02-18 2012-11-28 Rolls-Royce Deutschland Ltd & Co KG Gas turbine with a bleed air device for the compressor

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2673845A1 (en) * 1991-03-13 1992-09-18 Drecq Daniel Autonomous device for generating compressed air, and recompression casing incorporating it
EP2362079A3 (en) * 2010-02-18 2012-11-28 Rolls-Royce Deutschland Ltd & Co KG Gas turbine with a bleed air device for the compressor

Also Published As

Publication number Publication date
DE899588C (en) 1953-12-14
FR1013172A (en) 1952-07-23

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