GB1416011A - Gas turbine plants and related thermal process - Google Patents

Gas turbine plants and related thermal process

Info

Publication number
GB1416011A
GB1416011A GB2020172A GB2020172A GB1416011A GB 1416011 A GB1416011 A GB 1416011A GB 2020172 A GB2020172 A GB 2020172A GB 2020172 A GB2020172 A GB 2020172A GB 1416011 A GB1416011 A GB 1416011A
Authority
GB
United Kingdom
Prior art keywords
gas turbine
heat exchanger
tube assembly
compressor
heated
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
GB2020172A
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.)
BOLESTA D
Original Assignee
BOLESTA D
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 BOLESTA D filed Critical BOLESTA D
Priority to GB2020172A priority Critical patent/GB1416011A/en
Publication of GB1416011A publication Critical patent/GB1416011A/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
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/34—Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes
    • F01D1/36—Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes using fluid friction
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/25—Three-dimensional helical

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)

Abstract

1416011 Gas turbine plant; turbines D BOLESTA 1 Nov 1972 20201/72 Headings F1G and FIT A gas turbine plant comprises a heat exchanger which is arranged to rotate and serves both as a heat exchanger by which working fluid such as air is pre-heated, and as a power generating element in the form of a turbine the driving force of which, it is stated, is the force of friction produced by the flow of working fluid therethrough also by the reaction force of fluid discharging therefrom. In one embodiment, the heat exchanger comprises a series of V-shaped tubes pointing in the direction of rotation; combustion gases from a combustion chamber are directed by inlet guide nozzles into the tube assembly which is caused to rotate, the gases discharging from the tubes on to the blades of a turbine rotor which is connected to drive a compressor. Air from the compressor is directed across the tube assembly and is thereby pre-heated being then passed into the combustion chamber into which fuel is also injected. The rotary tube assembly provides useful power. Other embodiments are described.
GB2020172A 1972-11-01 1972-11-01 Gas turbine plants and related thermal process Expired GB1416011A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2020172A GB1416011A (en) 1972-11-01 1972-11-01 Gas turbine plants and related thermal process

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2020172A GB1416011A (en) 1972-11-01 1972-11-01 Gas turbine plants and related thermal process

Publications (1)

Publication Number Publication Date
GB1416011A true GB1416011A (en) 1975-12-03

Family

ID=10142108

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2020172A Expired GB1416011A (en) 1972-11-01 1972-11-01 Gas turbine plants and related thermal process

Country Status (1)

Country Link
GB (1) GB1416011A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8863530B2 (en) 2008-10-30 2014-10-21 Power Generation Technologies Development Fund L.P. Toroidal boundary layer gas turbine
US9052116B2 (en) 2008-10-30 2015-06-09 Power Generation Technologies Development Fund, L.P. Toroidal heat exchanger

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8863530B2 (en) 2008-10-30 2014-10-21 Power Generation Technologies Development Fund L.P. Toroidal boundary layer gas turbine
US9052116B2 (en) 2008-10-30 2015-06-09 Power Generation Technologies Development Fund, L.P. Toroidal heat exchanger
US9243805B2 (en) 2008-10-30 2016-01-26 Power Generation Technologies Development Fund, L.P. Toroidal combustion chamber
US10401032B2 (en) 2008-10-30 2019-09-03 Power Generation Technologies Development Fund, L.P. Toroidal combustion chamber

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Legal Events

Date Code Title Description
PS Patent sealed
PLNP Patent lapsed through nonpayment of renewal fees