GB137550A - Improvements in or relating to turbines or turbine compressors - Google Patents

Improvements in or relating to turbines or turbine compressors

Info

Publication number
GB137550A
GB137550A GB223818A GB223818A GB137550A GB 137550 A GB137550 A GB 137550A GB 223818 A GB223818 A GB 223818A GB 223818 A GB223818 A GB 223818A GB 137550 A GB137550 A GB 137550A
Authority
GB
United Kingdom
Prior art keywords
fluid
iii
turbine
supplied
conduits
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
GB223818A
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
Priority to GB223818A priority Critical patent/GB137550A/en
Publication of GB137550A publication Critical patent/GB137550A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D1/00Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/34Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes
    • F01D1/36Non-positive-displacement machines or engines, e.g. steam turbines characterised by non-bladed rotor, e.g. with drilled holes using fluid friction

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

137,550. Hough, R. H. Feb. 7, 1918. Screw motors; operated by fluid friction; radiat-flow (unbladed) type; working-fluid supply.-A turbine, operated by fluid friction and adapted to act conversely as a compressor, comprises a rotor 3, Fig. III., formed of two cones 30, 31 of different pitch having a space between them divided by a number of similaaÀ tapering helical vanes 42. 43 only two of which are, shown in Fig. III.) into helical-spiral conduits 44 which progressively increase in cross-sectional area from the base towards the apex, and also progressively approach the axis. When operating as a turbine, fluid is supplied to the conduits 44 through stator nozzles 64, Figs. III. and VI., and discharged at the apex end 37, where the linear velocity is less rapid. The vanes 42, 43 may extend only partly across the space between the cones 30, 31, and may be formed on the outer cone, Fig. VIII., on the inner cone, Fig. IX., or on both, Fig. X. The fluid conduits 44 may take the form or flat-spiral passages 404. Fig. XI., increasing in cross-sectional area from the motive-fluid inlets 405 towards the axis. Fig. II. shows a multi-stage turbine, which may comprise five rotors 3 of the kind shown in Fig. III. connected in series, supplied with combustion products from a furnace 12 fed with compressed air by a multi-stage compressor of the same type, which may comprise four rotors 5, Fuel is supplied by a pump 16 to a nozzle 18 in the air-inlet pipe 13 of the furnace 12, the combustion products being led to the first turbine unit 3 through a pipe 21 and a stator member 4.
GB223818A 1918-02-07 1918-02-07 Improvements in or relating to turbines or turbine compressors Expired GB137550A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB223818A GB137550A (en) 1918-02-07 1918-02-07 Improvements in or relating to turbines or turbine compressors

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB223818A GB137550A (en) 1918-02-07 1918-02-07 Improvements in or relating to turbines or turbine compressors

Publications (1)

Publication Number Publication Date
GB137550A true GB137550A (en) 1920-01-22

Family

ID=9736023

Family Applications (1)

Application Number Title Priority Date Filing Date
GB223818A Expired GB137550A (en) 1918-02-07 1918-02-07 Improvements in or relating to turbines or turbine compressors

Country Status (1)

Country Link
GB (1) GB137550A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1015573B (en) * 1956-02-02 1957-09-12 Arthur Pfeiffer Fa Molecular pump
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 (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1015573B (en) * 1956-02-02 1957-09-12 Arthur Pfeiffer Fa Molecular pump
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

Similar Documents

Publication Publication Date Title
US2709893A (en) Gas turbine power plant with heat exchanger and cooling means
US2078956A (en) Gas turbine system
US2435836A (en) Centrifugal compressor
US2715814A (en) Fuel-flow for plural radial inwardflow gas turbines
US2689681A (en) Reversely rotating screw type multiple impeller compressor
US2677932A (en) Combustion power plants in parallel
GB1113087A (en) Gas turbine power plant
US3240012A (en) Turbo-jet powerplant
US2520697A (en) Internal-combustion turbine plant
US2762559A (en) Axial flow compressor with axially adjustable rotor
GB626044A (en) Improvements in or relating to gas turbine power plants
US3469396A (en) Gas turbine
GB645258A (en) Improvements in or relating to turbines
US2474410A (en) Multistage compressor
GB1125251A (en) Improved gas turbine engine
GB935903A (en) Gas turbine power plant having centripetal flow compressors and centrifugal flow turbines
US2382564A (en) Turbine system
GB137550A (en) Improvements in or relating to turbines or turbine compressors
GB724176A (en) Improvements in and relating to combustion turbine plants
US3056580A (en) Gas turbine starter
US2621476A (en) Gas turbine installation operating on gaseous fuels
US4431371A (en) Gas turbine with blade temperature control
US2393713A (en) Aircraft supercharger
US2380772A (en) Centrifugal compressor
US3018623A (en) Explosion gas turbines