GB704678A - Improvements in gas turbines - Google Patents

Improvements in gas turbines

Info

Publication number
GB704678A
GB704678A GB293351A GB293351A GB704678A GB 704678 A GB704678 A GB 704678A GB 293351 A GB293351 A GB 293351A GB 293351 A GB293351 A GB 293351A GB 704678 A GB704678 A GB 704678A
Authority
GB
United Kingdom
Prior art keywords
combustion chamber
shaft
turbine
compressor
bearings
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
GB293351A
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 GB293351A priority Critical patent/GB704678A/en
Priority to FR1076479D priority patent/FR1076479A/en
Publication of GB704678A publication Critical patent/GB704678A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/52—Toroidal combustion chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)

Abstract

704,678. Gas turbine plant. BUDWORTH, D. D. Feb. 6, 1952 [Feb. 6, 1951], No. 2933/51. Class 110 (3). [Also in Groups XII and XXVII] In a gas turbine plant comprising an annular combustion chamber 19, 20 having fuel injection means 22 and a centrifugal compressor 6 and an inward radial flow turbine 24 mounted on a common shaft 15, the shaft is journalled in bearings situated at a point remote from the combustion chamber and overhangs said bearings and the turbine is concentrically arranged within or adjacent to the combustion chamber and is connected to an output shaft 33 through suitable gearing. The plant comprises a casing 1 having end plates 2, 10 and a partition 3 for dividing it into a gear casing 4 and a compressor casing 5. Air is drawn through ports 7 and guide vanes 8 into the compressor 6 and is discharged through a diffuser 17 into the combustion chamber. The fuel injectors 22 are offset with respect to kidney-shaped holes 48 in the member 20. The products of combustion together with air entering the member 20 through ports 21 are fed to the turbine 24 through guide nozzles 25. The turbine and compressor units are pinned together as shown or are formed integral with one another. Oil is fed to the gearing through pipes 40, 41; a branch pipe 42 supplying the bearings of the shaft 15. Starting is effected by driving the shaft 33 through a free wheel clutch and a sprocket and chain driving mechanism 36, 37, 38 having a starting dog 39. It is stated in the Provisional Specification that the air supplied to the combustion chamber may be preheated in one or more heat exchangers.
GB293351A 1951-02-06 1951-02-06 Improvements in gas turbines Expired GB704678A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB293351A GB704678A (en) 1951-02-06 1951-02-06 Improvements in gas turbines
FR1076479D FR1076479A (en) 1951-02-06 1953-04-27 Gas turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB293351A GB704678A (en) 1951-02-06 1951-02-06 Improvements in gas turbines

Publications (1)

Publication Number Publication Date
GB704678A true GB704678A (en) 1954-02-24

Family

ID=9748790

Family Applications (1)

Application Number Title Priority Date Filing Date
GB293351A Expired GB704678A (en) 1951-02-06 1951-02-06 Improvements in gas turbines

Country Status (2)

Country Link
FR (1) FR1076479A (en)
GB (1) GB704678A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE968370C (en) * 1954-09-11 1958-02-06 Henschel & Sohn G M B H Gas turbine for smaller capacities
DE1072953B (en) * 1960-01-14 Obermaier ix Qe., Neustadt an der Weinstraße Device for quick drying of textiles
DE1076444B (en) * 1955-06-18 1960-02-25 Alfred J Buechi Gas turbine impeller
DE1079389B (en) * 1954-10-08 1960-04-07 David Dutton Budworth Combustion turbine with fuel evaporator
CN112483252A (en) * 2020-12-15 2021-03-12 通化师范学院 Vertical speed reduction gas turbine

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1072953B (en) * 1960-01-14 Obermaier ix Qe., Neustadt an der Weinstraße Device for quick drying of textiles
DE968370C (en) * 1954-09-11 1958-02-06 Henschel & Sohn G M B H Gas turbine for smaller capacities
DE1079389B (en) * 1954-10-08 1960-04-07 David Dutton Budworth Combustion turbine with fuel evaporator
DE1076444B (en) * 1955-06-18 1960-02-25 Alfred J Buechi Gas turbine impeller
CN112483252A (en) * 2020-12-15 2021-03-12 通化师范学院 Vertical speed reduction gas turbine

Also Published As

Publication number Publication date
FR1076479A (en) 1954-10-27

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