GB583763A - Improvements in or relating to internal combustion turbines - Google Patents

Improvements in or relating to internal combustion turbines

Info

Publication number
GB583763A
GB583763A GB2392644A GB2392644A GB583763A GB 583763 A GB583763 A GB 583763A GB 2392644 A GB2392644 A GB 2392644A GB 2392644 A GB2392644 A GB 2392644A GB 583763 A GB583763 A GB 583763A
Authority
GB
United Kingdom
Prior art keywords
casing
blade
ring
rotor
passages
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
GB2392644A
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 GB2392644A priority Critical patent/GB583763A/en
Publication of GB583763A publication Critical patent/GB583763A/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
    • F01D1/02—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines
    • F01D1/12—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines with repeated action on same blade ring
    • F01D1/14—Non-positive-displacement machines or engines, e.g. steam turbines with stationary working-fluid guiding means and bladed or like rotor, e.g. multi-bladed impulse steam turbines with repeated action on same blade ring traversed by the working-fluid substantially radially

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)

Abstract

583,763. Gas turbines. WRIGHT, E. H. Nov. 30, 1944, No. 23926. [Class 110 (iii)] An internal combustion gas turbine comprises a casing 1, a rotor 7 having a cylindrical flange 10 fitted with a member of blade rings 52, 52a, of which one ring 52, Fig. 6, extends through only a part of the flange circumference, a number of combustion chambers 25 which discharge through passages 50 tangentially against the rotor in the plane of the blade ring 52 and a member 15 attached to the casing having channels 56 which re-direct the exhaust from the blade ring 52 on to the blade ring 52a. The discharge from the blade ring 52a may be re-directed on to the blade ring by passages 76 formed in a block 75 attached to the casing. Explosive mixture from a carburettor 28, Fig. 2, is supplied to the cylinders 31, compressed and then passed, through passages 36 and valves 38 operated by a cam on the main shaft 4, to the combustion chambers where it is ignited. The rotor blades 52, Fig. 6, are arranged to cover a part of the flange 10 so that when the combustion chambers are being charged the outlet passages 50 are closed. The charges are ignited just as the first-blades 52 come into registration with the passages 50 and in order to keep the fuel charge in the combustion chamber under pressure the first blade 52 is pivoted on a pin 90. The blade is held in the closed position shown, Fig. 7, by a coil spring (not shown) until the pressure of the gases is sufficient to operate the turbine. The rotor 10, which is split at opposite ends of a diameter at 13, transmits power to the shaft 4 through a disc 7 and co-operating projections 11, 12 and 11<1>, 12<1>. The fixed member 15 is also split at 14 and is located in the casing by the pins 16. The rotor 10 and fixed member 15 are held tightly against each other and the casing 1 by a spreader ring 20 which has a conically tapered surface fitted to a similar surface on the member 15. The ring 20 is urged towards the side wall of the casing by bolts 22 having coiled springs 23 under the nut 24.
GB2392644A 1944-11-30 1944-11-30 Improvements in or relating to internal combustion turbines Expired GB583763A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2392644A GB583763A (en) 1944-11-30 1944-11-30 Improvements in or relating to internal combustion turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2392644A GB583763A (en) 1944-11-30 1944-11-30 Improvements in or relating to internal combustion turbines

Publications (1)

Publication Number Publication Date
GB583763A true GB583763A (en) 1946-12-30

Family

ID=10203543

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2392644A Expired GB583763A (en) 1944-11-30 1944-11-30 Improvements in or relating to internal combustion turbines

Country Status (1)

Country Link
GB (1) GB583763A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2301630A (en) * 1995-06-01 1996-12-11 Bridge Butler James Alexander Internal combustion turbine engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2301630A (en) * 1995-06-01 1996-12-11 Bridge Butler James Alexander Internal combustion turbine engine
GB2301630B (en) * 1995-06-01 1999-12-29 Bridge Butler James Alexander Internal combustion turbine engine

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