GB191207960A - Improvements in and relating to Internal Combustion Turbines. - Google Patents

Improvements in and relating to Internal Combustion Turbines.

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Publication number
GB191207960A
GB191207960A GB191207960DA GB191207960A GB 191207960 A GB191207960 A GB 191207960A GB 191207960D A GB191207960D A GB 191207960DA GB 191207960 A GB191207960 A GB 191207960A
Authority
GB
United Kingdom
Prior art keywords
combustion
turbine
charge
valve
combustion chamber
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
Inventor
Alexander Taylor Kasley
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
Application granted granted Critical
Publication of GB191207960A publication Critical patent/GB191207960A/en
Expired legal-status Critical Current

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Abstract

7960. Kasley, A. T. April 2. Plant; working-fluid supply. -A combustion-product turbine 15 and a steam turbine 16 are mounted upon a shaft 31. A centrifugal fan 33 subjects air and gas to an initial compression. The air and gas are led by pipes 38, 39 to valves 43, and the mixture is admitted successively through cam-operated lift valves 23 to four combustion chambers, two only of which, 11, 13, are shown in Fig. 1. Each valve 43 reciprocates in unison with the corresponding valve 23, thereby periodically cutting- off the supply. Also, the valves 43 may be rotated by a speed governor 63, thereby governing the amount, or, if desired, the quality of the charges. The charges in the combustion chambers are exploded successively. Pipes 28 lead from the combustion chambers to a rotary distributing-valve 17, which in itself forms the turbine casing. The valve 17 is so provided with nozzles and passages that the products of combustion of each combustion chamber are drawn off in three stages through three successive nozzles and directed upon the turbine wheel. After doing work upon the turbine, the fluid drawn from the combustion chamber during the third stages passes to the exhaust, that from the second stage is passed into a second combustion chamber to compress the charge therein, and that from the first stage to a third combustion chamber to compress the charge therein to a higher degree of compression. It wifl be noted that after a charge enters a combustion chamber, it is initially compressed by the explosion in a second chamber, and then finally compressed by the explosion in a third chamber. The charge is then fired, and the products of combustion are drawn off in three stages as described above. A water-jacket 18 surrounds the combustion chambers and forms a steam-generator for the steam turbine 16.
GB191207960D 1912-04-02 1912-04-02 Improvements in and relating to Internal Combustion Turbines. Expired GB191207960A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB191207960T 1912-04-02

Publications (1)

Publication Number Publication Date
GB191207960A true GB191207960A (en) 1913-01-09

Family

ID=32571357

Family Applications (1)

Application Number Title Priority Date Filing Date
GB191207960D Expired GB191207960A (en) 1912-04-02 1912-04-02 Improvements in and relating to Internal Combustion Turbines.

Country Status (1)

Country Link
GB (1) GB191207960A (en)

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