GB260364A - Improvements in internal combustion turbines - Google Patents

Improvements in internal combustion turbines

Info

Publication number
GB260364A
GB260364A GB1997025A GB1997025A GB260364A GB 260364 A GB260364 A GB 260364A GB 1997025 A GB1997025 A GB 1997025A GB 1997025 A GB1997025 A GB 1997025A GB 260364 A GB260364 A GB 260364A
Authority
GB
United Kingdom
Prior art keywords
combustion
piston
cylinder
pistons
charles
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
GB1997025A
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.)
JOHN LEONARD CHARLES
Original Assignee
JOHN LEONARD CHARLES
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 JOHN LEONARD CHARLES filed Critical JOHN LEONARD CHARLES
Priority to GB1997025A priority Critical patent/GB260364A/en
Publication of GB260364A publication Critical patent/GB260364A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C5/00Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/02Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant

Abstract

260,364. Charles, J. L., and Charles, A. E. Aug. 8, 1925. Generating combustion products under pressure.-A combustion product turbine is supplied by one or more combustion units each comprising a cylinder with a combustion space at each end and a double acting piston 10 therein and a pair of compression cylinders 13 the pistons 12 of which are rigidly connected to the combustion cylinder piston 10. The charge enters the compression cylinders 13 by inlets 14 and passes through ports 16 to the combustion cylinder when these are opened by the reduced portions 11 of the piston rod 9. The combustion piston 10 acts as a valve to release the combustion products to the turbine which in their passage may draw in by injector action air or steam generated in a water container 3 which houses the combustion units. The firing of the plugs 15 is controlled by the compression pistons 12 acting on an adjustable spring-pressed pin 23 to close the electrical circuit. At starting cornpressed air admitted at ports 20 operates the pistons 12 and mixture is admitted through a port 17 to the combustion cylinder 10.
GB1997025A 1925-08-08 1925-08-08 Improvements in internal combustion turbines Expired GB260364A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1997025A GB260364A (en) 1925-08-08 1925-08-08 Improvements in internal combustion turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1997025A GB260364A (en) 1925-08-08 1925-08-08 Improvements in internal combustion turbines

Publications (1)

Publication Number Publication Date
GB260364A true GB260364A (en) 1926-11-04

Family

ID=10138139

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1997025A Expired GB260364A (en) 1925-08-08 1925-08-08 Improvements in internal combustion turbines

Country Status (1)

Country Link
GB (1) GB260364A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1113334B (en) * 1958-07-11 1961-08-31 Max Bochskanl Gas turbine in connection with a gas generator
DE1128707B (en) * 1958-11-21 1962-04-26 Max Bochskanl Gas turbine in connection with a gas generator
EP3019703A4 (en) * 2013-07-10 2016-08-03 Derrick Miller Engine propulsion system

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1113334B (en) * 1958-07-11 1961-08-31 Max Bochskanl Gas turbine in connection with a gas generator
DE1128707B (en) * 1958-11-21 1962-04-26 Max Bochskanl Gas turbine in connection with a gas generator
EP3019703A4 (en) * 2013-07-10 2016-08-03 Derrick Miller Engine propulsion system

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