GB721206A - Improvements in gas turbines - Google Patents

Improvements in gas turbines

Info

Publication number
GB721206A
GB721206A GB2104451A GB2104451A GB721206A GB 721206 A GB721206 A GB 721206A GB 2104451 A GB2104451 A GB 2104451A GB 2104451 A GB2104451 A GB 2104451A GB 721206 A GB721206 A GB 721206A
Authority
GB
United Kingdom
Prior art keywords
chamber
gases
gas turbines
combustion
akindele
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
GB2104451A
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.)
JOSEPH ADEBAYO OMOLOLU AKINDEL
Original Assignee
JOSEPH ADEBAYO OMOLOLU AKINDEL
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 JOSEPH ADEBAYO OMOLOLU AKINDEL filed Critical JOSEPH ADEBAYO OMOLOLU AKINDEL
Priority to GB2104451A priority Critical patent/GB721206A/en
Publication of GB721206A publication Critical patent/GB721206A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion

Abstract

721,206. Generating combustion products under pressure. AKINDELE, J. A. O. July 14, 1952, [Sept. 6, 1951.] No. 21044/51. Class 51 (1). [Also in Group XXVI] The plant comprises a rotary compressor A which supplies a chamber B, having a fuel jet X, a chamber D in which partial combustion takes place, and a chamber C in which further combustion is effected, at constant pressure. The gases are led to a turbine Q which exhausts to the atmosphere, or the gases may be further utilized. An oil burner F is provided for the chamber C.
GB2104451A 1951-09-06 1951-09-06 Improvements in gas turbines Expired GB721206A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2104451A GB721206A (en) 1951-09-06 1951-09-06 Improvements in gas turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2104451A GB721206A (en) 1951-09-06 1951-09-06 Improvements in gas turbines

Publications (1)

Publication Number Publication Date
GB721206A true GB721206A (en) 1955-01-05

Family

ID=10156237

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2104451A Expired GB721206A (en) 1951-09-06 1951-09-06 Improvements in gas turbines

Country Status (1)

Country Link
GB (1) GB721206A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2307008A (en) * 1995-11-13 1997-05-14 Fred Moseley Gas turbine engine with two stage combustion

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2307008A (en) * 1995-11-13 1997-05-14 Fred Moseley Gas turbine engine with two stage combustion

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