FR1122874A - Combustion chambers for jet engines, gas turbines or other devices - Google Patents

Combustion chambers for jet engines, gas turbines or other devices

Info

Publication number
FR1122874A
FR1122874A FR1122874DA FR1122874A FR 1122874 A FR1122874 A FR 1122874A FR 1122874D A FR1122874D A FR 1122874DA FR 1122874 A FR1122874 A FR 1122874A
Authority
FR
France
Prior art keywords
devices
combustion chambers
gas turbines
jet engines
engines
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
Other languages
French (fr)
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.)
ZF International UK Ltd
Original Assignee
Lucas Industries Ltd
Joseph Lucas Industries Ltd
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 Lucas Industries Ltd, Joseph Lucas Industries Ltd filed Critical Lucas Industries Ltd
Application granted granted Critical
Publication of FR1122874A publication Critical patent/FR1122874A/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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
FR1122874D 1954-01-21 1955-04-21 Combustion chambers for jet engines, gas turbines or other devices Expired FR1122874A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB180754A GB763359A (en) 1954-01-21 1954-01-21 Combustion chambers for jet propulsion engines, gas turbines or other apparatus

Publications (1)

Publication Number Publication Date
FR1122874A true FR1122874A (en) 1956-09-13

Family

ID=9728360

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1122874D Expired FR1122874A (en) 1954-01-21 1955-04-21 Combustion chambers for jet engines, gas turbines or other devices

Country Status (4)

Country Link
CH (1) CH330988A (en)
DE (1) DE1006215B (en)
FR (1) FR1122874A (en)
GB (1) GB763359A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1097213B (en) * 1958-05-22 1961-01-12 Rolls Royce Incinerator for gas turbine engines
DE10237341A1 (en) 2002-08-14 2004-02-26 Siemens Ag Finite vortex model for use in fluid flow numerical simulation, especially for modeling unsteady flows, whereby a general roll-off model is used to model the finite edge vortex

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB694448A (en) * 1950-10-09 1953-07-22 Rolls Royce Improvements in or relating to gas-turbine engines
US2609663A (en) * 1951-07-21 1952-09-09 United Aircraft Corp Rotatable combustion apparatus for aligning individual flame tubes with access partsor manholes
GB710589A (en) * 1952-03-19 1954-06-16 Lucas Industries Ltd Combustion chambers for jet engines or gas turbines

Also Published As

Publication number Publication date
DE1006215B (en) 1957-04-11
CH330988A (en) 1958-06-30
GB763359A (en) 1956-12-12

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