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BE516800A - - Google Patents

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Publication number
BE516800A
BE516800ABE516800DABE516800ABE 516800 ABE516800 ABE 516800ABE 516800D ABE516800D ABE 516800DABE 516800 ABE516800 ABE 516800A
Authority
BE
Belgium
Application number
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.)
Publication of BE516800ApublicationCriticalpatent/BE516800A/xx

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BE516800D1952-01-08BE516800A (en)

Applications Claiming Priority (2)

Application NumberPriority DateFiling DateTitle
GB313233X1952-01-08
GB50153X1953-01-05

Publications (1)

Publication NumberPublication Date
BE516800Atrue BE516800A (en)

Family

ID=26239529

Family Applications (1)

Application NumberTitlePriority DateFiling Date
BE516800DBE516800A (en)1952-01-08

Country Status (4)

CountryLink
BE (1)BE516800A (en)
CH (1)CH313233A (en)
FR (1)FR1073487A (en)
GB (1)GB744593A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US2930194A (en)*1956-11-191960-03-29Bendix Aviat CorpCombustor having high turbulent mixing for turbine-type starter
US2979898A (en)*1958-04-251961-04-18United Aircraft CorpHooded crossover tube
FR2673454A1 (en)*1991-02-281992-09-04SnecmaCombustion chamber comprising a bottom wall comprising a plurality of partial truncated cones

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US2930193A (en)*1955-08-291960-03-29Gen ElectricCowled dome liner for combustors
DE1060667B (en)*1955-10-151959-07-02Stroemungsmasch Anst Combustion device for gas turbines
DE1181004B (en)*1959-03-111964-11-05Rolls Royce Combustion chamber for gas turbine jet engines
FR2222124A1 (en)*1973-03-231974-10-18Pillard ChauffageCombustion gases homogenizing equipment - ensures uniform temperatures for drying plants, gas turbines and jet engines
EP2966356B1 (en)*2014-07-102020-01-08Ansaldo Energia Switzerland AGSequential combustor arrangement with a mixer

Cited By (3)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US2930194A (en)*1956-11-191960-03-29Bendix Aviat CorpCombustor having high turbulent mixing for turbine-type starter
US2979898A (en)*1958-04-251961-04-18United Aircraft CorpHooded crossover tube
FR2673454A1 (en)*1991-02-281992-09-04SnecmaCombustion chamber comprising a bottom wall comprising a plurality of partial truncated cones

Also Published As

Publication numberPublication date
CH313233A (en)1956-03-31
FR1073487A (en)1954-09-27
GB744593A (en)1956-02-08

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