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.)
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Rolls Royce PLC
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Rolls Royce PLC
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Publication date
Application filed by Rolls Royce PLCfiledCriticalRolls Royce PLC
Priority to ES0255694ApriorityCriticalpatent/ES255694A1/en
Publication of ES255694A1publicationCriticalpatent/ES255694A1/en
A fuel installation for a gas turbine engine, for regulating the supply of pressurized fuel from a source of origin thereof to a burner of a gas turbine engine, system comprising: means that create a measuring orifice; means for supplying pressurized fuel from said source to said burner through said measuring orifice; means modifying the size of the measuring orifice according to the speed of rotation of the motor e, independently, in functional relation to the ratio of the output and inlet pressures of a motor compressor; and means for measuring or calibrating the flow of fuel to the burner according to the loss of load through the measuring hole. (Machine-translation by Google Translate, not legally binding)
ES0255694A1960-02-111960-02-11A fuel installation for gas turbine engine (Machine-translation by Google Translate, not legally binding)
ExpiredES255694A1
(en)