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.)
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.)
Bendix Aviation Corp
Original Assignee
Bendix Aviation Corp
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 Bendix Aviation CorpfiledCriticalBendix Aviation Corp
Priority to ES0245568ApriorityCriticalpatent/ES245568A1/en
Publication of ES245568A1publicationCriticalpatent/ES245568A1/en
Improvements in the fuel control systems of gas turbo-engines, characterized in that the engine comprises a nozzle for fuel and also a pump for the fuel as well as the combination of a first fuel conduit connected to the nozzle; a second fuel conduit; a third fuel conduit connected to the pump; a first restriction element, connected between the first and second fuel conduits, for controlling the circulation of this to the nozzle; a second restriction element connected between the second and third fuel conduits, and operative to maintain a predetermined pressure difference in the fuel through the first restriction element, and between a first fuel pressure inside the first conduit thereof and a second fuel pressure inside the second conduit thereof. (Machine-translation by Google Translate, not legally binding)
ES0245568A1958-11-261958-11-26Improvements in the gas turbomotor fuel control systems (Machine-translation by Google Translate, not legally binding)
ExpiredES245568A1
(en)