ES245568A1 - Improvements in the gas turbomotor fuel control systems (Machine-translation by Google Translate, not legally binding) - Google Patents

Improvements in the gas turbomotor fuel control systems (Machine-translation by Google Translate, not legally binding)

Info

Publication number
ES245568A1
ES245568A1 ES0245568A ES245568A ES245568A1 ES 245568 A1 ES245568 A1 ES 245568A1 ES 0245568 A ES0245568 A ES 0245568A ES 245568 A ES245568 A ES 245568A ES 245568 A1 ES245568 A1 ES 245568A1
Authority
ES
Spain
Prior art keywords
fuel
translation
machine
control systems
legally binding
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
ES0245568A
Other languages
Spanish (es)
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 Corp filed Critical Bendix Aviation Corp
Priority to ES0245568A priority Critical patent/ES245568A1/en
Publication of ES245568A1 publication Critical patent/ES245568A1/en
Expired legal-status Critical Current

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Abstract

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)
ES0245568A 1958-11-26 1958-11-26 Improvements in the gas turbomotor fuel control systems (Machine-translation by Google Translate, not legally binding) Expired ES245568A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES0245568A ES245568A1 (en) 1958-11-26 1958-11-26 Improvements in the gas turbomotor fuel control systems (Machine-translation by Google Translate, not legally binding)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES0245568A ES245568A1 (en) 1958-11-26 1958-11-26 Improvements in the gas turbomotor fuel control systems (Machine-translation by Google Translate, not legally binding)

Publications (1)

Publication Number Publication Date
ES245568A1 true ES245568A1 (en) 1959-05-01

Family

ID=34448790

Family Applications (1)

Application Number Title Priority Date Filing Date
ES0245568A Expired ES245568A1 (en) 1958-11-26 1958-11-26 Improvements in the gas turbomotor fuel control systems (Machine-translation by Google Translate, not legally binding)

Country Status (1)

Country Link
ES (1) ES245568A1 (en)

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