ES318389A1 - Improvements in appliances for fuel control. (Machine-translation by Google Translate, not legally binding) - Google Patents

Improvements in appliances for fuel control. (Machine-translation by Google Translate, not legally binding)

Info

Publication number
ES318389A1
ES318389A1 ES0318389A ES318389A ES318389A1 ES 318389 A1 ES318389 A1 ES 318389A1 ES 0318389 A ES0318389 A ES 0318389A ES 318389 A ES318389 A ES 318389A ES 318389 A1 ES318389 A1 ES 318389A1
Authority
ES
Spain
Prior art keywords
fuel
engine
conduit
nozzle
bypass valve
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
ES0318389A
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 Corp
Original Assignee
Bendix 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 Corp filed Critical Bendix Corp
Publication of ES318389A1 publication Critical patent/ES318389A1/en
Expired legal-status Critical Current

Links

Landscapes

  • Fuel-Injection Apparatus (AREA)

Abstract

"Improvements in equipment for fuel control", for a combustion engine, equipped with a combustion chamber; of a compressor to supply compressed air to the combustion chamber; a fuel nozzle for injecting compressed fuel into said chamber, and a control lever for regulating the operation of the engine; said apparatus includes a fuel conduit connecting an origin thereof to the nozzle thereof and in which conduit a fuel pump is operatively connected to said compressor, to pressurize the fuel originating from the origin to the nozzle thereof, CHARACTERIZED by that the fuel conduit has three holes mounted in series in it, whose surfaces are controlled respectively by valves, one of them driven by a regulator dependent on the speed of the engine and with its graduation adjusted by the control lever to maintain a speed chosen from the motor, and the other two valves, operated, respectively, by devices depending on the operating parameters of the motor; and a bypass line connects the fuel conduit, after said fuel pump, and the fuel conduit, before said pump and contains a bypass valve that controls the fuel stream in said bypass conduits; said bypass valve is functionally connected to a device dependent on the total difference in fuel pressures through the above-mentioned orifices, and to a third operating parameter of the engine; said pressure difference and the third parameter, exert actions in opposite directions on an element of this device that drives the bypass valve and moves it to a position corresponding to the balance of said actions. (Machine-translation by Google Translate, not legally binding)
ES0318389A 1964-10-12 1965-10-11 Improvements in appliances for fuel control. (Machine-translation by Google Translate, not legally binding) Expired ES318389A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US40307164A 1964-10-12 1964-10-12

Publications (1)

Publication Number Publication Date
ES318389A1 true ES318389A1 (en) 1966-02-16

Family

ID=38572079

Family Applications (1)

Application Number Title Priority Date Filing Date
ES0318389A Expired ES318389A1 (en) 1964-10-12 1965-10-11 Improvements in appliances for fuel control. (Machine-translation by Google Translate, not legally binding)

Country Status (1)

Country Link
ES (1) ES318389A1 (en)

Similar Documents

Publication Publication Date Title
ES275951A1 (en) Fuel control device for a combustiĆ³n engine (Machine-translation by Google Translate, not legally binding)
GB917699A (en) Improvements in or relating to a gaseous fluid actuated hydraulic power unit
US3123128A (en) Fuel metering system
ES268708A1 (en) Fuel control for combustion engines
ES318389A1 (en) Improvements in appliances for fuel control. (Machine-translation by Google Translate, not legally binding)
GB1445347A (en) Fuel control apparatus for gas turbine engines
ES472122A1 (en) Fuel injection pumping apparatus for internal combustion engines including manifold pressure device
US2588530A (en) Apparatus for supplying liquid fuel to the combustion chamber of, and controlling the quantity of motive air in, hot-air engines
SU253489A1 (en) Fuel supply regulator for a compressed-air gas turbine engine
ES234991A1 (en) Governor controlled engine
GB833418A (en) Improvements in or relating to liquid distributing systems
GB836067A (en) Carburettors
GB751361A (en) Improvements in or relating to liquid fuel control systems particularly for gas turbine apparatus
GB754854A (en) Improvements in jet propulsion engines including at least one control device for temporarily modifying the operation of said engine
GB762194A (en) Improvements in apparatus for feeding liquid fuel to the burners of continuous combustion turbine engines
GB937951A (en) Control system for sandblasting equipment
GB840456A (en) Fuel control apparatus for gas turbine engines
GB899670A (en) Governor for turbo-supercharged prime movers
GB772247A (en) Improvements in or relating to gas-turbine engines
GB712775A (en) Liquid fuel control means for jet-propulsion engines
GB802923A (en) Improvements in or relating to fuel supply systems for gas turbine engines
GB1002534A (en) Improvements in or relating to acceleration-control devices for use in liquid-fuel supply systems, more particularly of gas turbines
GB815584A (en) Speed-responsive governors
GB791621A (en) Improvements in or relating to gas turbine engine fuel systems
ES249888A1 (en) Perfected control system for an engine equipped with a variable surface exhaust nozzle and a controlled fluid origin (Machine-translation by Google Translate, not legally binding)