×

Electronic fuel control system

  • US 4,296,601 A
  • Filed: 08/23/1979
  • Issued: 10/27/1981
  • Est. Priority Date: 08/23/1979
  • Status: Expired due to Term
First Claim
Patent Images

1. A fuel control system for gas turbine engines, comprising:

  • a hydromechanical fuel section for providing fuel flow to the engine at commanded power settings and including means for augmenting said fuel flow in response to a fuel flow modifying signal, andsignal processing means for providing said fuel flow modifying signal in response to signals applied thereto, said signals reflecting power setting, engine speed and ambient and engine conditions,characterized in that said processing means comprises means for providing a correction signal which is summed with an engine speed signal, said correction signal being selected from a plurality of signals each reflecting a maximum engine speed, at least one of said signals being related to the power setting, engine speed and any difference between engine speed and a scheduled engine speed for the particular power setting in such a way as to reflect the required change, if any, in engine speed in order to produce, between actual engine speed and maximum engine speed, a ratio which is the same as the ratio between the actual power setting and the maximum power setting.

View all claims
  • 0 Assignments
Timeline View
Assignment View
    ×
    ×