Control system for plural engines

Details Control system for plural engines Control system for plural engines

1977-07-22

1979-02-06

Ostrager, Allen M.

Power plants

System having plural motors or having diverse types of...

Having condition responsive control

60716, F01B 2100

Patent

active

041377214

ABSTRACT:
Two gas turbine helicopter engines are coupled together for isochronous operation to supply a common load. A control circuit assures that the power delivered to the common load is equally divided between the two engines. The torque of each engine is detected and the torques are compared to established control signals for the engines.

REFERENCES:
patent: 2103274 (1937-12-01), Sanford
patent: 3234740 (1966-02-01), Moore
patent: 3511052 (1970-05-01), Gillespie

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