Electromechanical power source

Details Electromechanical power source Electromechanical power source

1985-05-14

1987-01-20

Dobeck, Benjamin

Prime-mover dynamo plants

Turbogenerators

60 39464, H02K 2112

Patent

active

046381732

ABSTRACT:
Electric power for a missile during flight is provided by a solid propell gas generator coupled through a magnetically-controlled gas flow diverter valve to drive an axial flow impulse turbine. The turbine is coupled to drive an alternator which produces ac power which is conditioned to supply all the electric power for the missile. The frequency or voltage of the alternator output is sensed and fed back to the speed control circuit where it is compared to the desired value of the chosen parameter. The speed control circuit modulates the glass flow valve to adjust the flow to the turbine to drive the turbine the required speed.

REFERENCES:
patent: 3013388 (1961-12-01), Loughran
patent: 3024366 (1962-03-01), Yanagimachi
patent: 3187188 (1965-06-01), Adkins et al.
patent: 3409782 (1968-11-01), Bronicki
patent: 3541409 (1970-11-01), Storsand
patent: 4033115 (1977-07-01), Baits
patent: 4473754 (1984-09-01), Joy
patent: 4577116 (1986-03-01), Pinson

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