Propulsion aggregate for an aircraft

Details Propulsion aggregate for an aircraft Propulsion aggregate for an aircraft

1984-02-06

1986-12-02

Powell, Jr., Everette A.

Fluid reaction surfaces (i.e., impellers)

Interrelated controls for impeller and drive means

Pitch adjustment and throttle regulation with condition...

416 30, B64C 1134

Patent

active

046261702

ABSTRACT:
A propulsion aggregate for an aircraft consisting of a multicylinder-injection internal combustion engine and of a propeller with adjustable blade pitch driven either directly by the engine or by way of a speed reduction gear. The internal combustion engine is equipped with a commercially available continuously operating fuel injection system which for safety reasons and for designing for optimum aircraft operation, is additionally provided with additional control installations. A throttle valve in the suction line of the internal combustion engine, the blade pitch of the propeller and, in case the internal combustion engine is charged by a turbocharger, also the charging pressure are adjustable by a common adjusting mechanism.

REFERENCES:
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patent: 2480758 (1949-08-01), Mock et al.
patent: 2485431 (1949-10-01), Chudyk
patent: 2486212 (1949-10-01), Schorn et al.
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patent: 2612226 (1952-09-01), Crum
patent: 2727578 (1955-12-01), Alexanderson et al.
patent: 2818847 (1958-01-01), Mock
patent: 3876329 (1975-04-01), Miller

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