Internal-combustion engines – Starting device – For airplane
Patent
1976-10-13
1979-01-02
Myhre, Charles J.
Internal-combustion engines
Starting device
For airplane
123139ST, 261 50A, 261 39B, F02N 1700
Patent
active
041322118
ABSTRACT:
A fuel injection system for continuous injection to an internal combustion engine has a pivoting air sensor plate with a correction lever that engages a fuel control plunger for metering out fuel in proportion to the air flow. The system also includes a bimetallic, temperature-dependent strip which exerts an opening force on the correction lever when the engine is cold. An electric heater is energized by the starter switch and begins to reduce the force due to the bimetallic strip even before the engine has actually warmed up. A second electric heater of reduced power maintains the strip in disengagement during normal engine operation.
REFERENCES:
patent: 3613650 (1971-10-01), Stampp et al.
patent: 3628515 (1971-12-01), Knapp et al.
patent: 3730155 (1973-05-01), Knapp
patent: 3752133 (1973-08-01), Irish et al.
patent: 3806854 (1974-04-01), Armstrong
patent: 3999527 (1976-12-01), Wessel et al.
patent: 4026259 (1977-05-01), Meyerdierks et al.
Grassle Alfred
Peters Klaus-Jurgen
Wilfert Thomas
Greigg Edwin E.
Myhre Charles J.
Reynolds David D.
Robert & Bosch GmbH
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