Back to results
US 2018/0023489 A1Published application
Single Input Engine Controller and System
AssigneeDeltaHawk Engines, Inc.
InventorsDennis R. Webb, William J. Cranmer, Douglas A. Doers
Life of this patent
Estimating the term…
Abstract
A single input engine controller and system are provided for translating a single input indicative of the amount of fuel to be supplied to an engine from a fuel control interface into separate signals for controlling the amount of fuel supplied to the engine and the RPM of a propeller powered by that engine. The single input controller translating the single input into the separate signal for the RPM of the propeller according to a fuel efficiency relationship between the fuel amount and the propeller RPM.
Claims15
A single input aircraft engine and propeller control system comprising:
- a fuel control interface to produce a first mechanical signal corresponding to a specific amount of fuel to be fed to an engine to produce a specific amount of horsepower, the specific amount of horsepower having a corresponding RPM setting for a propeller coupled to the engine, the RPM setting corresponding to a maximum fuel efficiency;
- a single input engine controller coupled to the fuel control interface to receive the first mechanical signal, translate the first mechanical signal into a second mechanical signal indicative of the RPM setting corresponding to the specific amount of horsepower, and output a third mechanical signal indicative of the specific amount of fuel, the third mechanical signal being induced by the first mechanical signal;
- a fuel distribution system coupled to the single input engine controller to receive the third mechanical signal, the third mechanical signal triggering the fuel distribution system to feed the specific amount of fuel to the engine;
- and
- a propeller RPM controller coupled to the single input engine controller to receive the second mechanical signal, the second mechanical signal triggering the RPM controller to set the RPM of the propeller to the corresponding RPM setting.
2 more elements
A single input aircraft engine and propeller control system comprising:
- a fuel control interface to produce a first mechanical signal corresponding to a specific amount of fuel to be fed to an engine to produce a specific amount of horsepower, the specific amount of horsepower having a corresponding RPM setting for a propeller coupled to the engine, the RPM setting corresponding to a maximum fuel efficiency;
- a housing having a first pivot point and a second pivot point;
- a fuel control lever pivotably coupled to the first pivot point;
- an RPM control lever having a cammed slot and being pivotably coupled to the second pivot point, the fuel control lever, and the fuel control interface such that the first mechanical signal induces the RPM control lever and the fuel control lever to pivot about the first and second pivot points, the cammed slot being shaped and sized to translate the pivoting of the RPM control lever into a second mechanical signal indicative of the RPM setting corresponding to the specific amount of horsepower;
- a fuel distribution system pivotably coupled to the fuel control lever to receive a third mechanical signal induced by the pivoting of the fuel control lever, the third mechanical signal triggering the fuel distribution system to feed the specific amount of fuel to the engine;
- and
- a propeller RPM controller slidably coupled to the cammed slot to receive the second mechanical signal induced by the pivoting of the RPM control lever, the second mechanical signal triggering the RPM controller to set the RPM of the propeller to the corresponding RPM setting.
4 more elements
A single input engine controller comprising:
- a housing having a first pivot point and a second pivot point;
- a fuel control lever pivotably coupled to the first pivot point;
- an RPM control lever having a cammed slot and being pivotably coupled to the second pivot point and the fuel control lever to receive a first mechanical signal indicative of a specific amount of fuel, pivot about the second pivot point in response to the first mechanical signal, and induce the fuel control lever to pivot about the first pivot point, the cammed slot being shaped and sized to translate the pivoting of the RPM control lever into a second mechanical signal indicative of an RPM setting corresponding to the specific amount of fuel;
- and
- wherein the pivoting of the fuel control lever induces a third mechanical signal proportional to the first mechanical signal and indicative of the specific amount of fuel.
2 more elements
Dependencies are inferred from the claim text.