Aviation hydraulic propulsion system utilizing secondary controlled drives
A hydraulic propulsion system is disclosed which includes an input interface configured to receive mechanical power from a power source, a pressure source comprising one or more fixed or variable displacement pumps coupled to the input interface and adaptable to convert mechanical power to hydraulic power and controlling outlet pressure of the pressure source (system pressure), one or more variable displacement motors coupled to the pressure source via a corresponding high-pressure line configured to be mechanically coupled to one or more aerodynamic rotors of an aircraft and comprising a closed loop speed control arrangement in response to a commanded rotor speed, and a controller configured to control the speed of one or more variable displacement motors by providing a control signal for controlling the system pressure.
1. A hydraulic propulsion system, comprising:
an input interface configured to receive mechanical power from a power source;
a pressure source comprising one or more fixed or variable displacement pumps coupled to the input interface and adaptable to convert mechanical power to hydraulic power and controlling outlet pressure of the pressure source (system pressure);
one or more variable displacement motors coupled to the pressure source via a corresponding hydraulic line having a fluid therein the one or more variable displacement motors configured to be mechanically coupled to one or more aerodynamic rotors of an aircraft and comprising a closed loop speed control arrangement having one or more speed sensors in response to a commanded rotor speed; and
a controller configured to control the speed of the one or more variable displacement motors by providing a control signal for controlling the system pressure,
the controller further configured to receive signals corresponding to attitude and one or more of position and motion of the aircraft and to generate system pressure using a feedback control system strategy which includes a pressure sensor adapted to adjust fluid pressure in the hydraulic propulsion system, the feedback control system strategy configured to adjust the system pressure based on a desired attitude representing a first system pressure provided as a first pressure sensor reading and a corresponding actual attitude representing a second system pressure provided as a second pressure sensor reading.
2. The system of claim 1 , wherein the power source is one or more internal combustion engines.
3. The system of claim 1 , wherein the power source is one or more electric motors.
4. The system of claim 1 , wherein the power source is one or more turbine engines.
5. The system of claim 1 , wherein the system pressure is set using one of an associated electro-hydraulic displacement control device, hydro-mechanical displacement control device, electro-mechanical displacement control device, and a combination thereof.
6. The system of claim 1 , wherein the speed of the variable displacement motors is controlled by a closed loop speed control utilizing a speed sensing device for measuring rotor speed and one of an associated electro-hydraulic displacement control device, mechanical displacement control device, electro-mechanical displacement control device, and a combination thereof.
7. The system of claim 1 , wherein a system pressure command for the system pressure of the pressure source is generated by one of a flight thrust control computer, a pilot, and a combination thereof.
8. The system of claim 1 , wherein the commanded rotor speed is provided by one of a thrust control computer, a pilot, and a combination thereof.
9. The system of claim 1 , further comprising a fluid cooling device adapted to cool fluid used therein.
10. The system of claim 1 , the controller further configured to receive a signal corresponding to the speed of each motor and to provide the speed information as speed feedback signals to the thrust control computer.
11. The system of claim 10 , further comprising a closed-loop control arrangement using the speed feedback signals.
12. The system of claim 10 , further configured to receive a signal corresponding to the displacement of each motor and to provide the displacement information as displacement feedback signals to the thrust control computer.
13. The system of claim 12 , further comprising a closed-loop control arrangement using the displacement feedback signals.
14. The system of claim 1 , wherein the one or more fixed or variable displacement pumps are coupled to each other in series manner, whereby flow of fluid through each of the pumps is substantially equal and whereby pressure across each of the pumps is additive to establish the system pressure.
15. The system of claim 1 , wherein the variable displacement pumps are coupled in pairs in a parallel manner, whereby pressure across each of the pumps is substantially the same, and fluid flow through the pumps is additive.
16. The system of claim 14 , wherein each pump is coupled to a dedicated power source.
17. The system of claim 14 , wherein each pump is coupled to the one or more input interfaces.
18. The system of claim 17 , wherein the one or more input interfaces is a gearbox.
19. The system of claim 1 , wherein the fluid is acted upon by a compressible fluid.
20. The system of claim 19 , wherein the compressible fluid is air.
21. The system of claim 1 , wherein the fluid is an incompressible fluid.
22. The system of claim 21 , wherein the incompressible fluid is one of hydraulic oil, water, fuel, antifreeze, and a combination thereof.