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US 5,865,602 AGranted
Aircraft hydraulic pump control system
AssigneeThe Boeing Company
InventorFarhad Nozari
Life of this patent
Estimating the term…
Abstract
A control system for an aircraft's electrically driven hydraulic pump. An electronic motor controller having closed loop feedback is utilized to directly control the prime mover speed in response to pump loading.
Claims2
A pressure regulated hydraulic supply system of an aircraft comprising:
- a variable displacement swash pump comprising a swash plate for regulating system pressure;
- a variable speed electric motor for driving said variable displacement swash pump;
- control circuit means for controlling said variable displacement swash pump to displace said swash plate in response to system demand;
- sensing means for sensing a displacement of said swash plate;
- said control circuit means driving said variable speed electric motor at a speed responsive to said sensed displacement of said swash plate;
- and
- said control circuit means controlling the speed of said variable speed electric motor in a continuous and gradual manner in response to said sensed displacement of said swash plate, wherein the speed of said variable speed electric motor is increased or decreased at a rate slower than a rate at which said swash plate is being displaced.
4 more elements
A method for operating a hydraulic supply system of an aircraft including a variable displacement swash pump having a swash plate, said variable displacement swash pump driven by a variable speed electric motor, comprising the steps of:
- operating said variable speed electric motor at high speed with said swash plate at full displacement when said hydraulic supply system requires a high fluid flow for maintaining system pressure;
- reducing said variable speed electric motor speed and said swash plate at reduced displacement when said hydraulic supply system requires a low pump flow;
- sensing said swash plate displacement;
- and
- controlling the speed of said variable speed electric motor in a continuous and gradual manner in response to said sensed swash plate displacement, wherein the speed of said variable speed electric motor is increased or decreased at a rate slower than a rate at which said swash plate is being displaced.
2 more elements
Dependencies are inferred from the claim text.