This application relates to an improved design for a piezo-electric fluid pump which may, for example, be used as a hydraulic pump in aircraft systems.
Other than small personal aircraft, present day aircraft have a number of hydraulically operated systems, such as wing flap actuators and landing gear actuators. To date a central hydraulic pump is provided to provide a supply of pressurised hydraulic fluid to each system. Each system may have its own dedicated pump, or multiple pumps, or alternatively all the hydraulic systems are serviced by the same pump(s). This centralised arrangement has a number of disadvantages, such as weight and the number of components (hydraulic pipes, connectors and valves for example) subject to wear.
To mitigate against the disadvantages of a centralised hydraulic system for aircraft it is possible to make use of electro-hydraulic actuators (EHA), in which each actuator has its own associated, often integrated, electrically driven hydraulic pump. Distributing power around the aircraft to each of the actuators electrically rather than hydraulically brings with it a reduction in weight and a reduction in the number of components.
A conventional electro-hydraulic actuator includes a hydraulic pump driven by a separate electric motor. These separate components can be replaced by piezo-electric pump, thereby bringing about a further reduction in weight and the number of components prone to wear. The basic principle of a piezo-electric pump is that a stack of piezo-electric elements are driven by an alternating current, thus causing the stack to alternatively expand and contract in a reciprocating motion, which in turn can cause the volume of a fluid pumping chamber to alternatively increase and decrease, thus causing a volume of fluid to be pumped in and out of the chamber.
However, piezo-electric pumps typically have low pressure and low flow rate capabilities, which are undesirable for use in electro-hydraulic actuators for aircraft applications.
A piezo-electric pump is provided comprising: a main housing; a fluid reservoir located within the main housing; a piston head moveably mounted within the main housing; a piezo-electric stack; a bias mechanism arranged to couple the piston head and piezo-electric stack and maintain the piezo-electric stack in compression; an outlet plate statically mounted within the main housing adjacent to the piston head, wherein the adjacent surfaces of the outlet plate and piston head define a pumping chamber; an inlet disc valve arranged to permit a one-way flow of fluid from the reservoir into the pumping chamber; and an outlet disc valve arranged to permit a one-way flow of fluid out of the pumping chamber.
The combination of pre-loading of the piezo-electric stack in compression and use of inlet disc valve enables the piezo-electric pump described above to exhibit substantial improvement to the pressure and flow capability compared to other piezo-electric pumps.
The piezo-electric stack may be located between the piston head and a base plate and the bias mechanism may comprise a spring element arranged to exert a force biasing the piston head and base plate towards each other.
Maintaining the piezo-electric stack in compression has the advantage of avoiding undesirable tensile loads being applied to the stack in operation.
A piston rod may be coupled to the piston head and the piston rod extends from the piston head through the reservoir and the base plate and is coupled to the base plate. The piston rod may be coupled to the base plate by one or more retaining elements and the spring element is located between the retaining elements and the base plate. The spring element may comprise one or more Belleville washers.
Alternatively, the spring element may be arranged around the outside of the piezo-electric stack and is coupled to the piston head and the base plate.
The piezo-electric stack may include an internal void that comprises the fluid reservoir. This has the advantage of the pumping fluid within the reservoir acting as a coolant to prevent excessive heat build-up in the piezo-electric stack.
The piezo-electric pump may further include a fluid inlet port in fluid communication with the fluid reservoir.
One or more fluid inlet passages may be formed in the piston head providing fluid communication between the fluid reservoir and the pumping chamber and the inlet disc valve is arranged to prevent fluid flow from the pumping chamber into the fluid inlet passages.
Similarly, the one or more fluid outlet passages may be formed in the outlet plate providing fluid communication out of the pumping chamber into a fluid outlet chamber and the outlet disc valve is arranged to prevent fluid flow from the fluid outlet chamber into the fluid outlet passages.
Piezo pumps have the aforementioned benefit of reducing the number of components and the wearing surfaces of a traditional EHA solution. However to compete with a traditional EHA, there needs to be a substantial improvement in the pressure and flow capability. However, increasing the pressure and flow capability of a piezo-electric pump requires a number of challenges to be addressed.
The high frequency operation required to accumulate very small pumped volumes into appreciable flows results in the need for responsive valves controlling the flow of the pumped fluid into and out of the pumping chamber capable of operating at such high frequencies. Operating a piezo-electric stack at high frequencies generates a significant amount of heat in the stack, thereby requiring increased heat dissipation from the piezo stack. Also, the piezo-electric material making up the individual elements of a piezo-electric stack has significantly less ability to resist tensile loads than compression loads. Unless mitigated against, operating the piezo stack at high frequencies can result in high tensile loads being applied to the stack and a method of preloading the piezo stack to ensure tensile loads on the piezo stack are limited is therefore desirable.
Hydraulic fluid will exhibit some degree of compressibility, albeit small. This will arise, for example, from entrained air in the oil and inherent properties of the hydraulic fluid. Consequently, because the magnitude of motion provided by piezo-electric elements is small, the volume of the pumping chamber must be minimised to ensure that compressibility effects do not reduce the overall pressure capability of the pump.
As with all pumps, sealing of the pumping chamber is important to ensure that lost flow is minimised.
Integration of the pump to accommodate high frequency valves, methods of preloading and sealing whilst maintaining the required low pump chamber volumes all present technical problems that need to be addressed.
The Piezo-electric stack 106 is hollow, i.e. it is formed with an internal void 112. The void allows the pumped fluid to flow through the piezo-electric stack 106. Located between the piezo-electric stack 106 and the outlet plate 104 is a piston head 114. A piston rod (or tie rod) 116 extends from the piston head through the interior void of the piezo-electric stack and passes through a base plate 118 of the stack. The base plate 118 is arranged to be fixed relative to the main housing 102. The piston rod 116 is arranged to reciprocate with the piezo-electric stack through the base plate. The end of the piston rod 116 that protrudes beyond the base plate 118 within the housing 102 has one or more nuts 120 threaded onto it. One or more resilient elements 122, such as Belleville washers, are secured by the nuts between the nuts 120 and the base plate 118. The resilient elements 122 are held in compression against the base plate 118 by the nuts, and as a consequence exert a bias force through the piston rod and piston head to piezo-electric stack 106. This bias force provides a preloading to the piezo-electric stack such that the stack is permanently held in compression.
The base plate 118 has one or more fluid passages 124 formed in it that allow a flow of fluid into the void 112 within the piezo-electric stack 106. A fluid supply is provided, in use, to an inlet port in the main housing (not illustrated).
The space between the opposing faces of the piston head 114 and outlet plate 104 constitute a pumping chamber 126 (more easily seen in the subsequent figures). The piston head 114 includes one or more fluid inlet passages 128 that provide fluid communication between the internal void 112 of the piezo-electric stack and the pumping chamber 126. An inlet disc valve 130 is secured to the face of the piston head defining the pumping chamber and is arranged to control flow of the pumping fluid through the fluid inlet passages 128 from the void 112 into the pumping chamber 126. The outlet plate 104 also includes one or more fluid outlet passages 132 that provide fluid communication between the pumping chamber 126 and a fluid outlet chamber 134 of the pump 100 from which, in use, pressurised fluid is provided. An outlet disc valve 136 is secured to the face of the outlet plate 104 of the opposing face to that defining the pumping chamber, i.e. the face of the outlet plate adjacent to the fluid outlet chamber 134. The outlet disc valve 136 is arranged to control flow of the pumping fluid through the fluid outlet passages 132 from the pumping chamber 126 into the fluid outlet chamber 134.
The operation of the pump 100 will now be described with reference to
The movement of the piezo-electric stack 106 between the positions illustrated in
As also previously noted, operating the piezo-electric stack under a tensile load at the above mentioned frequencies is undesirable. This is overcome by use of the Belleville washers 122, which allow the piezo-electric stack 106 to be held in compression between the piston head 114 and the base plate 118 at all times, whilst still allowing the stack to extend and retract. The Belleville washers may be replaced with any other suitable resilient element, such as a coil spring, but the
Belleville washers have the advantage of providing a relatively high spring force for their overall size and displacement. Pre-loading the piezo stack with a Belleville washer can also increase the pressure capability of the pump by operating within the region of the Belleville washer spring curve characteristic where force is constant over displacement. Other mechanisms for pre-loading the piezo-electric stack may however be used, such as providing a spring or bellows around the outside of the stack and connected between the piston head 114 and the base plate 118 such that the spring tension acting on the piston head and base plate exerts a compressive force on the intervening stack elements.
To avoid any compressibility effects arising from the pumped fluid, and because the displacement of the piezo-electric stack is inherently small (of the order of sub-millimetre), the volume of the pumping chamber is kept to a minimum. For example, the pumping chamber volume may be of the order of 0.7 mL, with a length of 1mm. The overall length of the piezo-electric stack for such a pumping chamber volume will be of the order of 60-70mm. The dimensions are provided purely as an aid to understanding the scale of the pump and are not necessarily desired or preferred dimensions.
The high frequency operation required to accumulate very small pumped volumes into appreciable flows requires responsive valves. The dynamic capability of inlet and outlet disc valves meet this requirement. Additionally, the incorporation of the low profile inlet disc valve onto the piston head minimises the pumping chamber volume resulting in a higher pressure capability, as discussed above.
The combination of features (flow of pumped fluid through the hollow piezo-electric stack for cooling, pre-loading of the piezo-electric stack, and use of inlet and outlet disc valves) enables the piezo-electric pump described above to exhibit substantial improvements to the pressure and flow capability compared to other piezo-electric pumps. As a result, possible aircraft applications for such an improved piezo-electric pump include (but are not limited to) landing gear up-locks, lock-stays, gear door actuators, and brake and steering actuators, engines bleed valves, and aircraft environmental systems.
Number | Date | Country | Kind |
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21180101.4 | Jun 2021 | EP | regional |
Filing Document | Filing Date | Country | Kind |
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PCT/EP2022/066554 | 6/17/2022 | WO |