Power transfer unit with breakout friction reduction and leakage reduction
A power transfer unit includes a first hydraulic circuit, a second hydraulic circuit fluidly connected to the first hydraulic circuit, a pump and motor assembly fluidly connected between the first hydraulic circuit and the second hydraulic circuit, an isolation valve arranged along the first hydraulic circuit and fluidly connected to an inlet of the pump and motor assembly. The isolation valve is movable between a closed position and an open position to prevent and enable high-pressure fluid flow to the inlet, respectively. An unloader valve is arranged along the second hydraulic circuit and fluidly connected to an outlet of the pump and motor assembly, and an orifice is arranged along the second hydraulic circuit and fluidly connected to the unloader valve to reduce back pressure in the second hydraulic circuit.
1. A power transfer unit comprising:
a first hydraulic circuit;
a second hydraulic circuit operatively coupled to the first hydraulic circuit;
a pump and motor assembly fluidly connected between the first hydraulic circuit and the second hydraulic circuit;
an isolation valve arranged along the first hydraulic circuit and fluidly connected to an inlet of the pump and motor assembly, wherein the isolation valve is movable between a closed position and an open position to prevent and enable high-pressure fluid flow to the inlet, respectively;
an unloader valve arranged along the second hydraulic circuit and fluidly connected to an outlet of the pump and motor assembly;
an orifice arranged along the second hydraulic circuit and fluidly connected to the unloader valve to reduce back pressure in the second hydraulic circuit; and
an arming valve arranged along the first hydraulic circuit for piloting the isolation valve, wherein the arming valve is a three-way normally open solenoid valve.
2. The power transfer unit of claim 1 further comprising a low-pressure pilot pump arranged along the second hydraulic circuit and coupled for rotation with the pump and motor assembly.
3. The power transfer unit of claim 2 , wherein the low-pressure pilot pump is communicatively coupled to the unloader valve and the isolation valve.
4. The power transfer unit of claim 3 , wherein the low-pressure pilot pump is a gerotor.
5. The power transfer unit of claim 1 further comprising a check valve arranged along the second hydraulic circuit.
6. The power transfer unit of claim 1 further comprising a compensator valve that is arranged along the first hydraulic circuit and fluidly connected to the isolation valve.
7. The power transfer unit of claim 6 , wherein the outlet of the pump and motor assembly is communicatively coupled with the compensator valve.
8. The power transfer unit of claim 1 , wherein the first hydraulic circuit and the second hydraulic circuit are arranged for unidirectional flow from the first hydraulic circuit to the second hydraulic circuit.
9. The power transfer unit of claim 1 , wherein the unloader valve is spring-biased in a normally open position.
10. The power transfer unit of claim 1 , wherein the isolation valve is spring-biased in a normally closed position.
11. The power transfer unit of claim 1 further comprising a relief valve arranged along the second hydraulic circuit.
12. The power transfer unit of claim 1 , wherein the pump and motor assembly includes a motor arranged along the first hydraulic circuit and a pump arranged along the second hydraulic circuit.
13. An aircraft control system comprising:
a first hydraulic system; and
a second hydraulic system independent from the first hydraulic system;
wherein a power transfer unit according to claim 1 is connected between the first hydraulic system and the second hydraulic system for transferring power between the first hydraulic system and the second hydraulic system.
14. A power transfer unit comprising:
a first hydraulic circuit;
a second hydraulic circuit operatively coupled to the first hydraulic circuit;
a pump and motor assembly fluidly connected between the first hydraulic circuit and the second hydraulic circuit;
an isolation valve arranged along the first hydraulic circuit and fluidly connected to an inlet of the pump and motor assembly, wherein the isolation valve is movable between a closed position and an open position to prevent and enable high-pressure fluid flow to the inlet, respectively;
an unloader valve arranged along the second hydraulic circuit and fluidly connected to an outlet of the pump and motor assembly;
an orifice arranged along the second hydraulic circuit and fluidly connected to the unloader valve to reduce back pressure in the second hydraulic circuit; and
a low-pressure pilot pump arranged along the second hydraulic circuit and coupled for rotation with the pump and motor assembly, wherein the low-pressure pilot pump is communicatively coupled to the unloader valve and the isolation valve.
15. The power transfer unit of claim 14 , wherein the low-pressure pilot pump is a gerotor.