Power transmission
AssigneeVickers, Incorporated
InventorLowell D. Hansen
Life of this patent
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AssigneeVickers, Incorporated
InventorLowell D. Hansen
Estimating the term…
A rotary hydraulic vane pump includes a rotor mounted within a housing, with a plurality of vanes individually slidably disposed in corresponding slots in the rotor periphery. A cam ring surrounds the rotor within the housing and has a radially inwardly facing vane track defining as least one arcuate fuel pressure cavity between the rotor and the cam ring. A fuel inlet in the housing includes a primary inlet port opening into the cavity at the leading circumferential edge of the cavity with respect to the direction of rotation of the rotor within the housing. A pump outlet includes an outlet port that opens into the cavity adjacent to the trailing circumferential edge of the cavity. A secondary inlet port opens into the cavity circumferentially between the primary inlet port and the outlet port, and is directly connected to the pump outlet port such that fluid, at outlet pressure is available at the secondary inlet port. A pressurization valve, having a predetermined threshold pressure for permitting flow of fluid therethrough, is connected between the pump outlet and the primary pump inlet port.
A two-stage fuel pump for aircraft turbine engine applications comprising:
The pump set forth in claim 9 wherein said vane pump fluid inlet means comprises at least one inlet passage extending radially from said cavity, and wherein said pump fluid inlet includes an axial inlet passage in said housing aligned with said shaft, a cylindrical filter coaxially surrounding said inlet passage, and a chamber externally surrounding said filter for receiving filtered inlet fluid flowing radially through said filter,
Dependencies are inferred from the claim text.