Direct control for variable displacement pumps
US-2024240631-A1 · Jul 18, 2024 · US
US10138816B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10138816-B2 |
| Application number | US-201514858614-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 18, 2015 |
| Priority date | Nov 20, 2014 |
| Publication date | Nov 27, 2018 |
| Grant date | Nov 27, 2018 |
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A fuel pumping unit has a low pressure centrifugal pump and a high pressure centrifugal pump. In use, the low pressure pump supplies fuel at a boosted pressure to the high pressure pump for onward supply to a fuel metering unit. The pumping unit further has a drive input which drives the low and high pressure pumps. A gear arrangement is operatively located between the drive input and the low and high pressure pumps such that the low and high pressure pumps are driven at different speeds by the drive input.
Opening claim text (preview).
The invention claimed is: 1. A fuel pumping unit comprising: a low pressure centrifugal pump and a high pressure centrifugal pump, the low pressure centrifugal pump supplying fuel at a boosted pressure to the high pressure centrifugal pump for onward supply to a fuel metering unit; a drive input that drives the low pressure centrifugal pump and the high pressure centrifugal pump, the drive input being a single input drive shaft from an engine accessory gearbox; a gear arrangement that is operatively located between the drive input and the low pressure centrifugal pump and the high pressure centrifugal pump such that the low pressure centrifugal pump and the high pressure centrifugal pump are driven at different speeds by the drive input; a positive displacement start pump that is driven by the drive input via the gear arrangement; and a selector valve that is configured to selectably provide a high pressure mode, a low pressure mode, and a start mode, wherein: in the high pressure mode, the low pressure centrifugal pump supplies fuel at the boosted pressure to the high centrifugal pressure pump for onward supply to the fuel metering unit, the selector valve isolating the start pump or recirculating fuel between the start pump and the selector valve; in the low pressure mode, the fuel supply from the low pressure centrifugal pump to the high pressure centrifugal pump is shut off such that the high pressure centrifugal pump runs dry and the low pressure centrifugal pump supplies fuel to the fuel metering unit, the selector valve isolating the start pump or recirculating fuel between the start pump and the selector valve; and in the start mode, the low pressure centrifugal pump supplies fuel at the boosted pressure to the start pump for onward supply to the fuel metering unit, and the fuel supply from the low pressure centrifugal pump to the high pressure centrifugal pump is shut off such that the high pressure centrifugal pump runs dry. 2. The fuel pumping unit according to claim 1 , wherein the high pressure centrifugal pump is driven at a higher speed than the low pressure centrifugal pump. 3. The fuel pumping unit according to claim 1 , wherein the gear arrangement includes a bevel gear drive. 4. The fuel pumping unit according to claim 1 , further having an axial flow inducer at an inlet to the low pressure centrifugal pump. 5. The fuel pumping unit according to claim 1 , wherein rotation axes of the low pressure centrifugal pump and the high pressure centrifugal pump are inclined relative to each other. 6. The fuel pumping unit according to claim 1 , wherein the low pressure centrifugal pump and the start pump are driven at the same speed by the drive input. 7. The fuel pumping unit according to claim 1 , wherein the fuel pumping unit is suitable for pumping fuel for an aero-engine. 8. An aero-engine having the fuel pumping unit according to claim 1 .
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