Emergency power supply system, aircraft having such an emergency power supply system and a method for providing at least electric power and hydraulic power in case of an emergency in an aircraft
US-10676208-B2 · Jun 9, 2020 · US
US10926870B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10926870-B2 |
| Application number | US-201715824528-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 28, 2017 |
| Priority date | Dec 5, 2016 |
| Publication date | Feb 23, 2021 |
| Grant date | Feb 23, 2021 |
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A method and apparatus for operating a power system architecture including an electrical power storage system, a power distribution bus selectively connected with the electrical power storage device, a hydraulic pump selectively connected with the electrical power storage device and a controller module communicatively connected with the electrical power storage system and the hydraulic pump.
Opening claim text (preview).
The invention claimed is: 1. A power system architecture comprising: a rechargeable electrical power storage system; a connection between the electrical power storage system and a power distribution bus; a hydraulic pump/generator selectively connected with the rechargeable electrical power storage system, and configured to operate as a motor to provide hydraulic power to a hydraulic system and as a generator to generate electrical power from hydraulic power stored in a hydraulic system; and a controller module communicatively coupled with the connection and the hydraulic pump/generator, and configured to selectively actuate the connection upon receiving a power demand signal indicative of a demand for supplemental electrical power to controllably operate at least one of the electrical power storage system or the hydraulic pump/generator in response to the power demand signal. 2. The power system architecture of claim 1 , wherein the power demand signal is indicative of a demand for emergency electrical power. 3. The power system architecture of claim 2 , wherein the electrical power storage system is the only available source of emergency electrical power. 4. The power system architecture of claim 3 , wherein the electrical power storage system is a bank of batteries. 5. The power system architecture of claim 4 , where at least a subset of the bank of batteries are rechargeable batteries. 6. The power system architecture of claim 5 , wherein the rechargeable batteries are recharged by the power system architecture. 7. The power system architecture of claim 6 , wherein the bank of batteries are sized to controllably supply power from the power storage system to the power distribution bus. 8. The power system architecture of claim 7 , wherein the bank of batteries are disposed about an aircraft. 9. The power system architecture of claim 8 , wherein the bank of batteries are disposed about an aircraft to provide aircraft balance during flight operations. 10. The power system architecture of either of claim 2 , wherein the power distribution bus is an emergency power distribution bus. 11. The power system architecture of claim 1 , wherein the electrical power storage system includes at least one rechargeable battery, and wherein the hydraulic pump/generator is configured to recharge the at least one rechargeable battery when operating as a generator. 12. A method of operating a power system architecture, comprising: receiving, by a control module, a demand signal indicative of at least one of an emergency demand for electrical power or an emergency demand for hydraulic power; and in response to receiving the demand signal, controlling, by the control module, a supplying of electrical power stored in an electrical power storage system to a respective emergency power bus and to a hydraulic pump motor, and to a set of hydraulic loads wherein supplying electrical power is proportional to the emergency demand. 13. The method of claim 12 , further comprising receiving, by the control module a hydraulic demand signal indicative of the emergency demand for hydraulic power and an electrical demand signal indicative of the emergency demand for electrical power. 14. The method of claim 13 , further comprising operating a hydraulic pump/generator as a generator in response to receiving a hydraulic demand signal that does not indicate an emergency demand for hydraulic power.
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