Taxi vehicle for moving an aircraft

US10569904B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10569904-B2
Application numberUS-201715805419-A
CountryUS
Kind codeB2
Filing dateNov 7, 2017
Priority dateNov 16, 2016
Publication dateFeb 25, 2020
Grant dateFeb 25, 2020

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  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

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Abstract

Official abstract text for this publication.

In one aspect, there is disclosed a taxi vehicle comprising a chassis having a coupler to connect to a coupling location of a craft and a set of wheels with at least one electric motor coupled to the set of wheels. The taxi vehicle can include a fuel cell coupled to the at least one electric motor and a battery coupled to the fuel cell. The battery can be configured to supply peak power demand to the at least one electric motor to start moving the craft. The battery can receive charging from the fuel cell when not supplying peak power demand while the fuel cell supplies power to the at least one electric motor to continue moving the craft.

First claim

Opening claim text (preview).

The invention claimed is: 1. A taxi vehicle for moving a craft, the taxi vehicle comprising: a chassis having a coupler to connect to a coupling location of the craft; a set of wheels to move the chassis; a hybrid fuel cell engine including a fuel cell and a gas turbine engine; at least one electric motor coupled to the set of wheels; the fuel cell in the chassis coupled to the at least one electric motor to energize the at least one electric motor; and a battery coupled to the fuel cell and to the at least one electric motor, wherein the battery is configured to supply peak power demand to the at least one electric motor to start moving the craft or to start the fuel cell, and to receive charge from the fuel cell when not supplying peak power demand while the fuel cell supplies power to the at least one electric motor to continue moving the craft. 2. The taxi vehicle of claim 1 , wherein the fuel cell is one of a solid oxide fuel cell or a molten carbonate fuel cell. 3. The taxi vehicle of claim 1 , wherein the craft is an aircraft and the coupling location is a nose wheel of the aircraft. 4. The taxi vehicle of claim 3 , further comprising a power connector to provide electrical power from the fuel cell to the aircraft. 5. The taxi vehicle of claim 4 , wherein the gas turbine engine provides a pneumatic power deliverable to the aircraft through the power connector. 6. The taxi vehicle of claim 3 , wherein the coupler is a lift mechanism to engage and lift the nose wheel. 7. The taxi vehicle of claim 6 , wherein the chassis comprises a hydraulic pump powered by the fuel cell and the lift mechanism includes a hydraulic supply connected to the hydraulic pump. 8. The taxi vehicle of claim 1 , further comprising a power connector to provide electrical power from the fuel cell to the craft. 9. The taxi vehicle of claim 8 , wherein the gas turbine engine provides a pneumatic power deliverable to the aircraft through the power connector. 10. The taxi vehicle of claim 8 , wherein the coupler is a lift mechanism and the power connector is part of the lift mechanism to connect electrical power to the craft as the lift mechanism engages and lifts the craft at the coupling location. 11. A method of moving and starting a craft using a taxi vehicle, wherein the taxi vehicle comprises: a chassis having a coupler to connect to a coupling location of the craft; a set of wheels to move the chassis; at least one electric motor coupled to the set of wheels; a hybrid fuel cell engine including a fuel cell and a gas turbine engine; the fuel cell in the chassis coupled to the at least one electric motor to energize the at least one electric motor; and a battery coupled to the fuel cell and to the at least one electric motor, wherein the battery is configured to supply peak power demand to the at least one electric motor to start moving the craft or to start the fuel cell, and to receive charge from the fuel cell when not supplying peak power demand while the fuel cell supplies power to the at least one electric motor to continue moving the craft; the method comprising: engaging a coupling location of the craft with a coupler of a taxi vehicle powered by a fuel cell and a battery coupled to at least one electric motor to move the taxi vehicle; connecting electrical power from the fuel cell to the craft and a pneumatic supply from the taxi vehicle to the craft while engaging the coupling location; driving the taxi vehicle to a starting point for the craft; and starting the craft using the electrical power and the pneumatic supply from the taxi vehicle. 12. The method of claim 11 , further comprising disengaging the coupling location from the coupler and disconnecting the electrical power and the pneumatic supply from the craft after the craft is started. 13. The method of claim 11 , wherein the craft is an aircraft and the coupling location is a nose wheel of the aircraft. 14. The method of claim 13 , wherein the coupler is a lift mechanism to engage and lift the nose wheel. 15. The method of claim 11 , wherein the starting point is a holding area near a runway remote from an airport terminal. 16. The method of claim 11 , further comprising automatically coupling hydraulic power from the taxi vehicle to the craft while engaging the coupling location. 17. The method of claim 11 , further comprising driving the taxi vehicle by remote control from a location inside the craft. 18. A method of moving an aircraft using a taxi vehicle wherein the taxi vehicle comprises: a chassis having a coupler to connect to a coupling location of the craft; a set of wheels to move the chassis; at least one electric motor coupled to the set of wheels; a hybrid fuel cell engine including a fuel cell and a gas turbine engine; the fuel cell in the chassis coupled to the at least one electric motor to energize the at least one electric motor; and a battery coupled to the fuel cell and to the at least one electric motor, wherein the battery is configured to supply peak power demand to the at least one electric motor to start moving the craft or to start the fuel cell, and to receive charge from the fuel cell when not supplying peak power demand while the fuel cell supplies power to the at least one electric motor to continue moving the craft; the method comprising: engaging a nose wheel of the aircraft with a coupler of a taxi vehicle powered by a fuel cell and a battery coupled to at least one electric motor to move the taxi vehicle from a first location; connecting electrical power from the fuel cell to the aircraft and a pneumatic supply from the taxi vehicle to the aircraft while engaging the nose wheel; driving the taxi vehicle to a second location; attaching a ground power supply to the aircraft; and disengaging the nose wheel of the aircraft from the coupler, and disconnecting the electrical power and the pneumatic supply from the aircraft after the ground power supply is attached. 19. The method of claim 18 , wherein the coupler is a lift mechanism to engage and lift the nose wheel.

Assignees

Inventors

Classifications

  • B64F1/227Primary

    for direct connection to aircraft, e.g. tow tractors without towing bars · CPC title

  • B64F1/225Primary

    Vehicles specially adapted therefor, e.g. aircraft tow tractors · CPC title

  • Electric power distribution systems onboard aircraft · CPC title

  • for starting propulsion plant · CPC title

  • Mobile units · CPC title

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Frequently asked questions

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What does patent US10569904B2 cover?
In one aspect, there is disclosed a taxi vehicle comprising a chassis having a coupler to connect to a coupling location of a craft and a set of wheels with at least one electric motor coupled to the set of wheels. The taxi vehicle can include a fuel cell coupled to the at least one electric motor and a battery coupled to the fuel cell. The battery can be configured to supply peak power demand …
Who is the assignee on this patent?
GE Aviation Systems Limted, Ge Aviat Systems Ltd
What technology area does this patent fall under?
Primary CPC classification B64F1/227. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Feb 25 2020 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).