FUEL DELIVERY SYSTEM
    11.
    发明申请

    公开(公告)号:US20230092811A1

    公开(公告)日:2023-03-23

    申请号:US17823732

    申请日:2022-08-31

    Inventor: Chloe J. PALMER

    Abstract: A fuel delivery system for a gas turbine engine comprises a cryogenic fuel tank, a first fuel line for connection to the cryogenic fuel tank, a fuel pump connected to receive fuel via the first fuel line, a plurality of fuel lines connecting the fuel pump to a combustor of the gas turbine engine, a controller configured to operate the fuel delivery system, a purge gas tank connected to the first fuel line and configured to store a purge gas for purging the plurality of fuel lines and a fuel gas tank connected to the first fuel line and configured to store a fuel gas for flushing purge gas from the plurality of fuel lines.

    ELECTRIC TURBOMACHINE
    12.
    发明申请

    公开(公告)号:US20200263545A1

    公开(公告)日:2020-08-20

    申请号:US16779712

    申请日:2020-02-03

    Abstract: Turbomachinery comprising first and second sets of rotors configured to operate on a working fluid. The machinery further comprises first and second sets of electric machines coupled to the respective first and second rotors, and a coupling arrangement arranged to couple adjacent rotors of the first and second rotor sets to provide for fixed ratio, contra-rotation of the first and second rotor sets.

    SUPERCONDUCTING ELECTRICAL POWER DISTRIBUTION NETWORK

    公开(公告)号:US20200243225A1

    公开(公告)日:2020-07-30

    申请号:US16734480

    申请日:2020-01-06

    Inventor: Chloe J. PALMER

    Abstract: A superconducting electrical power distribution network has a superconducting bus bar and superconducting cables electrically connected to the bus bar at respective joints distributed along the bus bar. The network further has a first coolant system for providing first cryogenic fluid and first circuits for circulating the first cryogenic fluid provided by the first coolant system. The first circuits comprise: a bus bar flow path which extends along and thereby cools the bus bar, cable flow paths which respectively extend along and thereby cool the cables, cooling junctions where the bus bar and cable flow paths meet at the electrical connection joints, inflow lines which send the first cryogenic fluid from the first coolant system to the flow paths, and outflow lines which remove the first cryogenic fluid from the flow paths.

    HEAT EXCHANGER
    14.
    发明申请
    HEAT EXCHANGER 审中-公开

    公开(公告)号:US20200224975A1

    公开(公告)日:2020-07-16

    申请号:US16716873

    申请日:2019-12-17

    Inventor: Chloe J. PALMER

    Abstract: The present disclosure concerns a heat exchanger, which may for example be utilised in a gas turbine engine or in other applications. Example embodiments include a heat exchanger comprising: an external surface for exchanging heat with an external fluid flow passing over the external surface; a first fluid passage extending through the heat exchanger from a first fluid inlet to a first fluid outlet, a first portion of the first fluid passage extending along the heat exchanger adjacent to the external surface for a first cooling fluid passing through the first fluid passage to exchange heat with the external fluid flow; and a second fluid passage extending through the heat exchanger from a second fluid inlet to a second fluid outlet located at the external surface for a second cooling fluid to pass from the second fluid inlet into the external fluid flow.

    AIRCRAFT WING COMPRISING A STORAGE TANK FOR GASEOUS HYDROGEN

    公开(公告)号:US20250115347A1

    公开(公告)日:2025-04-10

    申请号:US18729431

    申请日:2023-01-04

    Abstract: A storage tank for gaseous hydrogen includes a continuous tank wall defining a serial array of hollow elongate tank portions of substantially constant cross-section and hollow connecting portions defining an internal storage volume, wherein adjacent ends of any pair of adjacent hollow elongate tank portions are connected by a hollow connecting portion having a cross-sectional dimension smaller than those of the adjacent hollow elongate tanks portions. The tank may be included in an aircraft wing such that it extends spanwise through one or more internal spars of the wing, thus providing a continuous gas storage volume at a given chordwise position notwithstanding the spars, and providing for storage of gaseous hydrogen at higher gravimetric efficiency than is achievable by a plurality of coupled discrete tanks disposed between the spars.

    GAS TURBINE ENGINE FUEL SYSTEM
    17.
    发明公开

    公开(公告)号:US20240229717A9

    公开(公告)日:2024-07-11

    申请号:US18379717

    申请日:2023-10-13

    CPC classification number: F02C7/224 F02C3/22 F02C7/14

    Abstract: A gas turbine engine fuel system includes a fuel offtake configured to divert a portion of hydrogen fuel from a main fuel conduit, a burner configured to burn the portion of hydrogen fuel diverted from the main fuel conduit, a heat exchanger configured to transfer heat from exhaust gasses produced by the burner to hydrogen fuel in the main fuel conduit and a power recovery device configured to extract power from exhaust gasses of the burner downstream of the heat-exchanger.

    GAS TURBINE ENGINE FUEL SYSTEM
    18.
    发明公开

    公开(公告)号:US20240133343A1

    公开(公告)日:2024-04-25

    申请号:US18379717

    申请日:2023-10-12

    CPC classification number: F02C7/224 F02C3/22 F02C7/14

    Abstract: A gas turbine engine fuel system includes a fuel offtake configured to divert a portion of hydrogen fuel from a main fuel conduit, a burner configured to burn the portion of hydrogen fuel diverted from the main fuel conduit, a heat exchanger configured to transfer heat from exhaust gasses produced by the burner to hydrogen fuel in the main fuel conduit and a power recovery device configured to extract power from exhaust gasses of the burner downstream of the heat-exchanger.

    COMBINED GAS TURBINE ENGINE AND FUEL CELL
    19.
    发明公开

    公开(公告)号:US20240133340A1

    公开(公告)日:2024-04-25

    申请号:US18379728

    申请日:2023-10-12

    Abstract: A combined gas turbine engine and hydrogen fuel cell system includes a hydrogen fuelled gas turbine engine, a cryogenic liquid hydrogen fuel tank, a first fuel offtake configured and arranged to divert a portion of hydrogen fuel from a main fuel conduit, a burner configured and arranged to burn the portion of hydrogen fuel diverted from the main fuel conduit, a heat exchanger configured and arranged to transfer heat from exhaust gasses produced by the burner to hydrogen fuel in the main fuel conduit, a second fuel offtake arranged to divert a portion of hydrogen fuel from the main fuel conduit downstream of the heat exchanger, and a hydrogen fuel cell configured and arranged to produce electric power using hydrogen fuel diverted from the second fuel offtake.

    SUPERCONDUCTING ELECTRICAL POWER DISTRIBUTION SYSTEM

    公开(公告)号:US20200244130A1

    公开(公告)日:2020-07-30

    申请号:US16734491

    申请日:2020-01-06

    Inventor: Chloe J. PALMER

    Abstract: A superconducting electrical power distribution system has a superconducting bus bar and one or more bus bar thermal conductor lines extending in thermal proximity along the bus bar to receive heat from the bus bar over the length of the bus bar. The system further has superconducting cables electrically connected to the bus bar at respective electrical joints distributed along the bus bar. The system further has a cryogenic cooling sub-system. The system further has a network comprising first and second thermal conductor lines, each line comprising a cold end which is cooled by the cryogenic cooling sub-system, and an opposite hot end, whereby heat received by each line is normally conducted along the line in a direction from its hot end to its cold end.

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