Sacrificial anode
    2.
    发明授权
    Sacrificial anode 有权
    牺牲阳极

    公开(公告)号:US09045834B2

    公开(公告)日:2015-06-02

    申请号:US13657288

    申请日:2012-10-22

    Inventor: Alexis Lambourne

    Abstract: This invention relates to a sacrificial anode, comprising: a first layer of a first material; and, a second layer of a second material which is electrically connected to the first layer, wherein the first material is more anodic with respect to a galvanic series than the second material. The invention also relates to a body including the sacrificial anode.

    Abstract translation: 本发明涉及一种牺牲阳极,包括:第一材料的第一层; 以及电连接到第一层的第二材料的第二层,其中第一材料相对于比第二材料的电流系列更阳极。 本发明还涉及包括牺牲阳极的主体。

    Aircraft comprising hydrogen storage tanks

    公开(公告)号:US11905028B2

    公开(公告)日:2024-02-20

    申请号:US17562775

    申请日:2021-12-27

    CPC classification number: B64D37/30 B64C1/22 B64D37/04 B64D37/06

    Abstract: An aircraft comprises a hydrogen-fuelled propulsion system, a plurality of like generally cylindrical hydrogen storage tanks and a conveying system arranged to convey hydrogen from the hydrogen storage tanks to the hydrogen-fuelled propulsion system. The aircraft further comprises a fuselage having a cargo bay (502) including one or more (510A-G) of the plurality of hydrogen storage tanks, the longitudinal axes (511A-G) of the one or more hydrogen storage tanks within the cargo bay extending parallel to the longitudinal axis (501) of the fuselage and lying in one or more planes (595, 597) extending across the width dimension of the cargo bay. The hydrogen storage tanks within the cargo bay have a common aspect ratio R in the range 4.2≤R≤25.7, allowing the volume of space with the cargo bay occupied by stored hydrogen to be maximised or approximately maximised.

    BLADED DISC
    4.
    发明公开
    BLADED DISC 审中-公开

    公开(公告)号:US20230203956A1

    公开(公告)日:2023-06-29

    申请号:US18062734

    申请日:2022-12-07

    CPC classification number: F01D5/3007 F02C7/36 F01D5/02 F03G7/0614

    Abstract: A bladed disc for a rotating machine comprising a central disc that rotates about a central axis, the central disc having a series of blades arranged around its periphery; the blades have dovetail roots which engage with slots on the central disc; the bladed disc being configured so that there is a pre-loading force between the blades and the central disc such that each blade is forced away from the central axis of the bladed disc; and wherein the pre-loading force is equal or greater than 40% of the maximum centrifugal force applied to the blade during a flight cycle.

    Induction motor rotor and a method of manufacturing the same

    公开(公告)号:US10951101B2

    公开(公告)日:2021-03-16

    申请号:US15357647

    申请日:2016-11-21

    Abstract: A method of manufacturing an induction motor rotor assembly, the method includes the steps of: providing a rotor; machining a plurality of re-entrant slots axially along an outer surface of the rotor; positioning a sleeve concentrically over the outer surface of the rotor; applying a friction stir welding process to the sleeve along each re-entrant slot axially along the outer surface of the rotor to cause the sleeve material to plasticise and flow into the axial re-entrant slot to form an axial re-entrant slot bar; and providing an electrical connection at each of the opposing axial ends of the rotor between respective ones of opposing ends of each of the axial re-entrant slot bars to thereby form the induction motor rotor.

    Composite gas storage tank
    7.
    发明授权

    公开(公告)号:US11828415B2

    公开(公告)日:2023-11-28

    申请号:US17398174

    申请日:2021-08-10

    Inventor: Alexis Lambourne

    Abstract: A composite gas storage tank includes a composite wall defining a main storage volume and a hollow conduit portion communicating with and extending away from the main storage volume. A hollow coupling element has a length portion which is partially embedded within and extends substantially parallel to the hollow conduit portion of the composite wall. The hollow conduit portion and the coupling element provide communication between the main storage volume and the tank exterior. A leakage path around the hollow coupling element is significantly longer than those of tanks of the prior art and reduces the rate at which hydrogen leaks from the tank. A carbon fibre filament winding extends over the length of the hollow conduit portion and provides a radially inwardly-directed force biasing the carbon fibre material of the hollow conduit portion into contact with the coupling element, further reducing the leakage rate on the leakage path.

    Electrical machine winding assembly and method of manufacture thereof

    公开(公告)号:US11329536B2

    公开(公告)日:2022-05-10

    申请号:US16558652

    申请日:2019-09-03

    Abstract: A method of manufacturing a winding assembly for an electrical machine, the method comprising: selecting (S1) a mathematical function defining the spatial separation between adjacent turns of a winding path, the mathematical function dependent on one or more parameters of the electrical machine and/or of the anticipated operating environment of the electrical machine; forming (S2), by three-dimensional, 3D, printing, an electrically insulating body comprising a channel defining the winding path in accordance with said function, the channel having an inlet and an outlet; heating (S3) the electrically insulating body to a temperature above the melting point of an electrically conducting material; flowing (S4) the electrically conducting material through the inlet to the outlet to fill the channel; and cooling the electrically insulating body to solidify the electrically conducting material within the channel, thereby forming said winding assembly.

Patent Agency Ranking