公开(公告)号：US20230227173A1

公开(公告)日：2023-07-20

申请号：US17577878

申请日：2022-01-18

Applicant: Lockheed Martin Corporation

Inventor： Michael A. Connor ,  Jesse Elia Morzel ,  Marc A. Antonetz ,  Igor Cherepinsky

IPC: B64D43/00 ,  H01H47/22

CPC classification number: B64D43/00 ,  H01H47/226

Abstract: A cockpit switch device can include a pushbutton switch, a bi-stable relay and a toggle component. The pushbutton switch can be configured to be manually actuated by a user into a command state. The bi-stable relay can be controlled by input commands from the pushbutton switch and input commands from a processor, and can be configured to control operation of one or more systems of an a aircraft. The toggle component can be connected to the pushbutton switch, the processor and the bi-stable relay. The toggle component can receive an input command signal from at least one of the pushbutton switch or the processor, and cause a state of the bi-stable relay to be flipped responsive to the input command signal from the at least one of the pushbutton switch or the processor.

公开(公告)号：US12060158B2

公开(公告)日：2024-08-13

申请号：US17577878

申请日：2022-01-18

Applicant: Lockheed Martin Corporation

Inventor： Michael A. Connor ,  Jesse Elia Morzel ,  Marc A. Antonetz ,  Igor Cherepinsky

IPC: B64D43/00 ,  H01H47/22

CPC classification number: B64D43/00 ,  H01H47/226

Abstract: A cockpit switch device can include a pushbutton switch, a bi-stable relay and a toggle component. The pushbutton switch can be configured to be manually actuated by a user into a command state. The bi-stable relay can be controlled by input commands from the pushbutton switch and input commands from a processor, and can be configured to control operation of one or more systems of an aircraft. The toggle component can be connected to the pushbutton switch, the processor and the bi-stable relay. The toggle component can receive an input command signal from at least one of the pushbutton switch or the processor, and cause a state of the bi-stable relay to be flipped responsive to the input command signal from the at least one of the pushbutton switch or the processor.

公开(公告)号：US12030624B2

公开(公告)日：2024-07-09

申请号：US17485192

申请日：2021-09-24

Applicant: Lockheed Martin Corporation

Inventor： Eric S. Parsons ,  Christopher Michael Colschen ,  Claude George Matalanis ,  Benjamin Edward Isabella ,  Marc A. Antonetz ,  Timothy James Conti ,  Frank M. Caputo

IPC: B64C27/473 ,  H02B1/20 ,  H02B1/26 ,  H02B1/30 ,  H02G15/007 ,  H02G15/06 ,  H02G15/18

CPC classification number: B64C27/473 ,  H02B1/202 ,  H02B1/26 ,  H02B1/305 ,  H02G15/007 ,  H02G15/06 ,  H02G15/1833

Abstract: An electrical conductor assembly for a rotor blade includes a substrate and at least one electrical conductor. The substrate includes an inboard end portion and an outboard end portion. The at least one electrical conductor is attached to the substrate and extends between the inboard end portion and the outboard end portion. The at least one electrical conductor is configured to transmit electricity along a length of the rotor blade. The inboard end portion and the outboard end portion are structured such that when the electrical conductor assembly is installed within the rotor blade, the inboard end portion is securable relative to the rotor blade and the outboard end portion is movable relative to the rotor blade.

公开(公告)号：US20240326994A1

公开(公告)日：2024-10-03

申请号：US18744276

申请日：2024-06-14

Applicant: Lockheed Martin Corporation

Inventor： Eric S. Parsons ,  Christopher Michael Colschen ,  Claude George Matalanis ,  Benjamin Edward Isabella ,  Marc A. Antonetz ,  Timothy James Conti ,  Frank M. Caputo

IPC: B64C27/473 ,  H02B1/20 ,  H02B1/26 ,  H02B1/30 ,  H02G15/007 ,  H02G15/06 ,  H02G15/18

CPC classification number: B64C27/473 ,  H02B1/202 ,  H02B1/26 ,  H02B1/305 ,  H02G15/007 ,  H02G15/06 ,  H02G15/1833

Abstract: A method of manufacturing an electrical conductor assembly includes attaching a substrate and at least one electrical conductor to a cable assembly machine, tensioning the substrate, and holding the substrate stationary while wrapping the at least one electrical conductor around the substrate. The at least one electrical conductor is wrapped around the substrate independent of the tension on the substrate.

公开(公告)号：US20230098029A1

公开(公告)日：2023-03-30

申请号：US17485192

申请日：2021-09-24

Applicant: Lockheed Martin Corporation

Inventor： Eric S. Parsons ,  Christopher Michael Colschen ,  Claude George Matalanis ,  Benjamin Edward Isabella ,  Marc A. Antonetz ,  Timothy James Conti ,  Frank M. Caputo

IPC: B64C27/68 ,  H01B7/18 ,  H02G15/007 ,  H02G15/06 ,  H01B13/22

Abstract: An electrical conductor assembly for a rotor blade includes a substrate and at least one electrical conductor. The substrate includes an inboard end portion and an outboard end portion. The at least one electrical conductor is attached to the substrate and extends between the inboard end portion and the outboard end portion. The at least one electrical conductor is configured to transmit electricity along a length of the rotor blade. The inboard end portion and the outboard end portion are structured such that when the electrical conductor assembly is installed within the rotor blade, the inboard end portion is securable relative to the rotor blade and the outboard end portion is movable relative to the rotor blade.