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1.发明申请公开(公告)号：US20230054703A1
公开(公告)日：2023-02-23
申请号：US17977965
申请日：2022-10-31
发明人： Joseph Pantalone, III , Timothy James Conti , Daniel Caleb Sargent , Benjamin Edward Isabella , Masruk Siddique
摘要： A replacement tip section for a rotor blade, from which a legacy tip section was removed, includes a blade tip portion configured to be attached to an intermediate section of the rotor blade after removal of the legacy section. The intermediate section has a connection feature at an end of the intermediate section to which the blade tip portion is attachable. The replacement tip section includes a transition region configured to be attached to a forward end of the connection feature. The transition region is configured to form a leading edge of the rotor blade and extends from the blade tip portion to form an opening into which the intermediate section is attached. The transition region includes a first end having a first airfoil that conforms to the intermediate section airfoil at the connection feature, and a second end having a second airfoil that conforms to the blade tip portion.
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2.发明授权公开(公告)号：US12037108B2
公开(公告)日：2024-07-16
申请号：US17977965
申请日：2022-10-31
发明人： Joseph Pantalone, III , Timothy James Conti , Daniel Caleb Sargent , Benjamin Edward Isabella , Masruk Siddique
CPC分类号： B64C27/463 , B64F5/40 , Y10T29/49732
摘要： A replacement tip section for a rotor blade, from which a legacy tip section was removed, includes a blade tip portion configured to be attached to an intermediate section of the rotor blade after removal of the legacy section. The intermediate section has a connection feature at an end of the intermediate section to which the blade tip portion is attachable. The replacement tip section includes a transition region configured to be attached to a forward end of the connection feature. The transition region is configured to form a leading edge of the rotor blade and extends from the blade tip portion to form an opening into which the intermediate section is attached. The transition region includes a first end having a first airfoil that conforms to the intermediate section airfoil at the connection feature, and a second end having a second airfoil that conforms to the blade tip portion.
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公开(公告)号：US12030624B2
公开(公告)日：2024-07-09
申请号：US17485192
申请日：2021-09-24
发明人： Eric S. Parsons , Christopher Michael Colschen , Claude George Matalanis , Benjamin Edward Isabella , Marc A. Antonetz , Timothy James Conti , Frank M. Caputo
IPC分类号： B64C27/473 , H02B1/20 , H02B1/26 , H02B1/30 , H02G15/007 , H02G15/06 , H02G15/18
CPC分类号： B64C27/473 , H02B1/202 , H02B1/26 , H02B1/305 , H02G15/007 , H02G15/06 , H02G15/1833
摘要： 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.
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4.发明公开公开(公告)号：US20240326994A1
公开(公告)日：2024-10-03
申请号：US18744276
申请日：2024-06-14
发明人： Eric S. Parsons , Christopher Michael Colschen , Claude George Matalanis , Benjamin Edward Isabella , Marc A. Antonetz , Timothy James Conti , Frank M. Caputo
IPC分类号： B64C27/473 , H02B1/20 , H02B1/26 , H02B1/30 , H02G15/007 , H02G15/06 , H02G15/18
CPC分类号： B64C27/473 , H02B1/202 , H02B1/26 , H02B1/305 , H02G15/007 , H02G15/06 , H02G15/1833
摘要： 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.
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公开(公告)号：US20230098029A1
公开(公告)日：2023-03-30
申请号：US17485192
申请日：2021-09-24
发明人： Eric S. Parsons , Christopher Michael Colschen , Claude George Matalanis , Benjamin Edward Isabella , Marc A. Antonetz , Timothy James Conti , Frank M. Caputo
IPC分类号： B64C27/68 , H01B7/18 , H02G15/007 , H02G15/06 , H01B13/22
摘要： 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.
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6.发明授权公开(公告)号：US11498671B2
公开(公告)日：2022-11-15
申请号：US16690447
申请日：2019-11-21
发明人： Joseph Pantalone, III , Timothy James Conti , Daniel Caleb Sargent , Benjamin Edward Isabella , Masruk Siddique
摘要： A replacement tip section for a rotor blade, from which a legacy tip section was removed, includes a blade tip portion configured to be attached to an intermediate section of the rotor blade after removal of the legacy section. The intermediate section has a connection feature at an end of the intermediate section to which the blade tip portion is attachable. The replacement tip section includes a transition region configured to be attached to a forward end of the connection feature. The transition region is configured to form a leading edge of the rotor blade and extends from the blade tip portion to form an opening into which the intermediate section is attached. The transition region includes a first end having a first airfoil that conforms to the intermediate section airfoil at the connection feature, and a second end having a second airfoil that conforms to the blade tip portion.
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