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公开(公告)号：US11873098B2
公开(公告)日：2024-01-16
申请号：US16573123
申请日：2019-09-17
Applicant: Goodrich Corporation
Inventor： Casey Slane , Jin Hu , Nathaniel Ching , Galdemir Cezar Botura , James A. Mullen , Mark James Didyk
CPC classification number: B64D15/12 , H05B3/145 , B82Y30/00 , F02C7/047 , H05B2203/017 , H05B2214/02 , H05B2214/04
Abstract: An ice protection system for an aircraft component includes a plurality of heaters. The aircraft component has at least two section and a junction area. At least one of the heaters is an H-shape carbon allotrope heater designed to apply heat to the junction area and prevent ice accumulation in the junction area.
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公开(公告)号：US11548648B2
公开(公告)日：2023-01-10
申请号：US16742637
申请日：2020-01-14
Applicant: GOODRICH CORPORATION
Inventor： Adam George , Mark James Didyk
Abstract: A heating element and conductive element system may include a heater conductive element and a heating element. The heater conductive element and the heating element may be integral components. The heater conductive element and the heating element may be discrete components. The heater conductive element may be configured for enhanced mechanical fatigue compared to typical conductive element.
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公开(公告)号：US20220017227A1
公开(公告)日：2022-01-20
申请号：US16932357
申请日：2020-07-17
Applicant: Goodrich Corporation
Inventor： Adam George , Mark James Didyk , Reid Philip Beery
Abstract: A system for controlling a multi-zone resistive heater. The system includes a first zone of the multi-zone resistive heater formed from a material having a negative temperature coefficient of resistivity (TCR) and configured to receive a first power to generate thermal energy. The system further includes a second zone of the multi-zone resistive heater formed from the material having the negative TCR, separated from the first zone by a gap, and configured to receive a second power to generate the thermal energy.
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公开(公告)号：US12145733B2
公开(公告)日：2024-11-19
申请号：US18535566
申请日：2023-12-11
Applicant: Goodrich Corporation
Inventor： Casey Slane , Jin Hu , Nathaniel Ching , Galdemir Cezar Botura , James A. Mullen , Mark James Didyk
Abstract: An ice protection system for an aircraft component includes a plurality of heaters. The aircraft component has at least two section and a junction area. At least one of the heaters is an H-shape carbon allotrope heater designed to apply heat to the junction area and prevent ice accumulation in the junction area.
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Patent Agency Ranking
公开(公告)号：US11814182B2
公开(公告)日：2023-11-14
申请号：US16932357
申请日：2020-07-17
Applicant: GOODRICH CORPORATION
Inventor： Adam George , Mark James Didyk , Reid Philip Beery
CPC classification number: B64D15/22 , B64D15/12 , G05D23/1902 , G05D23/24 , H05B1/0236
Abstract: A system for controlling a multi-zone resistive heater. The system includes a first zone of the multi-zone resistive heater formed from a material having a negative temperature coefficient of resistivity (TCR) and configured to receive a first power to generate thermal energy. The system further includes a second zone of the multi-zone resistive heater formed from the material having the negative TCR, separated from the first zone by a gap, and configured to receive a second power to generate the thermal energy.
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公开(公告)号：US20200331616A1
公开(公告)日：2020-10-22
申请号：US16389313
申请日：2019-04-19
Applicant: GOODRICH CORPORATION
Inventor： Mark James Didyk , James A. Mullen , Jin Hu , Galdemir Cezar Botura , Casey Slane
Abstract: An aircraft may include a fuselage and a wing extending away from the fuselage to a wing tip. The wing may have a leading edge portion, a suction side portion, and a pressure side portion. A thermoelectric element may be coupled to an inner surface of the wing. A chemical adhesive may be disposed on a thermoelectric inner surface. A structural rib may be adhesively bonded to the thermoelectric element by curing the chemical adhesive. The structural rib may be mechanically fastened to a suction side of the wing and to a pressure side of the wing.
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公开(公告)号：US20240124146A1
公开(公告)日：2024-04-18
申请号：US18535566
申请日：2023-12-11
Applicant: Goodrich Corporation
Inventor： Casey Slane , Jin Hu , Nathaniel Ching , Galdemir Cezar Botura , James A. Mullen , Mark James Didyk
Abstract: An ice protection system for an aircraft component includes a plurality of heaters. The aircraft component has at least two section and a junction area. At least one of the heaters is an H-shape carbon allotrope heater designed to apply heat to the junction area and prevent ice accumulation in the junction area.
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公开(公告)号：US20230112358A1
公开(公告)日：2023-04-13
申请号：US18080913
申请日：2022-12-14
Applicant: GOODRICH CORPORATION
Inventor： Adam George , Mark James Didyk
Abstract: A heating element and conductive element system may include a heater conductive element and a heating element. The heater conductive element and the heating element may be integral components. The heater conductive element and the heating element may be discrete components. The heater conductive element may be configured for enhanced mechanical fatigue compared to typical conductive element.
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公开(公告)号：US20210214090A1
公开(公告)日：2021-07-15
申请号：US16742637
申请日：2020-01-14
Applicant: GOODRICH CORPORATION
Inventor： Adam George , Mark James Didyk
Abstract: A heating element and conductive element system may include a heater conductive element and a heating element. The heater conductive element and the heating element may be integral components. The heater conductive element and the heating element may be discrete components. The heater conductive element may be configured for enhanced mechanical fatigue compared to typical conductive element.
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