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

IPC: B64D15/12 ,  B64C3/18 ,  B64F5/10

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.

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

IPC: B64D15/12 ,  H05B3/14

CPC classification number: B64D15/12 ,  H05B3/145 ,  B82Y30/00

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.

公开(公告)号：US20220295601A1

公开(公告)日：2022-09-15

申请号：US17752806

申请日：2022-05-24

Applicant: Goodrich Corporation

Inventor： George F. Owens ,  Kevin Edward Roach ,  James A. Mullen ,  Michael John Giamati ,  Jon Shearer ,  James Van Twisk ,  David L. Brittingham ,  Tommy M. Wilson, JR. ,  Jin Hu ,  William A. Veronesi ,  Mark R. Gurvich ,  Joseph Winesdoerffer ,  Jason Gesner

IPC: H05B3/26 ,  B64D13/08 ,  F24D13/02 ,  B32B3/12 ,  B32B7/12 ,  B32B15/20 ,  B64C1/18 ,  H01C17/06

Abstract: An aircraft heated floor panel includes a first face sheet, a second face sheet opposite the first face sheet, and core with an electrically conductive core portion. The electrically conductive core portion supports the first face sheet and the second face sheet, and is electrically insulated from the external environment to receive electrical power, resistively generate heat, and communicate heat to the first face sheet.

公开(公告)号：US20210291957A1

公开(公告)日：2021-09-23

申请号：US16824984

申请日：2020-03-20

Applicant: GOODRICH CORPORATION

Inventor： Brandon Hein ,  James A. Mullen ,  George F. Owens ,  Nathaniel Ching ,  Jin Hu

IPC: B64C1/18

Abstract: A heated floor panel may comprise a base assembly and a heating element located on a first surface of the base assembly. A panel skin may be located over the heating element and the first surface of the base assembly. The panel skin may extend from the first surface of the base assembly to a second surface of the base assembly opposite the first surface of the base assembly.

公开(公告)号：US10899427B2

公开(公告)日：2021-01-26

申请号：US16026899

申请日：2018-07-03

Applicant: Goodrich Corporation

Inventor： Casey Slane ,  Nathaniel Ching ,  Wenping Zhao ,  Daniel Waina ,  Jin Hu ,  Brandon Hein ,  George F. Owens ,  James A. Mullen

IPC: H05B3/20 ,  H05B3/28 ,  B64C1/18 ,  B32B3/12 ,  B32B5/02 ,  B32B5/18 ,  B32B15/14 ,  B32B15/18 ,  B32B15/20 ,  B64C1/00

Abstract: A heated floor panel assembly with an impact layer is made to absorb blunt force and protect a heating element inside the assembly. The assembly further includes a plurality of structural layer made of a reinforced polymer matrix, one or more core layer with a honeycomb or foam structure for absorbing shear stress, and a heating layer containing the heating element. The impact layer is a composite layer with a resin impregnated fiber matrix.

公开(公告)号：US20210009273A1

公开(公告)日：2021-01-14

申请号：US16509078

申请日：2019-07-11

Applicant: GOODRICH CORPORATION

Inventor： Galdemir Cezar Botura ,  James A. Mullen

IPC: B64D15/12 ,  H05B3/34 ,  H05B3/14 ,  H05B3/48

Abstract: An ice detector apparatus for an aircraft includes a heater strip and a temperature sensor. The heater strip is configured to be mounted to an external surface of an aircraft and the temperature sensor is coupled to the heater strip. The temperature sensor is configured to detect a temperature profile of the heater strip, wherein the temperature profile is indicative of an extent of icing. The temperature profile may be indicative of whether the aircraft is operating in an appendix C icing-envelope or an appendix O icing-envelope. The temperature sensor may include a plurality of temperature sensors coupled along a length of the heater strip, such that the temperature profile comprises a spatial temperature map of the heater strip.

公开(公告)号：US20200015325A1

公开(公告)日：2020-01-09

申请号：US16427896

申请日：2019-05-31

Applicant: Goodrich Corporation

Inventor： Wenping Zhao ,  Jin Hu ,  Nathaniel Ching ,  George F. Owens ,  Casey Slane ,  Brandon Hein ,  Daniel Waina ,  James A. Mullen ,  Melissa Leigh Patterson ,  Galdemir Cezar Botura

IPC: H05B3/28 ,  H05B3/03 ,  H05B3/06 ,  B64C1/18

Abstract: A heated floor panel assembly contains a positive temperature coefficient heater secured in the assembly through a number of welded joints through a thermoplastic dielectric layer. The positive temperature coefficient heater is on a thermoplastic substrate, which is bonded to the thermoplastic dielectric layer. The assembly further includes an impact layer, a core layer, and structural layers.

公开(公告)号：US11084593B2

公开(公告)日：2021-08-10

申请号：US16157733

申请日：2018-10-11

Applicant: Goodrich Corporation

Inventor： Adam George ,  Reid Philip Beery ,  James A. Mullen

IPC: B64D15/12 ,  H05B3/00 ,  H05B3/03 ,  H05B3/12 ,  H05B3/34

Abstract: An additively manufactured heating element is printed on a flexible substrate and attached to an aircraft component having a complex geometric surface. The heating element is made of a plurality of layers of a conductive ink, which is electrically connected to a controller through one or more leads.

公开(公告)号：US20200088593A1

公开(公告)日：2020-03-19

申请号：US16132986

申请日：2018-09-17

Applicant: Goodrich Corporation

Inventor： James A. Mullen

IPC: G01L1/22 ,  C09D11/52 ,  H01B1/22 ,  H05K1/09

Abstract: An additively manufactured strain gauge resides on the surface of a component to monitor component fatigue. The strain gauge is additively manufactured, and applied to the curvature of the component surface through either a flexible substrate or through direct printing.

公开(公告)号：US10470250B2

公开(公告)日：2019-11-05

申请号：US15373372

申请日：2016-12-08

Applicant: Goodrich Corporation

Inventor： James A. Mullen ,  Jin Hu ,  Galdemir Cezar Botura ,  Zaffir A. Chaudhry ,  Wenping Zhao

IPC: H05B3/14 ,  H05B3/10 ,  H05B3/12 ,  H05B3/20 ,  B64D15/12 ,  H05B3/26

Abstract: A carbon allotrope heating element includes an electrical resistivity between 0.005 ohms per square (Ω/sq) and 3.0 Ω/sq. A heating system includes a component and a carbon allotrope heating element having an electrical resistivity between 0.005 Ω/sq and 3.0 Ω/sq. A method includes modifying a carbon allotrope heating element to have an electrical resistivity between 0.005 Ω/sq and 3.0 Ω/sq and applying the carbon allotrope heating element to a component of an aircraft.