公开(公告)号：US12222128B2

公开(公告)日：2025-02-11

申请号：US18346447

申请日：2023-07-03

Applicant: THE BOEING COMPANY

Inventor： Bryce A. Vandyke ,  John Erik West ,  Douglas D. Maben ,  Andrew K. Fung ,  David R. C. Cannal

IPC: F24F13/02 ,  B64D13/06 ,  F24F13/24

Abstract: A duct includes a rigid air-permeable tube of composite material. The duct also includes a layer of insulation coupled to an exterior surface of the rigid air-permeable tube. The duct further includes a non-rigid insulation layer in contact with the layer of insulation. The non-rigid insulation layer forms an air-impermeable duct wall.

公开(公告)号：US20200056803A1

公开(公告)日：2020-02-20

申请号：US16105864

申请日：2018-08-20

Applicant: THE BOEING COMPANY

Inventor： Bryce A. Vandyke ,  John Erik West ,  Douglas D. Maben ,  Andrew K. Fung ,  David R.C. Cannal

IPC: F24F13/02

Abstract: A duct includes a rigid air-permeable tube of composite material. The duct also includes a layer of insulation coupled to an exterior surface of the rigid air-permeable tube. The duct further includes a non-rigid insulation layer in contact with the layer of insulation. The non-rigid insulation layer forms an air-impermeable duct wall.

公开(公告)号：US20230358433A1

公开(公告)日：2023-11-09

申请号：US18346447

申请日：2023-07-03

Applicant: The Boeing Company

Inventor： Bryce A. Vandyke ,  John Erik West ,  Douglas D. Maben ,  Andrew K. Fung ,  David R.C. Cannal

IPC: F24F13/02

CPC classification number: F24F13/0263 ,  F24F2013/242

Abstract: A duct includes a rigid air-permeable tube of composite material. The duct also includes a layer of insulation coupled to an exterior surface of the rigid air-permeable tube. The duct further includes a non-rigid insulation layer in contact with the layer of insulation. The non-rigid insulation layer forms an air-impermeable duct wall.

公开(公告)号：US10220931B2

公开(公告)日：2019-03-05

申请号：US14935788

申请日：2015-11-09

Applicant: THE BOEING COMPANY

Inventor： Thomas Seth Perkins ,  Cory Michael Hitchcock ,  John Erik West ,  Adam R. Weston ,  Gregory A. Tubbs

IPC: B64C1/06 ,  B64C1/40 ,  B64C1/00

Abstract: A return air bridge for use in an aircraft assembly includes an inboard portion configured to couple to a sidewall assembly at a bottom edge of the sidewall assembly and an outboard portion configured to couple to a structural member. The return air bridge also includes at least one support coupling the inboard portion to the outboard portion such that a return air flow path is defined between the inboard portion and the outboard portion. The outboard portion comprises a plate configured to direct an air flow along the return air flow path upwardly with respect to the bottom edge of the sidewall assembly.

公开(公告)号：US11739973B2

公开(公告)日：2023-08-29

申请号：US16105864

申请日：2018-08-20

Applicant: THE BOEING COMPANY

Inventor： Bryce A. Vandyke ,  John Erik West ,  Douglas D. Maben ,  Andrew K. Fung ,  David R. C. Cannal

IPC: F24F13/02 ,  F24F13/24 ,  B64D13/06

CPC classification number: F24F13/0263 ,  B64D2013/0603 ,  F24F13/0245 ,  F24F13/0281 ,  F24F2013/242

Abstract: A duct includes a rigid air-permeable tube of composite material. The duct also includes a layer of insulation coupled to an exterior surface of the rigid air-permeable tube. The duct further includes a non-rigid insulation layer in contact with the layer of insulation. The non-rigid insulation layer forms an air-impermeable duct wall.

公开(公告)号：US20170129581A1

公开(公告)日：2017-05-11

申请号：US14935788

申请日：2015-11-09

Applicant: THE BOEING COMPANY

Inventor： Thomas Seth Perkins ,  Cory Michael Hitchcock ,  John Erik West ,  Adam R. Weston ,  Gregory A. Tubbs

IPC: B64C1/06 ,  B64C1/18 ,  B64C1/40

CPC classification number: B64C1/066 ,  B64C1/40 ,  B64C2001/009 ,  Y02T50/46

Abstract: A return air bridge for use in an aircraft assembly includes an inboard portion configured to couple to a sidewall assembly at a bottom edge of the sidewall assembly and an outboard portion configured to couple to a structural member. The return air bridge also includes at least one support coupling the inboard portion to the outboard portion such that a return air flow path is defined between the inboard portion and the outboard portion. The outboard portion comprises a plate configured to direct an air flow along the return air flow path upwardly with respect to the bottom edge of the sidewall assembly.