公开(公告)号：US20170203856A1

公开(公告)日：2017-07-20

申请号：US15476785

申请日：2017-03-31

Applicant: B/E Aerospace, Inc.

Inventor： Matthew Dunn ,  Eric Johannessen ,  Gannon T. Gambeski ,  John Terence Barker ,  Ronnie R. Moss ,  Jesse Richard Peck ,  Robert Linton ,  Jonathan Todzia ,  Donald LaSala ,  Luis Sam

IPC: B64D47/02 ,  G10K11/178 ,  H04R3/04 ,  H04R1/02 ,  H04R3/12

CPC classification number: H04R3/04 ,  B64D11/0015 ,  B64D11/00155 ,  B64D2011/0053 ,  B64D2045/007 ,  B64D2231/025 ,  F21V33/0056 ,  G10K11/178 ,  G10K2210/1281 ,  G10K2210/3044 ,  H04R1/028 ,  H04R1/28 ,  H04R3/12 ,  H04R2201/028 ,  H04R2499/13 ,  Y02T50/46

Abstract: In an illustrative embodiment, an integrated speaker-light unit includes a base unit adapted to be mounted to a fixture of an aircraft, a speaker unit disposed proximate the base unit, a horn element having a proximal end and a distal end, the proximal end positioned proximate the speaker unit and defining a first aperture, and the distal end defining a second aperture, where a greatest measurement of the second aperture is larger than a greatest measurement of the first aperture, an LED unit disposed at least partially in the horn element, and a housing element at least partially surrounding the horn element. The greatest measurement of the second aperture may be less than 4 inches. The base unit may be mounted to a passenger service unit such that the integrated speaker-light unit is presented as a passenger reading light.

公开(公告)号：US12043418B2

公开(公告)日：2024-07-23

申请号：US17392994

申请日：2021-08-03

Applicant: B/E AEROSPACE, INC.

Inventor： Bryce Baker ,  Cory Kaufman ,  John Terence Barker ,  Samuel Anderson

IPC: B64G1/48 ,  G05D16/20

CPC classification number: B64G1/48 ,  G05D16/204

Abstract: An environmental control system for a space vehicle includes an oxygen supply, a nitrogen supply, a first pressure control panel having a first oxygen control board configured to receive an oxygen gas from the oxygen supply and a first nitrogen control board configured to receive a nitrogen gas from the nitrogen supply, and a supervisory controller configured to control the first pressure control panel and thereby to adjust a partial pressure of oxygen and an ambient pressure of an oxygen/nitrogen gas mixture within a first module.

公开(公告)号：US10219059B2

公开(公告)日：2019-02-26

申请号：US14869651

申请日：2015-09-29

Applicant: B/E AEROSPACE, INC.

Inventor： Matthew Dunn ,  Eric Johannessen ,  Gannon T. Gambeski ,  John Terence Barker ,  Ronnie R. Moss ,  Jesse Richard Peck ,  Robert Linton ,  Jonathan Todzia ,  Donald LaSala ,  Luis Sam

IPC: B64D45/00 ,  F21V33/00 ,  H04R1/02 ,  B64D11/00 ,  H04R1/28

Abstract: Disclosed herein is an overhead passenger service unit (PSU) for a vehicle, comprising: a mounting mechanism for mounting the PSU above at least one vehicle seat; a dynamic seat row marker that provides an indication of a seat position and a status portion indicating a status of a passenger or trip aspect that is readily viewable from a vehicle aisle and is changeable during a trip; and a programmable active display that is readily viewable from a passenger seat and provides trip changeable information about the trip to the passenger.

公开(公告)号：US20230042564A1

公开(公告)日：2023-02-09

申请号：US17392994

申请日：2021-08-03

Applicant: B/E AEROSPACE, INC.

Inventor： Bryce Baker ,  Cory Kaufman ,  John Terence Barker ,  Samuel Anderson

IPC: B64G1/48 ,  G05D16/20

Abstract: An environmental control system for a space vehicle includes an oxygen supply, a nitrogen supply, a first pressure control panel having a first oxygen control board configured to receive an oxygen gas from the oxygen supply and a first nitrogen control board configured to receive a nitrogen gas from the nitrogen supply, and a supervisory controller configured to control the first pressure control panel and thereby to adjust a partial pressure of oxygen and an ambient pressure of an oxygen/nitrogen gas mixture within a first module.

公开(公告)号：US20220297729A1

公开(公告)日：2022-09-22

申请号：US17203185

申请日：2021-03-16

Applicant: B/E Aerospace, Inc.

Inventor： John Terence Barker

IPC: B61D27/00 ,  B61B13/10 ,  A62B7/02

Abstract: A low pressure enclosure (LPE) vehicle can include a hull defining a cabin therein. The hull can be configured to travel within a LPE and the cabin can be configured to be pressurized. The LPE vehicle can include a supplemental oxygen system configured to be activated and/or made accessible to one or more occupants within the cabin in a depressurized state such that a cabin pressure is less than a threshold cabin pressure.

公开(公告)号：US20220219022A1

公开(公告)日：2022-07-14

申请号：US17147162

申请日：2021-01-12

Applicant: B/E Aerospace, Inc.

Inventor： John Terence Barker ,  Michael Brumley

IPC: A62B7/02 ,  B64G6/00 ,  A62B7/14

Abstract: A pulsed oxygen delivery system is disclosed for a closed breathing environment, which includes a source of gaseous oxygen, a phase dilution type oronasal dispensing mask worn by a user in a closed breathing environment defined by a pressure suit, and a pulse control module for delivering a timed and metered bolus of oxygen from the source of gaseous oxygen to the oronasal dispensing mask upon inhalation by the user.

公开(公告)号：US12186600B2

公开(公告)日：2025-01-07

申请号：US17203185

申请日：2021-03-16

Applicant: B/E Aerospace, Inc.

Inventor： John Terence Barker

IPC: A62B7/02 ,  B61B13/10 ,  B61D27/00

Abstract: A low pressure enclosure (LPE) vehicle can include a hull defining a cabin therein. The hull can be configured to travel within a LPE and the cabin can be configured to be pressurized. The LPE vehicle can include a supplemental oxygen system configured to be activated and/or made accessible to one or more occupants within the cabin in a depressurized state such that a cabin pressure is less than a threshold cabin pressure.

公开(公告)号：US12053654B2

公开(公告)日：2024-08-06

申请号：US17147162

申请日：2021-01-12

Applicant: B/E Aerospace, Inc.

Inventor： John Terence Barker ,  Michael Brumley

IPC: A62B7/02 ,  A62B7/14 ,  B64G6/00

CPC classification number: A62B7/02 ,  A62B7/14 ,  B64G6/00

Abstract: A pulsed oxygen delivery system is disclosed for a closed breathing environment, which includes a source of gaseous oxygen, a phase dilution type oronasal dispensing mask worn by a user in a closed breathing environment defined by a pressure suit, and a pulse control module for delivering a timed and metered bolus of oxygen from the source of gaseous oxygen to the oronasal dispensing mask upon inhalation by the user.

公开(公告)号：US11451462B2

公开(公告)日：2022-09-20

申请号：US17119898

申请日：2020-12-11

Applicant: B/E Aerospace, Inc.

Inventor： John Terence Barker

IPC: B64D13/02 ,  B64D13/04 ,  G05D16/20 ,  G06F7/00 ,  H04L43/50 ,  B64F5/60 ,  H04W4/80 ,  H04L67/12

Abstract: A control system for an aircraft system can include a controller configured to connect to one or more subsystems of the aircraft system, the controller having a built-in-test (BIT) module configured to test the one or more subsystems of the aircraft system and output test data. The control system can include a wireless communication module operatively connected to the controller and configured to receive the output data and to output a wireless signal as a function of the test data.

公开(公告)号：US20220191121A1

公开(公告)日：2022-06-16

申请号：US17119898

申请日：2020-12-11

Applicant: B/E Aerospace, Inc.

Inventor： John Terence Barker

IPC: H04L12/26 ,  H04W4/80 ,  B64F5/60

Abstract: A control system for an aircraft system can include a controller configured to connect to one or more subsystems of the aircraft system, the controller having a built-in-test (BIT) module configured to test the one or more subsystems of the aircraft system and output test data. The control system can include a wireless communication module operatively connected to the controller and configured to receive the output data and to output a wireless signal as a function of the test data.