公开(公告)号：US11006500B1

公开(公告)日：2021-05-11

申请号：US16746020

申请日：2020-01-17

Applicant: B/E AEROSPACE, INC.

Inventor： John Edquist ,  Jeremy Fredrich ,  Brendan M. Upton ,  Van Phifer

IPC: H05B45/58 ,  F21S43/31 ,  H05B45/12 ,  F21S43/40 ,  F21V23/00 ,  B64D47/06 ,  F21S43/14 ,  F21W107/30 ,  F21Y105/18 ,  F21Y115/10 ,  F21W103/10

Abstract: An end of life detection system for an anti-collision light may comprise a reflector and a plurality of LEDs located around an exterior of the reflector. A trend LED and reference LED may be located in an interior of the reflector. The trend LED may be powered on with plurality of LEDs. The reference LED may be powered on during an initial power-on self-check and turned off after completion of the initial power-on self-check.

公开(公告)号：US20240226354A1

公开(公告)日：2024-07-11

申请号：US18616502

申请日：2024-03-26

Applicant: B/E AEROSPACE, INC.

Inventor： John Edquist ,  Eric Johannessen

IPC: A61L2/10 ,  A61L2/24

CPC classification number: A61L2/10 ,  A61L2/24 ,  A61L2202/11 ,  A61L2202/14 ,  A61L2202/25

Abstract: A sanitization system for an aircraft may comprise: a power source; and a plurality of sanitizers in electrical communication with the power source, each sanitizer in the plurality of sanitizers configured to emit ultraviolet radiation having an average wavelength between 200 and 230 nm, the power source configured to provide power to each sanitizer in the plurality of sanitizers in succession during an occupied flight of the aircraft.

公开(公告)号：US11480329B2

公开(公告)日：2022-10-25

申请号：US17027496

申请日：2020-09-21

Applicant: B/E AEROSPACE, INC.

Inventor： John Edquist ,  Eric Johannessen

IPC: F21V33/00 ,  F21V3/06 ,  H05B45/10 ,  A61L2/10 ,  A61L2/24 ,  B64D47/02 ,  F21V19/00 ,  F21V23/00 ,  F21Y115/10 ,  F21W107/30 ,  F21W106/00

Abstract: A lighting unit may include a first light-emitting diode (“LED”), a second LED, and a third LED. The first LED may be configured to emit first electromagnetic radiation having a first wavelength of between about 600 nanometers (“nm”) and about 740 nm, the second LED may be configured to emit second electromagnetic radiation having a second wavelength of between about 500 nm and about 565 nm, and the third LED may be configured to emit third electromagnetic radiation having a third wavelength between about 315 nm and about 430 nm. Thus, the third electromagnetic radiation may be disinfecting UV-A radiation that is incorporated into a lighting unit that produces visible light.

公开(公告)号：US20220306296A1

公开(公告)日：2022-09-29

申请号：US17209715

申请日：2021-03-23

Applicant: B/E AEROSPACE, INC.

Inventor： John Edquist ,  Sanjay Bajekal ,  Frank Hashberger ,  Fangzhong Guo

IPC: B64D11/02 ,  A61L2/10 ,  A61L2/24

Abstract: A system for touchless control of a lavatory of an aircraft includes at least one sensor located in the lavatory and configured to detect detected data corresponding to the lavatory. The system further includes at least one actuator or light source located in the lavatory and configured to perform an action. The system further includes a central controller coupled to the at least one sensor and the at least one actuator or light source and configured to make an inference based on the detected data and to control the at least one actuator or light source based on the inference.

公开(公告)号：US20220062467A1

公开(公告)日：2022-03-03

申请号：US17184913

申请日：2021-02-25

Applicant: B/E AEROSPACE, INC.

Inventor： Daniel Tilmont ,  Eric Johannessen ,  John Edquist

IPC: A61L2/10 ,  A61L2/26 ,  A61L2/08 ,  A61L2/22 ,  A61L9/14

Abstract: A sanitization system for an aircraft cabin may comprise: a cabin of an aircraft; a light system including a lighting unit configured to emit an electromagnetic radiation output between 300 and 430 nanometers (“nm”); an external reactive oxygen species (ROS) generator in fluid communication with the cabin, wherein the sanitization system is configured to disinfect a target area of the cabin by targeting the target area with the electromagnetic radiation output and the ROS.

公开(公告)号：US20210291727A1

公开(公告)日：2021-09-23

申请号：US16826119

申请日：2020-03-20

Applicant: B/E AEROSPACE, INC.

Inventor： John Edquist ,  Jeremy Fredrich

IPC: B60Q3/47 ,  B64D47/02 ,  B64D11/00 ,  B60Q3/46 ,  H05B47/11

Abstract: An aircraft emergency lighting system is disclosed. This emergency lighting system may include interior emergency lighting, interior ambient light sensors, exterior emergency lighting, and exterior ambient light sensors. The interior emergency lighting, the exterior emergency lighting, or both, may be controlled based upon an input of the interior ambient light condition (e.g., using an output from at least one of the interior ambient light sensors) and based upon an input from at least one of the exterior ambient light sensors.