公开(公告)号：US11271355B2

公开(公告)日：2022-03-08

申请号：US16874367

申请日：2020-05-14

Applicant: The Boeing Company

Inventor： Mark Joseph Clemen, Jr. ,  John R. Hull

IPC: H01S3/0959 ,  H01S3/032 ,  H01S3/07 ,  H01S3/0975 ,  H01S3/102 ,  H01S3/10

Abstract: A system for generating an energy beam based laser includes an apparatus for receiving an energy beam and for generating an energy beam based laser. The apparatus is configurable or controllable for tuning an output wavelength of the laser generated by the apparatus using the energy beam. The apparatus includes a first component for producing a first magnetic field oriented in a first direction and a second component for producing a second magnetic field oriented in a second direction substantially opposite to the first direction. A channel through the apparatus is defined by the first component and the second component through which the energy beam passes to generate the laser at an output of the apparatus. The apparatus is configurable or controllable for modifying at least one of the first magnetic field and the second magnetic field for tuning the output wavelength of the laser.

公开(公告)号：US10455199B1

公开(公告)日：2019-10-22

申请号：US14823677

申请日：2015-08-11

Applicant: The Boeing Company

Inventor： Mark Joseph Clemen, Jr. ,  James A. Grossnickle

IPC: H04N7/18 ,  H04N5/247 ,  G06T7/00

Abstract: A method and apparatus for countering an attack on a platform. Images are received from cameras associated with the platform, and the images are identified from a group of the cameras that have a desired level of information when a group of light sources is directed at a camera system. A fused image is generated from a combination of the images from the group of the cameras and displayed on a display system for the platform. The fused image enables performing an operation using the platform.

公开(公告)号：US09758235B2

公开(公告)日：2017-09-12

申请号：US14881337

申请日：2015-10-13

Applicant: The Boeing Company

Inventor： Mark Joseph Clemen, Jr. ,  Jerry Lee Wert

IPC: B64C1/10 ,  B64C1/38 ,  B64C30/00 ,  F41H3/00 ,  H01F7/06 ,  H01F7/02

CPC classification number: B64C1/38 ,  B64C30/00 ,  F41H3/00 ,  H01F7/0236 ,  H01F7/0273 ,  H01F7/064 ,  H02N15/00

Abstract: A thermal insulation system for an aircraft that includes leading surfaces is provided. The thermal insulation system includes a carrier and a container. The carrier has an interior surface that includes a first plurality of magnets that generate a first magnetic field, and an exterior surface that is thermally coupled to the leading surfaces of the aircraft. The container is surrounded by the interior surface of the carrier, has an exterior surface including a second plurality of magnets that generate a second magnetic field oriented opposite the first magnetic field, and has an interior that includes electronics. The first magnetic field and the second magnetic field generate a gap between the carrier and the container to reduce a heat transfer from the leading surfaces to the electronics during operation of the aircraft.