公开(公告)号：US20160252603A1

公开(公告)日：2016-09-01

申请号：US14502015

申请日：2014-09-30

Applicant: The Boeing Company

Inventor： Bryan Lee Kelchner ,  Kenneth Jerkatis ,  Richard Brooks Holmes ,  Nikolaus Mcnerney ,  Jed Donaldson

IPC: G01S3/786 ,  G02B23/08 ,  G02B17/06 ,  G01J9/00 ,  H04N7/18 ,  B64C30/00 ,  G01C19/04 ,  G02B7/182 ,  G02B26/08

CPC classification number: G01S3/786 ,  B64C30/00 ,  G01C19/04 ,  G01J9/00 ,  G01M9/06 ,  G02B7/1821 ,  G02B17/061 ,  G02B17/0657 ,  G02B17/0663 ,  G02B23/08 ,  G02B26/0816 ,  G02B26/105 ,  G02B27/14 ,  H04N7/183

Abstract: The aircraft includes a fuselage and at least one aerodynamic interface surface. It further includes a gimbaled mirror system which includes a mirror supported by a gimbal to receive a light beam from a light emitting source and reflect the light beam to a first periscope fold mirror. A wave front measuring system includes at least five reflective which reflects the light beam to a fast steering mirror. The fast steering mirror reflects the light beam directly to a beam splitter wherein the light beam is split into a transmitted portion and a reflected portion of the light beam.

Abstract translation: 飞机包括机身和至少一个空气动力学界面。 它还包括万向反射镜系统，其包括由万向节支撑的反射镜，以接收来自发光源的光束并将光束反射到第一潜望镜折射镜。 波前测量系统包括将光束反射到快速转向镜的至少五个反射镜。 快速转向镜将光束直接反射到分束器，其中光束被分裂成光束的透射部分和反射部分。

公开(公告)号：US09606214B2

公开(公告)日：2017-03-28

申请号：US14502015

申请日：2014-09-30

Applicant: THE BOEING COMPANY

Inventor： Bryan Lee Kelchner ,  Kenneth Jerkatis ,  Richard Brooks Holmes ,  Nikolaus Mcnerney ,  Jed Donaldson

IPC: G06F7/70 ,  G06F19/00 ,  G06G7/00 ,  G06G7/76 ,  G01S3/786 ,  G01M9/06 ,  G01J9/00 ,  G02B17/06 ,  B64C30/00 ,  G01C19/04 ,  G02B7/182 ,  G02B23/08 ,  G02B26/08 ,  H04N7/18 ,  G02B26/10 ,  G02B27/14

CPC classification number: G01S3/786 ,  B64C30/00 ,  G01C19/04 ,  G01J9/00 ,  G01M9/06 ,  G02B7/1821 ,  G02B17/061 ,  G02B17/0657 ,  G02B17/0663 ,  G02B23/08 ,  G02B26/0816 ,  G02B26/105 ,  G02B27/14 ,  H04N7/183

Abstract: The aircraft includes a fuselage and at least one aerodynamic interface surface. It further includes a gimbaled mirror system which includes a mirror supported by a gimbal to receive a light beam from a light emitting source and reflect the light beam to a first periscope fold mirror. A wave front measuring system includes at least five reflective which reflects the light beam to a fast steering mirror. The fast steering mirror reflects the light beam directly to a beam splitter wherein the light beam is split into a transmitted portion and a reflected portion of the light beam.