公开(公告)号：US09551790B2

公开(公告)日：2017-01-24

申请号：US14268841

申请日：2014-05-02

申请人： The Boeing Company

发明人： Bobby Joe Marsh ,  Michael Anthony Lazar ,  Kinson D. Vanscotter ,  Barry Theophile Cooke ,  Leonard S. Bodziony ,  Richard M. Coleman ,  Michael Marcus Vander Wel ,  Andrew S. Olson ,  Douglas V. Dorsey ,  Orval Marion Nobles

IPC分类号： G01C3/08 ,  G01S17/88 ,  G01S17/08 ,  B64F5/00 ,  G01S17/66 ,  G01B11/00 ,  G01S7/48 ,  G01S17/87

CPC分类号： G01S17/88 ,  B64F5/10 ,  G01B11/002 ,  G01S7/4808 ,  G01S17/08 ,  G01S17/66 ,  G01S17/87

摘要： A method including placing first and second measurement devices proximate first and second aircraft doors, respectively, and determining a first position of the second measurement device relative to a second position of the first measurement device. The method includes placing first and second pluralities of reflective devices inside the aircraft proximate the first and second doors, respectively. The method includes measuring first and second distances from the first and second measurement devices to the first and second pluralities of reflective devices, respectively, and measuring second distances from the second measurement device to the second plurality of reflective devices. Based on a determined position of the second measurement device and further based on the first distances and second distances, third distances are determined between each of the first and second pluralities of reflective devices. The third distances provide a measurement baseline for points on a fuselage and wings.

摘要翻译： 一种方法，包括将第一和第二测量装置分别靠近第一和第二飞行器门，并且确定第二测量装置相对于第一测量装置的第二位置的第一位置。 该方法包括将第一和第二多个反射装置分别放置在靠近第一和第二门的飞机内部。 该方法包括分别测量从第一和第二测量装置到第一和第二多个反射装置的第一和第二距离，以及测量从第二测量装置到第二多个反射装置的第二距离。 基于第二测量装置的确定位置，并且还基于第一距离和第二距离，在第一和第二多个反射装置中的每一个之间确定第三距离。 第三个距离为机身和机翼上的点提供了测量基准。

公开(公告)号：US20170210489A1

公开(公告)日：2017-07-27

申请号：US15004808

申请日：2016-01-22

申请人： The Boeing Company

发明人： Aksel Bode ,  Peter Hoang Bui ,  Barry Theophile Cooke ,  Joseph Alan Leander ,  Ngan Minh Dinh ,  Paul Alan Koopman ,  Kevin Ronald Puzey

IPC分类号： B64F5/00 ,  G05B15/02

CPC分类号： G05B15/02 ,  B64C1/26 ,  B64F5/10 ,  B64F5/50 ,  G01B11/002 ,  G05B19/402 ,  G05B19/41805 ,  G05B19/4207 ,  G05B2219/40111 ,  G05B2219/45055 ,  G05B2219/49023 ,  Y02P90/04

摘要： Disclosed wing-to-body join methods include commanding a wing to a first command position and then iteratively repeating a first-phase movement and/or commanding a wing to a second command position and then iteratively repeating a second-phase movement. The first-phase movement includes determining a real position of the wing, calculating a first-phase difference between the real position and the first command position, and commanding the wing to reduce the magnitude of the first-phase difference. The second-phase movement includes determining a real position of the wing, determining a real position of the body, calculating a second-phase difference based on the second command position and the real positions of the wing and body, and commanding the wing to reduce the magnitude of the second-phase difference. Some embodiments include performing a port-side move for a port wing of the aircraft and performing a starboard-side move for a starboard wing of the aircraft.

公开(公告)号：US20150316649A1

公开(公告)日：2015-11-05

申请号：US14268841

申请日：2014-05-02

申请人： The Boeing Company

发明人： Bobby Joe Marsh ,  Michael Anthony Lazar ,  Kinson D. Vanscotter ,  Barry Theophile Cooke ,  Leonard S. Bodziony ,  Richard M. Coleman ,  Michael Marcus Vander Wel ,  Andrew S. Olson ,  Douglas V. Dorsey ,  Orval Marion Nobles

IPC分类号： G01S17/88 ,  G01S17/08

CPC分类号： G01S17/88 ,  B64F5/10 ,  G01B11/002 ,  G01S7/4808 ,  G01S17/08 ,  G01S17/66 ,  G01S17/87

摘要： A method including placing first and second measurement devices proximate first and second aircraft doors, respectively, and determining a first position of the second measurement device relative to a second position of the first measurement device. The method includes placing first and second pluralities of reflective devices inside the aircraft proximate the first and second doors, respectively. The method includes measuring first and second distances from the first and second measurement devices to the first and second pluralities of reflective devices, respectively, and measuring second distances from the second measurement device to the second plurality of reflective devices. Based on a determined position of the second measurement device and further based on the first distances and second distances, third distances are determined between each of the first and second pluralities of reflective devices. The third distances provide a measurement baseline for points on a fuselage and wings.

摘要翻译： 一种方法，包括将第一和第二测量装置分别靠近第一和第二飞行器门，并且确定第二测量装置相对于第一测量装置的第二位置的第一位置。 该方法包括将第一和第二多个反射装置分别放置在靠近第一和第二门的飞机内部。 该方法包括分别测量从第一和第二测量装置到第一和第二多个反射装置的第一和第二距离，以及测量从第二测量装置到第二多个反射装置的第二距离。 基于第二测量装置的确定位置，并且还基于第一距离和第二距离，在第一和第二多个反射装置中的每一个之间确定第三距离。 第三个距离为机身和机翼上的点提供了测量基准。