公开(公告)号：US20140026808A1

公开(公告)日：2014-01-30

申请号：US13989597

申请日：2011-11-09

Applicant: David Benjamin Hodgkinson ,  Stuart Lacy ,  Christopher Webb ,  Garry Anson

Inventor： David Benjamin Hodgkinson ,  Stuart Lacy ,  Christopher Webb ,  Garry Anson

IPC: B64D45/00

CPC classification number: B64D45/0005 ,  B64C25/00 ,  B64D2045/008

Abstract: A mechanical position indicator for providing a visual indication that a first part of an aircraft landing gear has assumed a predetermined position relative to a second part, the position indicator being arranged to be coupled to a first one of the first and second parts and in a first state arranged to hold an indicator element in a deployed position, the position indicator being arranged such that upon the first part assuming the predetermined position relative to the second part, a second one of the first and second parts changes the position indicator from the first state to a second state in which the indicator element is displaced from the deployed position, the position indicator being arranged to inhibit the indicator element thereafter returning to the deployed position.

Abstract translation: 一种用于提供飞行器起落架的第一部分相对于第二部分已经具有预定位置的视觉指示的机械位置指示器，所述位置指示器布置成联接到所述第一和第二部分中的第一部分，并且以 第一状态被布置成将指示器元件保持在展开位置，位置指示器布置成使得在第一部分相对于第二部分呈现预定位置时，第一部分和第二部分中的第二部分将位置指示器从第一部分 状态到第二状态，其中指示元件从展开位置移位，位置指示器布置成阻止指示元件返回到展开位置。

公开(公告)号：US09174727B2

公开(公告)日：2015-11-03

申请号：US13978790

申请日：2011-12-21

Applicant: Stuart Lacy ,  Yann Simonneaux

Inventor： Stuart Lacy ,  Yann Simonneaux

IPC: B64C25/36 ,  B64C25/50 ,  B64C25/34

CPC classification number: B64C25/50 ,  B64C25/34 ,  B64C25/36 ,  B64C2025/345

Abstract: A landing gear assembly for an aircraft, the landing gear assembly including: an elongate bogie beam; a first axle bearing having an outer part rotatably coupled to an inner part, the outer part being coupled to the bogie beam, the inner part including a mounting aperture; and an elongate axle provided through the mounting aperture of the inner part and coupled thereto, wherein the axle is coupled to the inner part of the first axle bearing in a configuration such that the longitudinal axis of the axle is spaced from the axis of rotation of the inner part, such that rotation of the inner part causes a change in the orientation of the axle relative to the bogie beam.

Abstract translation: 一种用于飞机的起落架组件，起落架组件包括：细长的转向架梁; 第一轴承，其具有可旋转地联接到内部的外部部分，所述外部部分联接到转向架梁，所述内部部分包括安装孔; 以及细长轴，其通过内部部分的安装孔提供并且联接到其上，其中轴以一种构造联接到第一轴承的内部，使得轴的纵向轴线与轴的旋转轴线间隔开 内部部分，使得内部部分的旋转引起轴相对于转向架梁的取向的改变。

公开(公告)号：US09272792B2

公开(公告)日：2016-03-01

申请号：US13989597

申请日：2011-11-09

Applicant: David Benjamin Hodgkinson ,  Stuart Lacy ,  Christopher Webb ,  Garry Anson

Inventor： David Benjamin Hodgkinson ,  Stuart Lacy ,  Christopher Webb ,  Garry Anson

IPC: B64D45/00 ,  B64C25/00 ,  G01L1/06

CPC classification number: B64D45/0005 ,  B64C25/00 ,  B64D2045/008

Abstract: A mechanical position indicator for providing a visual indication that a first part of an aircraft landing gear has assumed a predetermined position relative to a second part, the position indicator being arranged to be coupled to a first one of the first and second parts and in a first state arranged to hold an indicator element in a deployed position, the position indicator being arranged such that upon the first part assuming the predetermined position relative to the second part, a second one of the first and second parts changes the position indicator from the first state to a second state in which the indicator element is displaced from the deployed position, the position indicator being arranged to inhibit the indicator element thereafter returning to the deployed position.

Abstract translation: 一种用于提供飞行器起落架的第一部分相对于第二部分已经具有预定位置的视觉指示的机械位置指示器，所述位置指示器布置成联接到所述第一和第二部分中的第一部分，并且以 第一状态被布置成将指示器元件保持在展开位置，位置指示器布置成使得在第一部分相对于第二部分呈现预定位置时，第一部分和第二部分中的第二部分将位置指示器从第一部分 状态到第二状态，其中指示元件从展开位置移位，位置指示器布置成阻止指示元件返回到展开位置。

公开(公告)号：US20140048645A1

公开(公告)日：2014-02-20

申请号：US13978790

申请日：2011-12-21

Applicant: Stuart Lacy ,  Yann Simonneaux

Inventor： Stuart Lacy ,  Yann Simonneaux

IPC: B64C25/50

CPC classification number: B64C25/50 ,  B64C25/34 ,  B64C25/36 ,  B64C2025/345

Abstract: A landing gear assembly for an aircraft, the landing gear assembly including: an elongate bogie beam; a first axle bearing having an outer part rotatably coupled to an inner part, the outer part being coupled to the bogie beam, the inner part including a mounting aperture; and an elongate axle provided through the mounting aperture of the inner part and coupled thereto, wherein the axle is coupled to the inner part of the first axle bearing in a configuration such that the longitudinal axis of the axle is spaced from the axis of rotation of the inner part, such that rotation of the inner part causes a change in the orientation of the axle relative to the bogie beam.

Abstract translation: 一种用于飞机的起落架组件，起落架组件包括：细长的转向架梁; 第一轴承，其具有可旋转地联接到内部的外部部分，所述外部部分联接到转向架梁，所述内部部分包括安装孔; 以及细长轴，其通过内部部分的安装孔提供并且联接到其上，其中轴以一种构造联接到第一轴承的内部，使得轴的纵向轴线与轴的旋转轴线间隔开 内部部分，使得内部部分的旋转引起轴相对于转向架梁的取向的改变。