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公开(公告)号：US20160009357A1
公开(公告)日：2016-01-14
申请号：US14754620
申请日：2015-06-29
Applicant: B/E Aerospace, Inc.
Inventor： Justin C. Christenson , Graydon E. Loar
CPC classification number: B64C1/1423 , B64C1/1407 , B64D11/02 , E05D15/58 , E05F17/00 , E05Y2800/122 , E06B3/5009
Abstract: A telescoping aircraft door is disclosed having first and second panels that slide relative to one another to extend and retract as the door closes and opens, respectively. The first panel is hinged to the door frame in a traditional manner, and the second panel is fixed to the door frame by a linkage that limits the arc of the second panel. By selecting the location and length of the linkage, the relative movement of the two panels can be predictably controlled to reduce the depth of the door when closed and the length of the door when opened.
Abstract translation: 公开了一种伸缩式飞机门，其具有分别相对于彼此滑动的第一和第二面板，以在门关闭和打开时分别延伸和缩回。 第一面板以传统的方式铰接到门框，并且第二面板通过限制第二面板的弧的连杆固定到门框。 通过选择连杆的位置和长度，可以可预测地控制两个面板的相对运动，以在关闭时减小门的深度，并且在打开时减小门的长度。
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公开(公告)号：US10099768B2
公开(公告)日：2018-10-16
申请号：US15234684
申请日：2016-08-11
Applicant: B/E Aerospace, Inc.
Inventor： Justin C. Christenson , Graydon E. Loar
Abstract: A telescoping aircraft door is disclosed having first and second panels that slide relative to one another to extend and retract as the door closes and opens, respectively. The first panel is hinged to the door frame in a traditional manner, and the second panel is fixed to the door frame by a linkage that limits the arc of the second panel. By selecting the location and length of the linkage, the relative movement of the two panels can be predictably controlled to reduce the depth of the door when closed and the length of the door when opened.
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公开(公告)号：US20170001704A1
公开(公告)日：2017-01-05
申请号：US15234684
申请日：2016-08-11
Applicant: B/E Aerospace, Inc.
Inventor： Justin C. CHRISTENSON , Graydon E. Loar
IPC: B64C1/14
CPC classification number: B64C1/1423 , B64C1/1407 , B64D11/02 , E05D15/58 , E05F17/00 , E05Y2800/122 , E06B3/5009
Abstract: A telescoping aircraft door is disclosed having first and second panels that slide relative to one another to extend and retract as the door closes and opens, respectively. The first panel is hinged to the door frame in a traditional manner, and the second panel is fixed to the door frame by a linkage that limits the arc of the second panel. By selecting the location and length of the linkage, the relative movement of the two panels can be predictably controlled to reduce the depth of the door when closed and the length of the door when opened.
Abstract translation: 公开了一种伸缩式飞机门，其具有分别相对于彼此滑动的第一和第二面板，以在门关闭和打开时分别延伸和缩回。 第一面板以传统的方式铰接到门框，并且第二面板通过限制第二面板的弧的连杆固定到门框。 通过选择连杆的位置和长度，可以可预测地控制两个面板的相对运动，以在关闭时减小门的深度，并且在打开时减小门的长度。
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公开(公告)号：US09440727B2
公开(公告)日：2016-09-13
申请号：US14754620
申请日：2015-06-29
Applicant: B/E Aerospace, Inc.
Inventor： Justin C. Christenson , Graydon E. Loar
CPC classification number: B64C1/1423 , B64C1/1407 , B64D11/02 , E05D15/58 , E05F17/00 , E05Y2800/122 , E06B3/5009
Abstract: A telescoping aircraft door is disclosed having first and second panels that slide relative to one another to extend and retract as the door closes and opens, respectively. The first panel is hinged to the door frame in a traditional manner, and the second panel is fixed to the door frame by a linkage that limits the arc of the second panel. By selecting the location and length of the linkage, the relative movement of the two panels can be predictably controlled to reduce the depth of the door when closed and the length of the door when opened.
Abstract translation: 公开了一种伸缩式飞机门，其具有分别相对于彼此滑动的第一和第二面板，以在门关闭和打开时分别延伸和缩回。 第一面板以传统的方式铰接到门框，并且第二面板通过限制第二面板的弧的连杆固定到门框。 通过选择连杆的位置和长度，可以可预测地控制两个面板的相对运动，以在关闭时减小门的深度，并且在打开时减小门的长度。
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