Eine Plattform für die Wissenschaft: Bauingenieurwesen, Architektur und Urbanistik
Hinge hinge assembly for aircraft door
An articulated hinge assembly (200) for connecting a door (120) to a fuselage (106) of an aircraft (100) includes an articulated hinge arm (202) having a first hinge member (210) pivotally coupled to a second hinge member (250) at an elbow (204). The fuselage fitting (220) is pivotally coupled to the fuselage bracket (130), and the door fitting (260) is pivotally coupled to a door bracket (126) of the door (120). The articulated hinge arm (202) is movable from a retracted position to a deployed position to move the door (120) from a door closed position to a door open position. The articulated hinge assembly (200) includes a linkage assembly (300) coupled to the articulated hinge arm (202), the fuselage fitting (220), and the door fitting (260) that controls movement of the first hinge member (210) and the second hinge member (250) relative to each other and relative to the fuselage fitting (220). The linkage assembly (300) controls the positioning of the door (120).
用于将门(120)连接到飞机(100)的机身(106)的铰接铰链组件(200)包括具有在肘部(204)处可枢转地联接到第二铰链构件(250)的第一铰链构件(210)的铰接铰链臂(202)。机身配件(220)可枢转地联接到机身支架(130),并且门配件(260)可枢转地联接到门(120)的门支架(126)。铰接铰链臂(202)可从收缩位置移动到展开位置以将门(120)从门关闭位置移动到门打开位置。铰接铰链组件(200)包括联接到铰接铰链臂(202)、机身配件(220)和门配件(260)的联动装置组件(300),该联动装置组件控制第一铰链构件(210)和第二铰链构件(250)相对于彼此和相对于机身配件(220)的移动。联动装置组件(300)控制门(120)的定位。
Hinge hinge assembly for aircraft door
An articulated hinge assembly (200) for connecting a door (120) to a fuselage (106) of an aircraft (100) includes an articulated hinge arm (202) having a first hinge member (210) pivotally coupled to a second hinge member (250) at an elbow (204). The fuselage fitting (220) is pivotally coupled to the fuselage bracket (130), and the door fitting (260) is pivotally coupled to a door bracket (126) of the door (120). The articulated hinge arm (202) is movable from a retracted position to a deployed position to move the door (120) from a door closed position to a door open position. The articulated hinge assembly (200) includes a linkage assembly (300) coupled to the articulated hinge arm (202), the fuselage fitting (220), and the door fitting (260) that controls movement of the first hinge member (210) and the second hinge member (250) relative to each other and relative to the fuselage fitting (220). The linkage assembly (300) controls the positioning of the door (120).
用于将门(120)连接到飞机(100)的机身(106)的铰接铰链组件(200)包括具有在肘部(204)处可枢转地联接到第二铰链构件(250)的第一铰链构件(210)的铰接铰链臂(202)。机身配件(220)可枢转地联接到机身支架(130),并且门配件(260)可枢转地联接到门(120)的门支架(126)。铰接铰链臂(202)可从收缩位置移动到展开位置以将门(120)从门关闭位置移动到门打开位置。铰接铰链组件(200)包括联接到铰接铰链臂(202)、机身配件(220)和门配件(260)的联动装置组件(300),该联动装置组件控制第一铰链构件(210)和第二铰链构件(250)相对于彼此和相对于机身配件(220)的移动。联动装置组件(300)控制门(120)的定位。
Hinge hinge assembly for aircraft door
用于飞机门的铰接铰链组件
MORTLAND MICHAEL T (Autor:in)
17.09.2024
Patent
Elektronische Ressource
Chinesisch
IPC:
E05D
Scharniere oder andere Aufhängevorrichtungen für Türen, Fenster oder Flügel
,
HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS, OR WINGS