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Aeroplane with an air cargo restraint system along the centreline of an aeroplane cargo compartment and procedures for installing a containment system in a rivergzeug

机译:沿飞机货舱中心线设有航空货物限制系统的飞机,以及在Rivergzeug中安装安全壳系统的程序

摘要

an aeroplane with an air cargo hold system along the centreline (902) of an aeroplane cargo hold;the ground support outside the airframe area (970) is perpendicular to the aeroplane;a side cargo door (919) and longitudinal seat rails (410, 904A, 904B, 905A) mounted on one floor of the cargo compartment on both sides of the centre line (902);905B) and lockers (400, 906A, 906B) has, with a variety of mechanical restraints (100, 600, 920A to 920G, 930A to 930G),mounted on the bottom of the cargo compartment on both sides of the centreline (902) and at one end of each seat rail (410, 904A, 904B, 905A),905B) and at the opposite end are attached to each mounting frame (400, 906A, 906B) and to a plate with rollers,mounted at the bottom of the cargo compartment near the side cargo door (919) and at one of two opposite ends an incoming guidance device (122, 522, 704, 949A,951A) and along one side (951) of two opposite sides (951, 953) has several incoming guiding devices (122, 522, 704, 949A, 951A),where each mechanical restraint (100, 600, 920A to 920G, 930A to 930G) includes a locking head (124, 524, 947),which can be rotated between a position entered and an upright position, characterized by:the mechanical restraint systems (100, 600, 920A to 920G, 930A to 930G) are installed behind the wing compartment area (970) of the aircraft;at least one part of each mechanical restraint (100, 600, 920A to 920G, 930A to 930G) is above one of the ground supports running in the cross direction of the aircraft (970);and the roller -bearing plate consists of at least one pivot plate (937A, 937B) mounted on the other side of the centreline (902),which is removed from the side cargo door (919),where the spinning wheel plate (s) (937A, 937B) along another side (953) of the two opposite sides (951, 953) has a variety of mountings (957),included in a seat rail (410, 904A, 904B, 905A, 905B).
机译:沿着飞机货舱的中心线(902)装有空中货舱系统的飞机;机身区域(970)外部的地面支撑垂直于飞机;侧门(919)和纵向座椅导轨(410, 904A,904B,905A)安装在中心线(902)两侧的货舱地板上; 905B)和储物柜(400、906A,906B)具有各种机械约束(100、600、920A)到920G,930A到930G),安装在中心线(902)两侧货舱的底部以及每个座椅导轨(410、904A,904B,905A),905B的一端)和另一端固定在每个安装框架(400、906A,906B)和带有滚轮的板上,并安装在靠近侧门(919)的货舱底部,并在两个相对端之一处安装一个进入的导向装置(122, 522、704、949A,951A)和沿两个相对侧面(951、953)的一侧(951)具有多个进入的导向装置(122、522、704、949A,9)如图51A所示),其中每个机械约束(100、600、920A至920G,930A至930G)包括一个锁定头(124、524、947),该锁定头可以在进入的位置和直立的位置之间旋转,其特征在于:机械约束系统(100、600、920A至920G,930A至930G)安装在飞机机翼机舱区域(970)的后面;每个机械约束装置(100、600、920A至920G,930A至930G)的至少一部分位于沿飞机横向(970)运行的地面支撑之一的上方;滚轮轴承板由至少一个枢轴板(937A,937B)组成,该枢轴板安装在中心线(902)的另一侧,并从侧面货舱门(919)卸下,其中沿两个相对侧(951、953)的另一侧(953)的纺车轮板(937A,937B)具有各种安装件(957),包括在座椅导轨(410、904A,904B)中, 905A,905B)。

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