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SELF-SUPPORTING INTERNAL CONSTRUCTION UNIT OF THE SALON WITH THE INTERIOR ELEMENT OF THE SALON COMBINED WITH IT

机译:沙龙的自支撑内部建筑单元以及与其结合的沙龙内部元素

摘要

1. The structural block of the cabin, designed to attach the elements of the equipment of the cabin for the aircraft, which is made with the possibility of self-support and with the possibility of attachment to the structure (5; 6) of the aircraft. ! 2. The structural unit of the cabin according to claim 1, which contains:! free support (3), using which the structural unit (1) is attached to the structure (5; 6) of the aircraft, and at the same time has the ability to move in the longitudinal direction of the aircraft. ! 3. The structural unit of the cabin according to claim 1 or 2, which further comprises:! a fixed support (4), using which the structural unit (1) is attached to the structure (5; 6) of the aircraft in order to transmit forces along the longitudinal axis of the aircraft. ! 4. The structural unit of the cabin according to claim 1, which further comprises a damping element; ! moreover, the structural block (1) of the cabin is made with the possibility of fastening to the structure (5; 6) of the aircraft using a damping element to damp the vibrations of the aircraft structure. ! 5. The structural unit of the cabin according to claim 1, which further comprises:! many supporting frames (11); ! longitudinal rib (8) stiffening; ! moreover, the longitudinal rib (8) of stiffening is installed between all of the plurality of support frames (11); ! wherein the longitudinal rib (8) of stiffening is adapted to transmit forces along the longitudinal axis of the aircraft. ! 6. The structural unit of the cabin according to claim 1, which further comprises fixing means; ! moreover, the element (2) of the equipment of the cabin is attached, with the possibility of disconnection, to the structural unit (1) of the cabin, using the specified fastening means. ! 7. The structural block of the cabin according to claim 1, in which
机译:1.机舱的结构块,用于固定飞机机舱设备的元件,这种结构块具有自支撑的可能性,并且可以附接到飞机的结构(5; 6)。飞机。 ! 2.根据权利要求1所述的机舱的结构单元,其包括:自由支撑件(3),结构单元(1)通过该自由支撑件固定在飞机的结构(5; 6)上,同时具有在飞机纵向上移动的能力。 ! 3.根据权利要求1或2所述的机舱的结构单元,其进一步包括:固定支架(4),结构单元(1)通过该固定支架附接到飞机的结构(5; 6),以便沿飞机的纵轴传递力。 ! 4.如权利要求1所述的机舱的结构单元,其特征在于,还包括阻尼元件; !此外,机舱的结构块(1)可以通过使用阻尼元件来阻尼飞机结构的振动而固定到飞机的结构(5; 6)上。 ! 5.根据权利要求1所述的机舱的结构单元,其进一步包括:许多支撑框架(11); !纵向肋骨(8)变硬; !此外,在所有多个支撑框架(11)之间安装有纵向加强肋(8)。 !其中,加强的纵向肋(8)适于沿飞机的纵向轴线传递力。 ! 6.如权利要求1所述的机舱的结构单元,其特征在于,还包括固定装置。 !此外,使用指定的紧固装置,机舱设备的元件(2)可能断开连接到机舱的结构单元(1)。 ! 7.根据权利要求1所述的机舱的结构块,其中

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