摘要:
An aircraft cabin divider is so constructed that its installation can easily be handled by one person taking advantage of the force of gravity. For this purpose the divider has a frame with a first plug-in section that cooperates with a second socket section in the cabin structure, for example, the cabin floor or the cabin seating structure. The plug-in and socket sections cooperate so that an automatic lock-in is accomplished or so that a slight turn will provide the required interlocking. At least two couplings each including a plug-in section and a socket section are provided.
摘要:
A floor system for a fuselage section of an aircraft is provided. The floor system has an essentially self-supporting design and is substantially mechanically separate from the fuselage section as primary structure. Consequent to the free or self-supporting design of the floor system in the fuselage cell, the layout of the floor system along an aircraft axis can be matched to customer specifications in a simple manner without reference to structural boundary conditions of the fuselage structure. A floor surface for the floor system is formed from a number of floor elements which can be fitted with functional elements, wherein filling of empty spaces or cavities can be achieved with a number of floor equalization elements. As the floor elements have a relatively large support or fixing surface the loads induced by the functional elements are introduced into the floor system distributed over a large area such that the structural components thereof can be of a structurally lighter and thus weight-saving size.
摘要:
A module for an aircraft having a fuselage structure and a floor element defining a floor plane. The module includes a frame device adapted for mounting a functional element and the frame device is adapted for attachment to the floor element of the aircraft at a first location in the floor plane. The frame device is adapted for attachment to the fuselage structure of the aircraft at a second location, wherein the second location is not in the floor plane.
摘要:
The invention concerns a fuel tank (1) for a motor vehicle comprising a filler connection (2) enclosing a tank refueling passage (11) and operational and tank refueling venting conduits (3, 4) which are connected to a filler head (6) of the filler connection (2), wherein the filler head (6) has at least one change-over switching valve (9) which in a first switching position (tank refueling position) opens a flow path from the tank refueling venting conduit (3) to a fuel vapor filter and closes a connection of the operational venting conduit (4) to the tank refueling passage (11), and which in a second switching position (operational position) opens the connection of the operational venting conduit (4) to the tank refueling passage (11) and closes the flow path from the tank refueling venting conduit (3) to the fuel vapor filter. The fuel tank according to the invention is distinguished in that the operational venting means is connected to the fuel vapor filter primarily by way of the change-over switching valve (9), wherein the change-over switching valve opens the flow path from the operational venting conduit (4) to the fuel vapor filter in the second switching position and closes same in the first switching position (FIG. 1).
摘要:
A luggage retention device may be affixed underneath a seat area of a passenger seat and includes an upper element and a lower element which may be made of flexible materials. The upper element in the region of a backrest of the passenger seat is spaced apart from the lower element to form a raised part, and in the region of a front edge of a seat area contacts the lower element to form a part of the luggage retention device, the part being arranged so as to be lying substantially flat.
摘要:
A passenger chair or a group of passenger chairs, particularly in an aircraft cabin, is equipped with a convenience device that includes an open storage bail which can hold only flat articles but not waste material, and a waste container for holding waste material but not flat articles. The storage bail and waste container form either a mounting unit or retrofit kit or are separate components. In both instances the mounting unit and the separate components are secured to a back facing area of a chair or group of chairs. The separate components are preferably so constructed that individual retrofit kits are provided.
摘要:
Comprehensive techniques identify data leaks in software applications using Asset Flow Analysis (AFA) to determine whether critical data leaves a system through an exit point such that the data is no longer protected by mechanisms of the system. A novel data extrusion mechanism makes use of a relevant subset of all the possible data paths detected by AFA using a knowledge base of critical business functions and critical database content. The system checks if any code performs read access to critical business data and subsequently transfers this data beyond the control limits of the target system. The knowledge base can be extended by configuring which database content is to be regarded as critical in any given organization. The approach is particularly valuable in protecting systems that manipulate, distribute, or store sensitive information associated with financial, business, or personal data, including SAP® ABAP™ software applications.
摘要:
A module for an aircraft having a fuselage structure and a floor element defining a floor plane. The module includes a frame device adapted for mounting a functional element and the frame device is adapted for attachment to the floor element of the aircraft at a first location in the floor plane. The frame device is adapted for attachment to the fuselage structure of the aircraft at a second location, wherein the second location is not in the floor plane.
摘要:
A stowage bin arrangement for fastening a stowage bin for an aircraft, includes a stowage bin unit with a first direction of extension. The stowage bin unit may be fastened to an aircraft structure and be designed such that the stowage bin unit is capable of being telescopically extended along the first direction of extension.
摘要:
The present invention relates to a seat device for an aircraft. The seat device comprises a seat installation and a shell structure. In this arrangement the inside of the shell structure comprises an enclosed stowage space, wherein the shell structure is designed to attach the seat installation to a floor structure. In this arrangement the enclosed stowage space is designed to accommodate an item of baggage.