Cabinet for aircraft and aircraft
阅读说明:本技术 用于飞行器的机柜和飞行器 (Cabinet for aircraft and aircraft ) 是由 贝纳德·格兰 罗曼·德拉艾 于 2020-03-11 设计创作,主要内容包括:本发明涉及用于飞行器的机柜和飞行器。飞行器飞行所需的所有数据都存储在远离驾驶舱设置的包壳中,并且因此需要布线的长度很长。在远离地设置在航空电子设备舱室中的驾驶舱配置中,线缆长度较短。通过提出一种机柜,本发明提供了进一步的改善,所述机柜包括至少一个屏幕(30,32),所述至少一个屏幕允许显示所述飞行器飞行控制所需的数据,所述数据连接至至少一个用于管理所述数据的航空电子设备模块(22),所述屏幕至少部分地形成所述机柜(16)的侧面之一,并且所述一个或多个模块被安装在所述机柜内,所述机柜具有基部(26),所述基部允许将所述一个或多个屏幕放置在期望的高度。结果,屏幕和航空电子设备模块之间的线缆长度减少到最小。(The invention relates to a cabinet for an aircraft and an aircraft. All the data required for the flight of the aircraft are stored in an envelope located remotely from the cockpit and therefore require a long length of wiring. In cockpit configurations remotely located in the avionics bay, the cable length is short. The invention provides a further improvement by proposing a cabinet comprising at least one screen (30, 32) allowing the display of data required for flight control of the aircraft, said data being connected to at least one avionics module (22) for managing said data, said screen forming at least partially one of the sides of the cabinet (16), and said one or more modules being mounted inside the cabinet, said cabinet having a base (26) allowing the placement of said one or more screens at a desired height. As a result, the cable length between the screen and the avionics module is reduced to a minimum.)
1. A cabinet for an aircraft, characterized in that it comprises at least one screen (30, 32) allowing the display of data required for the flight of the aircraft, said data being connected to at least one avionics module (22) for managing the data, said screen forming at least partially one of the sides of the cabinet (16), and said one or more modules (22) being mounted inside the cabinet, said cabinet having a base (26) allowing the placement of said one or more screens at a desired height.
2. The cabinet according to claim 1, characterized in that at least one screen (30, 32) is movable so as to allow access to at least one avionics module (22).
3. The cabinet according to claim 2, wherein the one or more avionics modules are placed behind at least one screen (30, 32) allowing access to all of the modules.
4. The cabinet according to one of the preceding claims, wherein in the case of a plurality of avionics modules (22), the avionics modules (22) take the form of parallelepiped units juxtaposed on a horizontal plane.
5. The cabinet of one of the preceding claims, wherein at least one screen (30, 32) is hinged to rotate around one of the edge corners of the cabinet.
6. The cabinet according to one of the preceding claims, characterized in that one part of the screen (30, 32) forms a flight data display device and in that another part of the screen forms a device for displaying the environment outside the aircraft.
7. The cabinet according to one of the preceding claims, characterized in that the cabinet (16) comprises two screens (30, 32) at different vertical levels.
8. The cabinet according to claim 7, characterized in that the upper screen (30) is in a vertical plane and the lower screen (32) is in an inclined plane.
9. The cabinet according to any one of the preceding claims, wherein a control (34) is fixed to or incorporated in the base (26).
10. The cabinet according to one of the preceding claims, wherein the base (26) comprises a compartment for storing aircraft equipment.
11. An aircraft comprising a cockpit (6) comprising at least one cabinet according to one of claims 1 to 10.
12. The aircraft of claim 11, characterized in that the cockpit (6) is remotely located with respect to an upper forward portion (8) of the aircraft.
Technical Field
The present application relates to the field of structures for supporting equipment for processing and displaying data required for the flight of an aircraft. The application also relates to an aircraft equipped with such a structure.
Background
The present invention relates to the field of transport aircraft, and in particular to passenger transport aircraft and/or transport aircraft carrying cargo. The cockpit is the space reserved for the pilot. The cockpit is generally found in the cockpit, traditionally located at the front of the fuselage, in the upper region of the nose, equipped with large front and side windows that provide the pilot with a direct view of the external environment. The cockpit contains all the controls (for actuating the control surfaces and other controls for the high-lift flaps, landing gear, brakes, etc.) and also the instrumentation required for the flight, for example a screen allowing the display of flight data. Such a collection of controls and meters is hereinafter referred to as a flight device. In the cockpit, the screen faces the driver. The structure used to hold the screen at the level of the pilot is often heavy, complex, and heavy. These structures must support electrical harnesses, data transmission cables, and ventilation ducts that allow screen operation.
All data required for the flight (hereinafter referred to as avionics data) are stored in an enclosure or cabinet containing a computer, board, power module, or any other electronic and/or electrical equipment. These enclosures are usually arranged vertically and are constructed based on a load-bearing chassis on which horizontal shelves are mounted. The electrical and mechanical connections are made using a rack. The cabinet is arranged, remote from the cabin, in a so-called avionics cabin located in the lower fuselage portion, below the floor supporting the cockpit and the passengers, and for example in the nose, below the cabin. In view of the amount of data to be stored and processed, the cooling and ventilation devices required, the accessibility required for performing maintenance operations, the operations of checking and replacing or repairing components, there is not enough space in the cabin area to install and maintain these. As a result, the length of wiring that transfers data from the enclosure in the avionics compartment to the controls, screens, or other equipment in the cockpit is long.
Patent application FR3000028 filed on 12/19/2013 of AIRBUS SAS discloses a cockpit which is located far away from the upper region of the nose, i.e. in a cabin, for example. As a result, the cockpit is closer to the avionics bay and the length of the cables is reduced.
It is an object of the invention to propose an aircraft cabinet enabling a further improvement in the proximity between the flight control screen and the avionics modules.
Disclosure of Invention
To this end, the invention relates to a cabinet for an aircraft, characterized in that it comprises at least one screen allowing the display of data required for flight control of the aircraft, said data being connected to at least one avionics module for managing said data, said screen forming at least partially one of the sides of the cabinet, and said one or more modules being mounted inside the cabinet, said cabinet having a base allowing the placement of said one or more screens at a desired height.
In this way, the avionics module is as close as possible to the flight control screen in a very simple holding structure.
The present invention contemplates at least one of the following optional features, taken alone or in combination.
At least one screen is movable to allow access to at least one avionics module.
The one or more avionics modules are placed behind at least one screen that allows access to all of the modules.
In the case of a plurality of avionics modules, said avionics modules take the form of parallelepiped units juxtaposed on a horizontal plane.
At least one screen is hinged to rotate about one of the edge corners of the cabinet.
One part of the screen forms a flight data display device and another part of the screen forms a device for displaying the environment outside the aircraft.
The cabinet includes two screens at different vertical levels.
The upper screen is in a vertical plane and the lower screen is in a tilted plane.
Controls are fixed to or incorporated in the base.
The base includes a compartment for storing aircraft equipment.
The invention also relates to an aircraft comprising a cockpit comprising at least one cabinet having one or more of the above-mentioned features.
The cockpit may be located remotely relative to the upper forward portion of the aircraft.
Drawings
Further objects, features and advantages will become apparent from the following description of the invention, given by way of non-limiting example only with reference to the accompanying drawings, in which:
figure 1 is a schematic side view in longitudinal section of a forward part of an aircraft according to the invention;
FIG. 2 is a schematic perspective view from the rear of a remote cockpit comprising a plurality of cabinets according to the present invention, one of which has a screen in an open position;
FIG. 3 is the same depiction as the cockpit of FIG. 2 with the multiple screens in an open position;
fig. 4 is a schematic perspective view of another form of embodiment of the cockpit in fig. 2 and 3, comprising only one single cabinet;
fig. 5 is the same depiction as the cockpit of fig. 4, with the avionics module depicted as transparent.
Detailed Description
The invention finds particular application in the field of the transportation of passengers or goods, in particular in the aeronautical field. The vehicle 2 given by way of illustration in the following description is an aircraft intended for commercial passenger transport. The invention can be applied in other fields and, for example, relates to transport aircraft carrying cargo.
It will be assumed that the aircraft 2 rests on a
The invention relates to a cockpit 6 that is remotely located with respect to a forward upper portion 8 of an aircraft that normally houses the cockpit (above a floor 9 separating the cockpit from an avionics compartment 10). More specifically, in the illustrated example, the cockpit is remotely located in an avionics bay 10, which is commonly referred to as an "electrical and electronics bay. This area is located in the nose 12, below the cabin, and partly below the floor 9 of the space dedicated to the passenger cabin 14. Any other area (e.g., a portion of luggage holder 18) that is sufficiently spacious to provide access to
The cockpit 6 includes at least one
The
The
a. the first part defines a storage and
b. A supporting second portion which forms the
In the embodiment illustrated in the figures, the
In accordance with the illustrated embodiment, the
The storage and
The second part is a base 26 forming a seat for the first part. The second portion supports the first portion. In this way, as seen previously, the screen supported by the first part is at the desired height, for example at an altitude that allows the data to be displayed appropriately to the pilot.
One or
Various embodiments are described in more detail in the remainder of the specification.
According to the embodiment of fig. 2 and 3, a plurality of
To ensure this cohesion uniformity, according to another possible form, the
In the embodiment of fig. 2 and 3, the first and second portions are composed of three
As depicted in fig. 3, the
In the embodiment shown in fig. 4 and 5, the cabinet is comprised of a single unit. The cabinet has the two parts. The first section includes two vertically juxtaposed
Fig. 5 shows transparently the
Since the avionics module has been integrated directly into the structure supporting the screen, the proposed cabinet makes it possible to provide easy access for maintenance simply by moving the screen. All the maintenance related to avionics modules, displays, interfaces is concentrated in the same single cabinet. The routing length and wiring harness between the screen and the avionics module are reduced to a minimum and the weight thereof is accordingly reduced. The base of the cabinet provides additional space for storing various items within the reach of the pilot.
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