Base plate assembly and aircraft containing it

Abstract

This application relates to the field of aircraft technology and discloses a base plate assembly for an aircraft cockpit, including a base plate that runs through the entire bottom area of ​​the aircraft and integrates a multi-functional block; the multi-functional block includes: a first functional area for placing nose equipment; a second functional area for placing the cockpit; and a third functional area for placing cable equipment.

Description

Technical Field

[0001] This application relates to the field of powered aircraft technology, and more particularly to a base plate assembly and an aircraft comprising the same. Background Technology

[0002] Existing aircraft place batteries, avionics, and wiring harnesses at the bottom of the cockpit, resulting in limited space at the bottom of the cockpit and limited height space inside the cockpit. This makes it impossible to guarantee sufficient height for users to stand up, or sufficient space at the bottom of the cockpit to accommodate equipment structures. Summary of the Invention

[0003] The purpose of this application is to provide a base plate assembly for an aircraft cockpit, comprising:

[0004] The base plate extends through the entire bottom area of ​​the aircraft and integrates multi-functional blocks;

[0005] The multi-functional block includes:

[0006] The first functional area is used to place the machine head equipment;

[0007] The second functional area is used to house the cockpit;

[0008] The third functional area is used to house cable equipment.

[0009] Optionally, the first functional area is provided with several seat pre-embedded parts for installing the nose seat.

[0010] Optionally, the second functional area includes an active area and a fixed area, wherein the active area is a space for user activities and the fixed area is for the placement of seats in the cabin.

[0011] Optionally, the active area has a recessed groove, the planar dimension of which is lower than the planar dimension of the fixed area.

[0012] Optionally, the fixing part is provided with a number of second-zone seat pre-embedded parts for installing cabin seats.

[0013] Optionally, the second zone seat embedded parts are distributed on both sides of the groove, and the second zone seat embedded parts are arranged in pairs.

[0014] Optionally, the third functional area has a base plate door, which communicates with the internal space of the base plate and is used to place cable equipment.

[0015] Optionally, the base plate is provided with a clearance groove around its perimeter.

[0016] Optionally, the back of the base plate is provided with strength reinforcing ribs.

[0017] This application also provides an aircraft that includes the base plate assembly described in the above-described scheme. Attached Figure Description

[0018] Figure 1 The diagram shown is an overall schematic diagram of the base plate assembly according to an embodiment of this application.

[0019] Figure 2 This is a schematic diagram of the overall functional areas of the base plate assembly in an embodiment of this application.

[0020] Figure 3 This is a detailed schematic diagram of the second functional area of ​​the base plate assembly according to an embodiment of this application.

[0021] Figure 4 This is a detailed schematic diagram of the groove in the second functional area of ​​the base plate assembly according to an embodiment of this application.

[0022] Figure 5 The diagram shows a detailed schematic of the reinforcing ribs in the second functional area of ​​the base plate assembly according to an embodiment of this application. Detailed Implementation

[0023] The following embodiments further illustrate the technical solutions of this application. It should be understood that the specific embodiments described herein are merely for explaining this application. Furthermore, it should be noted that, for ease of description, only the parts relevant to this application are shown in the accompanying drawings, not all of them.

[0024] In the description of this application, it should be noted that, unless otherwise expressly specified and limited, the terms "installation," "connection," and "linking" should be interpreted broadly. For example, they can refer to fixed connections or detachable connections; mechanical connections or electrical connections; direct connections or indirect connections through an intermediate medium; and internal connections between two components. Those skilled in the art can understand the specific meaning of the above terms in this application based on the specific circumstances.

[0025] In this application, unless otherwise expressly specified and limited, "above" or "below" the second feature can include direct contact between the first and second features, or contact between the first and second features through another feature between them. Furthermore, "above," "over," and "on top" of the second feature includes the first feature being directly above or diagonally above the second feature, or simply indicates that the first feature is at a higher horizontal level than the second feature. "Below," "below," and "under" the second feature includes the first feature being directly below or diagonally below the second feature, or simply indicates that the first feature is at a lower horizontal level than the second feature.

[0026] The term "aircraft" is defined as an air transport system of any size having at least one lift propeller as its propulsion source. The term "aircraft" can include both "manned" and "unmanned" air transport systems. A manned aircraft can mean an air transport system carrying one or more human passengers, none of whom have control over the aircraft. A manned aircraft can also mean an air transport system carrying one or more human passengers, some of whom, or one of whom, has partial or full control over the aircraft. An unmanned aircraft can mean an air transport system that does not carry any human passengers and flies autonomously or is remotely controlled by someone at a distance.

[0027] In this specification, "aircraft" includes manned aircraft and any unmanned vehicle, such as unmanned aerial vehicles (UAVs), unmanned aircraft, remote-controlled aircraft, unmanned aircraft systems, any aircraft classified by the International Civil Aviation Organization (ICAO) under cycle 328AN / 190, and so on. As an example, a drone can take the form of a single- or multi-rotor helicopter (such as a quadcopter) or a fixed-wing aircraft. Furthermore, certain portions of this disclosure can be used in conjunction with drones in the form of other types of unmanned vehicles (e.g., wheeled, tracked, and / or watercraft).

[0028] Embodiments of this application are described below with reference to the accompanying drawings, such as Figure 1 As shown, Figure 1 The present application describes a base plate assembly for an aircraft cockpit, comprising a base plate 400 extending through the entire bottom region of the aircraft, and integrating various multi-functional blocks on the base plate 400.

[0029] Specifically, refer to Figure 1 As shown, in this embodiment, the base plate 400 has an overall elliptical shape, and starting from the middle part of the base plate 400, it has a structure that gradually narrows from the middle to both ends.

[0030] Of course, in another embodiment, the base plate 400 may take on other shapes as a whole, such as a cuboid, and starting from the middle part of the base plate 400, it may take on a structure that gradually maintains the same width from the middle to both ends. This application does not impose any further restrictions on this.

[0031] Please continue reading now. Figure 1 ,like Figure 1 As shown, the base plate 400 in this embodiment integrates three functional areas, specifically including a first functional area 100, a second functional area 200, and a third functional area 300.

[0032] Of course, in other embodiments, more or fewer functional areas may be integrated, such as only two functional areas, or four or even five functional areas may be integrated. This application does not impose further restrictions on this.

[0033] Please continue reading now. Figure 1 ,like Figure 1 As shown, in this embodiment, the first functional area 100 is located at the front end of the base plate 400 and is mainly used to place various important equipment in the nose compartment; the second functional area 200 is adjacent to the first functional area 100 and is used to place various necessary equipment and devices in the cockpit; while the third functional area 300 is used to place cable equipment.

[0034] In another embodiment, the positions of the first functional area 100 and the third functional area 300 may be interchanged, or the positions of the second functional area 200 and the third functional area 300 may be interchanged. This application does not impose further restrictions on this.

[0035] Please continue reading now. Figure 1 ,like Figure 1 As shown, in this embodiment, the second functional area 200 occupies the largest space, followed by the first functional area 100, and finally the third functional area 300. Specifically, the second functional area 200 occupies approximately half of the entire base plate 400, the first functional area 100 occupies approximately 30% of the entire base plate 400, and the third functional area 300 occupies approximately 20% of the entire base plate 400.

[0036] Of course, in other embodiments, the first functional area 100 or the third functional area 300 may occupy the largest space. The design can be improved according to different user needs, and this application does not impose any further restrictions on this.

[0037] It is worth noting that, in this embodiment, one end of the first functional area 100 and the third functional area 300 is arc-shaped, and the other end is straight. Therefore, the first functional area 100 and the third functional area 300 as a whole present a semi-elliptical shape, while the cross-section of the second functional area 200 is rectangular, so it presents a rectangular shape as a whole.

[0038] Of course, in other embodiments, the first functional area 100, the second functional area 200 and the third functional area 300 may also present other shapes. For example, the second functional area 200 may also present a shape similar to an ellipse. This application does not impose further restrictions on this.

[0039] Please refer to the following for details. Figure 2The first functional area 100 mainly serves to place the equipment required for the engine head. Therefore, several seat pre-embedded parts 110 are provided in the first functional area 100, and then the engine head seat is installed at the seat pre-embedded parts 110.

[0040] Specifically, in this embodiment, the seat pre-embedded parts 110 are arranged in pairs, with four parts per group, thus forming a space for installing one seat. Specifically, this application provides eight seat pre-embedded parts 110, thus allowing the installation of two seats.

[0041] Of course, in other embodiments, the number of seat pre-embedded parts 110 can be other numbers, as long as it is an integer multiple of four. For example, the number of seat pre-embedded parts 110 can be twelve, so that three seats can be installed. Or, the number of seat pre-embedded parts 110 can be sixteen, so that four seats can be installed. Of course, when the space of the first functional area 100 is small, there can be only four seat pre-embedded parts 110, so that only one seat can be installed.

[0042] It is worth noting that, in this embodiment, the arrangement interval of the seat embedded parts 110 is equal, that is, the interval between every two seat embedded parts 110 is equal to that between each other.

[0043] Of course, in other embodiments, the spacing between the seat embedded parts 110 can be unequal. It can be set such that the spacing between the first group of seat embedded parts 110 is slightly larger and the spacing between the second group of seat embedded parts 110 is slightly smaller. In this way, one seat can be designed to be larger and the other seat can be designed to be smaller to meet the different needs of different users. This application does not impose any further restrictions on this.

[0044] Please continue reading now. Figure 2 ,like Figure 2 As shown, in this embodiment, the seat embedded part 110 is installed close to the junction of the first functional area 100 and the second functional area 200, which allows the seat to have more space for movement towards the head of the machine.

[0045] Of course, in another embodiment, when the space of the first functional area 100 is relatively large, the position of the seat embedded part 110 can be appropriately moved away from the junction of the first functional area 100 and the second functional area 200, so that more activity space is left at the junction of the first functional area 100 and the second functional area 200, or the spacing of the seat embedded part 110 can be appropriately increased, so that the seat occupies more space and improves the comfort of the seat.

[0046] Please continue reading now. Figure 3 ,like Figure 3As shown, in this embodiment, the second functional area 200 mainly includes an activity area 210 and a fixed area 220. Specifically, the activity area 210 is mainly used for user activity space, and the fixed area 220 is mainly used for the placement of seats in the cabin.

[0047] It is worth noting that in this embodiment, the active area 210 is located in the middle of the second functional area 200, while the fixed area 220 is located on both sides of the second functional area 200.

[0048] Of course, in another embodiment, the second functional area 200 can adopt other layouts. For example, the fixed area 220 is located in the middle of the second functional area 200, while the active area 210 is located on both sides of the second functional area 200. The specific design is based on different user needs, and this application does not impose further restrictions on this.

[0049] Furthermore, in this application, the activity area 210 occupies approximately half of the longitudinal direction of the entire second functional area 200 and is located approximately in the center of the second functional area 200, making it convenient for users to move around, while the remaining two sides are fixed areas 220.

[0050] Of course, in another embodiment, the proportion of the activity area 210 in the vertical direction of the entire second functional area 200 can be larger or smaller, depending on the specific user needs. This application does not impose any further restrictions on this.

[0051] Please continue reading now. Figure 3 ,like Figure 3 As shown, the activity area 210 roughly covers the entire horizontal area of ​​the second functional area 200, thus giving users more space to move around.

[0052] Of course, in another embodiment, the activity area 210 may occupy more or less of the horizontal space of the entire second functional area 200, depending on the specific user needs. This application does not impose any further restrictions on this.

[0053] It is worth noting that, please refer to the following now. Figure 4 ,like Figure 4 As shown in this application, different users have different heights. In order to accommodate different users with different heights, a downward recessed groove 260 is provided in the activity area 210. The planar dimension of the groove 260 is lower than the planar dimension of the fixed area 220. In this way, when a user enters the cabin, if the user's height is over 1.8 meters, he / she will not have to bend over when standing, thus improving the user's experience.

[0054] Specifically, the depth of the recess 260 is not further limited in this application, but can be adjusted according to actual needs.

[0055] Please refer to the following: Figure 3 ,like Figure 3 As shown, similar to the previous one, the fixed area 220 is provided with several second-zone seat pre-embedded parts 230 for installing cabin seats.

[0056] Each group of four can accommodate one cabin seat, distributed on both sides of the recess 260. Specifically, in this embodiment, there are four groups of second-zone seat pre-embedded parts 230 in the cabin, which can accommodate a total of four cabin seats.

[0057] Of course, in another embodiment, the number of embedded parts 230 for the second seat can be other groups, which can be adjusted according to actual needs. This application does not impose further restrictions.

[0058] Please continue reading now. Figure 3 ,like Figure 3 As shown, a base plate door 310 is provided within the third functional area 300. The base plate door 310 can be opened or closed and is connected to the internal space of the base plate 400. It can be used to place cables and other equipment.

[0059] Please continue reading now. Figure 3 ,like Figure 3 As shown, in order to install the aircraft door onto the base plate 400, several clearance slots 240 are provided around the base plate 400. This allows the aircraft door to be installed onto the main structure of the aircraft after filling the gaps in the clearance slots 240.

[0060] Please refer to now. Figure 5 ,like Figure 5 As shown, the back of the base plate 400 is provided with a strength reinforcing rib 250, which can increase the overall strength of the base plate 400.

[0061] Specifically, in this embodiment, the strength reinforcing ribs 250 are distributed throughout the entire base plate 400 and are arranged in an alternating manner.

[0062] This application also provides an aircraft that includes the base plate assembly described in the above-described scheme.

[0063] The above embodiments are merely illustrative of the principles and effects of this application. Any person skilled in the art can modify or alter the above embodiments without departing from the purpose of this application. Therefore, all equivalent modifications or alterations made by those skilled in the art without departing from the purpose disclosed in this application should still be covered by the claims of this application.

Claims

1. A base plate assembly for an aircraft cockpit, characterized in that, include: The base plate extends through the entire bottom area of ​​the aircraft and integrates multi-functional blocks; The multi-functional block includes: The first functional area is used to place the machine head equipment; The second functional area is used to house the cockpit; The third functional area is used to house cable equipment.

2. The base plate assembly according to claim 1, characterized in that, The first functional area is equipped with several seat pre-embedded parts for installing the nose seat.

3. The base plate assembly according to claim 1, characterized in that, The second functional area includes an active area and a fixed area. The active area is used for user activities, and the fixed area is used for the placement of seats in the cabin.

4. The base plate assembly according to claim 3, characterized in that, The active area has a recessed groove, the planar dimension of which is lower than the planar dimension of the fixed area.

5. The base plate assembly according to claim 4, characterized in that, The fixing part is provided with several second-zone seat pre-embedded parts for installing cabin seats.

6. The base plate assembly according to claim 5, characterized in that, The second-zone seat pre-embedded parts are distributed on both sides of the groove, and the second-zone seat pre-embedded parts are arranged in pairs.

7. The base plate assembly according to claim 6, characterized in that, The third functional area has a base plate door, which is connected to the internal space of the base plate and is used to place cable equipment.

8. The base plate assembly according to claim 2, characterized in that, The base plate is provided with clearance grooves around its perimeter.

9. The base plate assembly according to claim 8, characterized in that, The back of the base plate is provided with reinforcing ribs.

10. An aircraft, characterized in that, The aircraft includes the base plate assembly as described in any one of claims 1-9.

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