Flight training simulator cabin mechanical structure

Abstract

The utility model discloses a flight training simulator cabin mechanical structure which is composed of a front skin, a light shield, a windshield frame, an opening frame, a framework assembly, a rear skin, a seat support, a floor, a first equipment support, a second equipment support, side skins, trundles and a cover plate. The side skins are arranged on the two sides of the framework assembly, the light shield and the windshield frame are arranged on the front side of the upper end of the framework assembly, the opening frame is arranged at the upper end of the framework assembly, the seat support, the floor, the first equipment support and the second equipment support are arranged in the cabin, and the trundles are arranged at the bottom of the cabin. The bottom cover plate is arranged on the side face of the bottom of the framework assembly. According to the simulator cabin designed by the utility model, the internal and external structures of a real aircraft are restored to the greatest extent, and corresponding equipment can be mounted in the cabin frame to restore the driving state of the real aircraft, so that a pilot can quickly find the real driving state, the pilot is accelerated to be familiar with driving, and the efficiency is improved.

Description

Technical Field

[0001] This utility model relates to the field of flight simulator technology, and in particular to a mechanical structure for a flight training simulator cockpit. Background Technology

[0002] Flight training simulators are ground training support equipment that realistically simulates flight performance, handling characteristics, and cockpit layout. They primarily serve to simulate and train pilots in flying skills, handling special situations, and basic tactical skills, enabling them to become familiar with aircraft performance, master aircraft flying techniques, understand the functions, performance, and operation of airborne equipment and weapons, and master basic tactical methods. This reduces training safety risks and improves the military and economic benefits of training. This utility model provides a flight training simulator cockpit structure. Utility Model Content

[0003] The purpose of this invention is to provide a mechanical structure for a flight training simulator cockpit.

[0004] The above-mentioned technical objective of this utility model is achieved through the following technical solution:

[0005] A flight training simulator cockpit mechanical structure comprises a front skin, a sunshade, a windshield frame, an opening frame, a frame assembly, a rear skin, a seat bracket, a floor, equipment bracket one, equipment bracket two, side skins, casters, and a cover plate. The front and rear skins are mounted on the front and rear sides of the frame assembly, the side skins are located on both sides of the frame assembly, the sunshade and windshield frame are located on the upper front side of the frame assembly, the opening frame is located at the upper end of the frame assembly, the seat bracket, floor, equipment bracket one, and equipment bracket two are located inside the cockpit, the casters are located at the bottom of the cockpit, and the bottom cover plate is located on the bottom side of the frame assembly. Equipment bracket one and equipment bracket two provide installation interfaces for mounting equipment.

[0006] Furthermore, the skeleton assembly is welded together from ribs, stringers, crossbeams, and longitudinal beams.

[0007] Furthermore, the windshield frame is designed with a rearview mirror mounting interface.

[0008] Furthermore, the front skin and bottom cover are connected to the frame assembly via a quick-release structure.

[0009] In summary, the present invention has the following beneficial effects: the simulator cockpit designed by the present invention restores the internal and external structure of the real aircraft to the greatest extent, and can install corresponding equipment in the cockpit frame to restore the real aircraft's driving state, allowing pilots to quickly find the real driving state, speeding up pilots' familiarity with driving, and improving efficiency. Attached Figure Description

[0010] Figure 1This is a structural diagram of the cockpit;

[0011] Figure 2 This is a top-down view of the cockpit;

[0012] Figure 3 This is a structural diagram of the skeleton component.

[0013] In the diagram, 1-1, front skin; 1-2, sun visor; 1-3, windshield frame; 1-4, mouth frame; 1-5, frame assembly; 1-6, rear skin; 1-7, seat bracket; 1-8, floor; 1-9, equipment bracket one; 1-10, equipment bracket two; 1-11, side skin; 1-12, casters; 1-13, bottom cover plate; 2-1, rib plate; 2-2, stringer; 2-3, crossbeam; 2-4, longitudinal beam. Detailed Implementation

[0014] The present invention will be further described in detail below with reference to the accompanying drawings. The technical solutions in the embodiments of the present invention will be clearly and completely described. Obviously, the described embodiments are only some embodiments of the present invention, and not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those skilled in the art without creative effort are within the protection scope of the present invention.

[0015] like Figure 1-3 As shown, a flight training simulator cockpit mechanical structure comprises a front skin 1-1, a sunshade 1-2, a windshield frame 1-3, an air intake frame 1-4, a frame assembly 1-5, a rear skin 1-6, a seat bracket 1-7, a floor 1-8, an equipment bracket 1-9, an equipment bracket 2 1-10, side skins 1-11, casters 1-12, and a cover plate 1-13. The front skin 1-1 and the rear skin 1-6 are installed on the front and rear sides of the frame assembly 1-5, and the side skin 1-11 is located on the frame assembly 1-5. On both sides, the sunshade 1-2 and windshield frame 1-3 are located on the upper front side of the frame assembly 1-5, the mouth frame 1-4 is located on the upper end of the frame assembly 1-5, the seat bracket 1-7, floor 1-8, equipment bracket one 1-9, and equipment bracket two 1-10 are located inside the cabin, the casters 1-12 are located at the bottom of the cabin, and the bottom cover plate 1-13 is located on the bottom side of the frame assembly 1-5; the equipment bracket one 1-9 and equipment bracket two 1-10 provide installation interfaces for the installed equipment.

[0016] Furthermore, the frame assembly 1-5 is welded from rib plate 2-1, stringer 2-2, crossbeam 2-3, and longitudinal beam 2-4. Each component has a simple structure and has undergone heat treatment to meet strength requirements.

[0017] Furthermore, the windshield frame 1-3 is designed with a rearview mirror mounting interface. The front skin 1-1, sunshade 1-2, rear skin 1-6, side skin 1-11, and bottom cover 1-13 are exterior components, and their colors can be customized according to user requirements. The windshield frame 1-3 is designed with a rearview mirror mounting interface for mounting a rearview mirror; it also has a handrail for the pilot to use when getting on and off the aircraft. The frame 1-4 provides a mounting platform for the locking mechanism, the seat center pull ring safety pin support, the micro-explosive lock switch, etc. The seat bracket 1-7 provides a mounting interface for the pilot's seat. The floor 1-8 has pre-fabricated support plate nuts, providing a mounting interface for equipment such as the seat bracket 1-7. Equipment bracket one 1-9 and equipment bracket two 1-10 provide mounting interfaces for equipment such as the display screen. The sunshade 1-10 is mainly used to block external light to avoid affecting the pilot's view of the cockpit equipment display.

[0018] Furthermore, the front skin 1-1 and the bottom cover 1-13 are connected to the frame assembly 1-5 through a quick-release structure. The quick-release structure can be a buckle, pin, or other structure, which facilitates quick maintenance.

[0019] This specific embodiment is merely an explanation of the present utility model and is not intended to limit the present utility model. After reading this specification, those skilled in the art can make modifications to this embodiment without contributing any inventive step, but as long as they are within the scope of the claims of the present utility model, they are protected by patent law.

Claims

1. A mechanical structure for a flight training simulator cockpit, characterized in that: It consists of a front skin (1-1), a sunshade (1-2), a windshield frame (1-3), a door frame (1-4), a frame assembly (1-5), a rear skin (1-6), a seat bracket (1-7), a floor (1-8), an equipment bracket one (1-9), an equipment bracket two (1-10), side skins (1-11), casters (1-12), and a bottom cover plate (1-13). The front skin (1-1) and the rear skin (1-6) are installed on the front and rear sides of the frame assembly (1-5), and the side skins (1-11) are located on both sides of the frame assembly (1-5). The sunshade (1-2) and windshield frame (1-3) are located on the upper front side of the frame assembly (1-5), the mouth frame (1-4) is located on the upper end of the frame assembly (1-5), the seat bracket (1-7), floor (1-8), equipment bracket one (1-9), and equipment bracket two (1-10) are located inside the cabin, the casters (1-12) are located at the bottom of the cabin, and the bottom cover plate (1-13) is located on the bottom side of the frame assembly (1-5); the equipment bracket one (1-9) and equipment bracket two (1-10) provide installation interfaces for the installed equipment.

2. The mechanical structure of a flight training simulator cockpit according to claim 1, characterized in that: The skeleton assembly (1-5) is welded together from ribs (2-1), stringers (2-2), crossbeams (2-3), and longitudinal beams (2-4).

3. The mechanical structure of a flight training simulator cockpit according to claim 1, characterized in that: The windshield frame (1-3) is designed with a rearview mirror mounting interface.

4. The mechanical structure of a flight training simulator cockpit according to claim 1, characterized in that: The front skin (1-1) and the bottom cover (1-13) are connected to the skeleton assembly (1-5) via a quick-release structure.

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