CN210039208U - Aircraft simulator frame with buffer protection - Google Patents
Aircraft simulator frame with buffer protection Download PDFInfo
- Publication number
- CN210039208U CN210039208U CN201822042663.6U CN201822042663U CN210039208U CN 210039208 U CN210039208 U CN 210039208U CN 201822042663 U CN201822042663 U CN 201822042663U CN 210039208 U CN210039208 U CN 210039208U
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- frame
- protection plate
- aircraft simulator
- protection
- baffle
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Abstract
The utility model relates to an aircraft simulator frame with buffer protection, including base and support body subassembly, the base top surface is connected the support body subassembly, the support body subassembly includes left guard plate, right guard plate, coupling spring, baffle and operation frame, the right side of left guard plate is equipped with first spout, the left side of right guard plate is equipped with the second spout, left side guard plate is connected to the right guard plate, operation frame's left side is equipped with first draw runner, operation frame's right side is equipped with the second draw runner, operation frame's preceding window, diaphragm and control panel of being equipped with, operation frame is connected to the baffle. An aircraft simulator frame with buffer protection have good cushioning effect to the impulsive force, can effectually protect operating personnel.
Description
Technical Field
The utility model relates to an aircraft technical field especially relates to an aircraft simulator frame with buffering protection.
Background
In the prior art, in order to better simulate a specific driving environment, the aircraft simulator is usually arranged in a cabin, and a frame for installing and/or carrying the aircraft simulator is also arranged in the cabin; the aircraft simulator comprises a display screen, instrument equipment, host equipment and an operation and control device, wherein the aircraft simulator frame comprises a window frame for installing and bearing the display screen and a main frame for installing and/or bearing the instrument equipment, the host equipment and the operation and control device.
When an operator enters the interior of the airplane simulation cabin to carry out airplane simulation operation, flight simulation accidents and trauma occur due to improper operation of the operator or incomplete protection facilities of the simulation cabin in the simulation flight process, for example, in the simulation process of takeoff or emergency acceleration, the operator can be separated from operation due to backward movement of inertia, so that simulation accidents are caused; during the landing or scram simulation, the forward movement of the operator due to inertia can often cause the simulation personnel to impact on the frame during the simulated flight, causing trauma.
To this end, an aircraft simulator frame with cushioning protection is devised to solve the above-mentioned problems.
Disclosure of Invention
The utility model provides an airplane simulator frame with buffer protection to overcome the above disadvantages, which comprises a base and a frame body component;
the rear part of the top surface of the base is connected with the frame body component, the frame body component comprises a left protection plate, a right protection plate, a connecting spring, a baffle and an operation frame, the left protection plate and the right protection plate are correspondingly arranged on the left side and the right side of the top surface of the base, a first chute with a rightward opening is formed in the right side of the left protection plate, a second chute corresponding to the first chute is formed in the left side of the right protection plate, the baffle is fixedly connected with the rear part of the left protection plate and the right protection plate, the left protection plate, the right protection plate and the baffle are matched with each other to look down to form an n-shaped structure, the left protection plate is connected to the right protection plate through the operation frame, a first slide bar matched with the first chute is arranged on the left side of the operation frame, a second slide bar matched with the second chute is arranged on the right side of the operation frame, the front of the operation frame is sequentially provided with a window, a transverse plate and a control plate from top to bottom, the rear of the operation frame is connected to the baffle plate through the connecting spring, and the connecting spring can stretch and compress to play a role of buffering;
furthermore, the operating frame is in a bottomless trapezoid frame structure when viewed from top;
further, the number of the connecting springs is 2;
furthermore, the number of the windows is 3, and the windows are respectively arranged on the plane where the 3 edges of the operation frame are located;
further, the left protection plate and the right protection plate are both made of elastic rubber materials;
furthermore, a seat corresponding to the airplane simulator frame with the buffer protection is arranged behind the base.
The utility model has the advantages that:
an aircraft simulator frame with buffer protection have good cushioning effect to the impulsive force, can effectually protect operating personnel.
Drawings
Fig. 1 is a front view of an aircraft simulator frame with cushioning protection according to the present invention;
fig. 2 is a left side view of an aircraft simulator frame with cushioning protection according to the present invention;
fig. 3 is a top view of an aircraft simulator frame with cushioning protection according to the present invention;
fig. 4 is a schematic perspective view of an aircraft simulator frame with buffer protection according to the present invention;
wherein: 1-a base; 2-left guard plate; 201-a first runner; 3-right protective plate; 4-connecting a spring; 5-a baffle plate; 6-an operating frame; 601-a window; 602-a transverse plate; 603-control panel.
Detailed Description
The following detailed description will be made in conjunction with embodiments of the present invention with reference to the accompanying drawings.
An aircraft simulator frame with buffer protection comprises a base 1 and a frame body assembly;
the rear part of the top surface of the base 1 is connected with the frame body component, the frame body component comprises a left protection plate 2, a right protection plate 3, a connecting spring 4, a baffle 5 and an operation frame, the left protection plate 2 and the right protection plate 3 are correspondingly arranged on the left side and the right side of the top surface of the base 1, a first chute 201 with a rightward opening is arranged on the right side of the left protection plate 2, a second chute corresponding to the first chute 201 is arranged on the left side of the right protection plate 3, the baffle 5 is fixedly connected behind the left protection plate 2 and the right protection plate 3, the left protection plate 2, the right protection plate 3 and the baffle 5 are matched to form an n-shaped overlook structure, the left protection plate 2 is connected to the right protection plate 3 through the operation frame 6, a first slide bar matched with the first chute 201 is arranged on the left side of the operation frame 6, a second sliding strip matched with the second sliding groove is arranged on the right side of the operating frame 6, a window 601, a transverse plate 602 and a control plate 603 are sequentially arranged in front of the operating frame 6 from top to bottom, the rear of the operating frame 6 is connected to the baffle 5 through the connecting spring 4, and the connecting spring 4 can be stretched and compressed to play a buffering role;
further, the operating frame 6 is in a trapezoidal frame structure without a bottom line when viewed from top;
further, 2 connecting springs 4 are arranged;
furthermore, the number of the windows 601 is 3, and the windows are respectively installed on the plane where the 3 edges of the operating frame are located;
further, the left protection plate 2 and the right protection plate 3 are both made of elastic rubber materials;
further, a seat corresponding to the airplane simulator frame with the buffer protection is arranged behind the base 1.
The using method comprises the following steps:
an aircraft simulator frame with cushioning protection is installed.
When the aircraft is used, an operator controls the control panel 603 and observes the window 601 to simulate the flight of the aircraft; when the aircraft is in simulated takeoff or accelerated flight, people can move backwards due to inertia, people can pull the operating frame 6 forwards, the operating frame 6 can move forwards under the action of the sliding strip and the sliding groove, the distance between the operating frame 6 and an operator is shortened, and the operating frame 6 drives the connecting spring 4 to buffer external force; when emergency braking is performed, people can push the operating frame 6 backwards due to the fact that inertia inclines forwards, the operating frame 6 moves backwards under the action of the sliding strip and the sliding groove, the distance between the operating frame 6 and an operator is increased, and the operating frame 6 presses the connecting spring 4 backwards to buffer external force; people are when the simulation is turned, because the too fast health striking is on left guard plate 2 and right guard plate 3, and operating personnel can be protected to left guard plate 2 and right guard plate 3 of elastic material.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are used merely for convenience of description and for simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, should not be construed as limiting the present invention. Furthermore, the terms "first", "second", etc. are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first," "second," etc. may explicitly or implicitly include one or more of that feature. In the description of the present invention, unless otherwise specified, "X", "Y", "Z" in the coordinates refer to their mutual position or orientation relationship within the aircraft, merely for convenience of description of the movement or position relationship of the present invention, and are not to be construed as limiting thereof.
In the description of the present invention, "a plurality" means two or more unless otherwise specified.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art through specific situations.
It should be noted that, in the present invention, the embodiments and features of the embodiments may be combined with each other without conflict. The foregoing is only a preferred embodiment of the present invention, and it should be noted that, for those skilled in the art, various modifications and decorations can be made without departing from the principle of the present invention, and these modifications and decorations should also be regarded as the protection scope of the present invention.
Claims (6)
1. An aircraft simulator frame with buffer protection is characterized by comprising a base (1) and a frame body assembly;
the rear part of the top surface of the base (1) is connected with the frame body component, the frame body component comprises a left protection plate (2), a right protection plate (3), a connecting spring (4), a baffle (5) and an operation frame, the left protection plate (2) and the right protection plate (3) are correspondingly arranged on the left side and the right side of the top surface of the base (1), a first sliding groove (201) with a rightward opening is formed in the right side of the left protection plate (2), a second sliding groove corresponding to the first sliding groove (201) is formed in the left side of the right protection plate (3), the left protection plate (2) and the right protection plate (3) are fixedly connected with the baffle (5) at the rear part, the left protection plate (2), the right protection plate (3) and the baffle (5) are matched with each other to overlook to form an n pi-shaped structure, the left protection plate (2) is connected with the right protection plate (3) through the operation, the left surface of operation frame (6) be equipped with the first draw runner of first spout (201) looks adaptation, the right side of operation frame (6) be equipped with the second draw runner of second spout looks adaptation, the preceding from the top down of operation frame (6) is equipped with window (601), diaphragm (602) and control panel (603) in proper order, operation frame (6) rear is passed through connecting spring (4) are connected to baffle (5).
2. An aircraft simulator frame with shock absorbing protection according to claim 1, characterized in that the handling frame (6) is seen from above in a bottomless trapezoidal frame structure.
3. An aircraft simulator frame with shock protection according to claim 1, characterized in that there are 2 of said connecting springs (4).
4. An aircraft simulator frame with buffer protection according to claim 1 or 2, characterized in that the viewing windows (601) are provided in 3 numbers and are respectively mounted on the plane of the 3 sides of the handling frame (6).
5. An aircraft simulator frame with shock protection according to claim 1 or 2, characterized in that said left protection plate (2) and said right protection plate (3) are both of an elastic rubber material.
6. An aircraft simulator frame with buffer protection according to claim 1, characterized in that a seat corresponding to the aircraft simulator frame with buffer protection is provided behind the base (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822042663.6U CN210039208U (en) | 2018-12-06 | 2018-12-06 | Aircraft simulator frame with buffer protection |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822042663.6U CN210039208U (en) | 2018-12-06 | 2018-12-06 | Aircraft simulator frame with buffer protection |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210039208U true CN210039208U (en) | 2020-02-07 |
Family
ID=69342842
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822042663.6U Active CN210039208U (en) | 2018-12-06 | 2018-12-06 | Aircraft simulator frame with buffer protection |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210039208U (en) |
-
2018
- 2018-12-06 CN CN201822042663.6U patent/CN210039208U/en active Active
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