Novel seat type control indicating device

Abstract

The utility model relates to the technical field of aircrafts, in particular to a novel seat type control indicating device which comprises a seat body, control systems are arranged on armrests on the two sides of the seat body in a sliding mode, and a display system is connected to the seat body in a rotating mode. The seat body, the control system and the display system are integrally arranged, so that the space of the aircraft is greatly saved, further, the operation panel capable of moving leftwards and rightwards is arranged, a driver conveniently enters and exits the seat body, the display screen is controlled by the operation panel to rotate at any angle, and on one hand, the driver conveniently enters and exits the seat body; on the other hand, a driver can conveniently adjust the display screen to a proper position and angle, and flexible switching between view fields needed for viewing display screen information and observing the environment outside the aircraft is achieved.

Description

Technical Field

[0001] The utility model relates to the technical field of aircraft, in particular to a novel seat type control and indication device. Background Art

[0002] At the present stage in the market, aircraft have begun to be applied to the market. The use of aircraft has further solved people's pursuit of the sky. The previous aerial vehicles such as airplanes can no longer meet people's exploration of the sky. Currently, there are various types of vertical take-off and landing urban aircraft, including multi-rotor, compound wing, tilt-rotor, etc. The flight time of compound wing and tilt-rotor aircraft is much higher than that of multi-rotor aircraft, but the control logic is relatively complex, and there are still relatively high risks during flight conversion.

[0003] In small manned aircraft, vehicles and other traveling mechanisms, in order to be flexible in operation and reduce self-weight, on the one hand, the external design size is reduced, and on the other hand, the operation functions are highly integrated in the cockpit, which can reduce the occupation of limited space. At present, in most cockpits, the seat and the operation control mechanism are separated, and the control system and the display system are not provided on the cockpit seat. Such a structural design will cause the problem of space waste. Content of the Utility Model

[0004] Aiming at the technical problem that in the prior art, the seat and the operation control mechanism in the aircraft are of a separated design, and the control system and the display system are not provided on the cockpit seat, thus causing the occupation and waste of limited space.

[0005] Technical idea: Based on the above problems, the present application provides a novel seat type control and indication device. Through the design of combining the control and indication structure with the seat, on the one hand, space can be saved, and on the other hand, the seat realizes the combination of multiple functions of sitting and operation control.

[0006] In order to achieve the above object, the technical solution adopted by the utility model is as follows:

[0007] The present application provides a novel seat type control and indication device, including a seat body. Control systems are slidably arranged on both armrests of the seat body, and a display system is rotatably connected to the seat body.

[0008] Further, the control system includes an operation panel. A chute is opened on the bottom surface of the operation panel, a rack is arranged in the chute, the chute is matched with a slide rail arranged on both armrests of the seat body, a gear is arranged in the slide rail, the gear meshes with the rack, and one end of the gear is connected with a motor.

[0009] Specifically, the operation panel is arranged in a triangular inclined plane structure.

[0010] Furthermore, a connecting sleeve is provided at the end of any one of the operation panels, and a connecting column is provided at the end of the other operation panel. The connecting column is sleeved with the connecting sleeve.

[0011] Further, the control system further includes joysticks provided on the armrests on both sides of the seat body, and the joysticks are used to control the angle adjustment of the display system.

[0012] In the above technical solution, the display system includes connecting rods rotatably connected to the armrests on both sides of the seat body. One end of the connecting rod is fixedly connected with a display screen. The other end of any one of the connecting rods is fixedly connected with a connecting block. An electric telescopic rod is rotatably connected to the connecting block, and the electric telescopic rod is rotatably connected to the seat body.

[0013] Compared with the prior art, the beneficial effects of the present utility model are as follows:

[0014] 1. By providing a control system and a display system on the seat body, on the one hand, the present utility model achieves the effect of saving space, and on the other hand, enables the seat to achieve the technical effect of combining the functions of sitting and operation control.

[0015] 2. By providing an operation panel with a triangular inclined plane structure, on the one hand, it is convenient for the driver to operate and observe, and at the same time can avoid blocking the front view. On the other hand, instructions can be sent through the operation panel.

[0016] 3. By providing a rack in the chute opened at the bottom of the operation panel, and by providing slide rails on the armrests on both sides of the seat body, and a gear connected to a motor is provided in the slide rails. Through the mutual cooperation of the gear and the rack, the left and right movement of the operation panel is realized, thereby facilitating the driver to enter and exit the seat body. And through the cooperation of the connecting sleeve and the connecting column provided on the inner side of the operation panel, the connection and support of the two operation panels are realized, increasing the overall stability of the operation panel.

[0017] 4. By rotatably providing connecting rods on both sides of the seat body, the display screen fixedly connected to the connecting rods can be used to observe the flight situation of the aircraft. By controlling the telescopic movement of the electric telescopic rod through the operating rod, the display screen can be driven to rotate at any position and angle. On the one hand, it is convenient for the driver to enter and exit the seat body, and on the other hand, it is convenient for the driver to adjust the display screen to a suitable position and angle, realizing the flexible switching between viewing the information on the display screen and observing the required field of view of the external environment of the aircraft. Description of the Drawings

[0018] To more clearly illustrate the technical solutions of the embodiments of the present application, the accompanying drawings required for use in the embodiments will be briefly introduced below. It should be understood that the following drawings only show some embodiments of the present application and should not be regarded as limiting the scope. For those of ordinary skill in the art, without creative efforts, other related drawings can also be obtained based on these drawings.

[0019] Figure 1 It is a diagram of the initial state of the overall structure of the present utility model;

[0020] Figure 2 It is the front view of the overall structure of the present utility model;

[0021] Figure 3 It is the left view of the overall structure of the present utility model;

[0022] Figure 4 For the present utility model Figure 3 The enlarged view of part A in it;

[0023] Figure 5 It is the operation state diagram of the overall structure of the present utility model;

[0024] Figure 6 It is the schematic diagram of part of the structure of the present utility model;

[0025] Figure 7 It is the schematic diagram of the operation panel structure of the present utility model;

[0026] In the figure: 1. Seat body; 2. Control system; 21. Operation panel; 22. Slide groove; 23. Rack; 24. Slide rail; 25. Gear; 26. Motor; 27. Connecting sleeve; 28. Connecting column; 29. Operating rod; 3. Display system; 31. Link rod; 32. Display screen; 33. Connecting block; 34. Electric telescopic rod. Detailed implementation manners

[0027] In order to enable ordinary technicians in the art to better understand the technical solutions of the present utility model, the technical solutions of the present utility model will be further described below in conjunction with the drawings and embodiments.

[0028] In the description of the present utility model, it should be understood that the orientation or positional relationship indicated by terms such as "upper", "lower", "front", "rear", "left", "right", "front end", "rear end", "inner side", "outer side", etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore should not be construed as a limitation to the present utility model.

[0029] In the description of the present application, it should also be noted that unless otherwise clearly specified and limited, the terms "set", "installed", "connected", and "coupled" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral connection; it can be directly connected or indirectly connected through an intermediate medium, and it can be the communication inside two components. For those of ordinary skill in the art, the specific meanings of the above terms in the present application can be understood according to specific situations.

[0030] The inventors have found through research that in vertical take-off and landing aircraft, the existing aircraft usually separate the pilot's seat and the control system into two parts, which is not conducive to the rational use of the aircraft space.

[0031] Based on this, the present application provides a new type of seat-type control and indication device, including a seat body 1, control systems 2 are slidably arranged on both armrests of the seat body 1, and a display system 3 is rotatably connected to the seat body 1. Embodiment

[0032] Referring to Figures 1-7 As shown, the present application provides a new type of seat-type control and indication device, including a seat body 1, control systems 2 are slidably arranged on both armrests of the seat body 1, and a display system 3 is rotatably connected to the seat body 1.

[0033] It should be noted that the control system 2 and the display system 3 are electrically connected.

[0034] Further, the control system 2 includes an operation panel 21, a chute 22 is opened on the bottom surface of the operation panel 21, a rack 23 is arranged in the chute 22, the chute 22 is matched with a slide rail 24 arranged on both armrests of the seat body 1, a gear 25 is arranged in the slide rail 24, the gear 25 meshes with the rack 23, and one end of the gear 25 is connected with a motor 26.

[0035] Preferably, the operation panel 21 is a triangular inclined plane structure. On the one hand, it is convenient for the driver to operate and observe, and at the same time can avoid blocking the front view. On the other hand, instructions can be sent through the operation panel 21.

[0036] Furthermore, a connecting sleeve 27 is arranged at the end of any one operation panel 21, a connecting column 28 is arranged at the end of the other operation panel 21, and the connecting column 28 is sleeved with the connecting sleeve 27.

[0037] Specifically, the control system 2 further includes joysticks 29 arranged on both armrests of the seat body 1, and the joysticks 29 are used to control the angle adjustment of the display system 3.

[0038] During the specific operation process, the motor 26 drives the gear 25 to rotate. By the meshing of the gear 25 and the rack 23, the operation panel 21 can be moved left and right along the slide rail 24, facilitating the driver to enter and exit the seat body 1. And through the cooperation of the connecting sleeve 27 and the connecting column 28 arranged inside the operation panel 21, the connection and support of the two operation panels 21 are realized, increasing the overall stability of the operation panel 21.

[0039] Further, in the above technical solution, the display system 3 includes a connecting rod 31 rotatably connected to the armrests on both sides of the seat body 1. One end of the connecting rod 31 is fixedly connected with a display screen 32. The other end of any one of the connecting rods 31 is fixedly connected with a connecting block 33. An electric telescopic rod 34 is rotatably connected to the connecting block 33, and the electric telescopic rod 34 is rotatably connected to the seat body 1.

[0040] Preferably, the display screen 32 is a transparent sandwich structure, which can "see through" the display screen to continuously observe the outside real scene, and can also display the information required for flight as needed through the ultra-thin transparent light-emitting elements in the sandwich layer.

[0041] It should be noted that the flight condition of the aircraft can be observed through the display screen 32, and the position of the display screen 32 can be arbitrarily adjusted by controlling the electric telescopic rod 34 through the operating rod 29, facilitating the driver to flexibly switch between viewing the information on the display screen 32 and observing the required field of view of the external environment of the aircraft.

[0042] As an example, a micro-projector is provided at the front end of each armrest on both sides of the seat body 1, facilitating projection onto the windshield in front of and above the aircraft to form a head-up display.

[0043] Specific application cases

[0044] Taking a vertical takeoff and landing aircraft as an example, the application of a new type of seat-type control and indication device of the present application in a vertical takeoff and landing aircraft will be specifically described.

[0045] At the present stage in the market, aircraft have begun to be applied in the market. The use of aircraft has further solved people's pursuit of the sky. The previous aerial vehicles such as airplanes can no longer meet people's exploration of the sky. Currently, there are various types of vertical takeoff and landing urban aircraft, including multi-rotors, compound wings, tilt rotors, etc. For compound wings and tilt rotor aircraft, the flight time is greatly improved compared with multi-rotors, but the control logic is relatively complex, and there are still relatively high risks during flight conversion.

[0046] In small manned aircraft, in order to be flexible in operation and reduce the self-weight, on the one hand, the design size is reduced, and on the other hand, the operation functions are highly integrated in the cockpit, which can reduce the occupation of limited space.

[0047] Based on this, the present application proposes a novel seat-type operation indicating device applicable to an aircraft. During the specific operation process, the motor 26 is started, and the motor 26 drives the gear 25 to rotate. Through the meshing of the gear 25 and the rack 23, the chute 22 on the bottom surface of the operation panel 21 can move left and right along the slide rail 24, thereby driving the operation panel 21 to move to both sides, facilitating the driver to enter and exit the seat body 1.

[0048] Furthermore, by reversing the motor 26, and then through the cooperation of the gear 25 and the rack 23, the operation panel 21 moves towards the inside of the seat body 1. Through the mutual sliding and sleeving of the connecting sleeve 27 and the connecting column 28 provided on the inside of the operation panel 21, the connection and support of the two operation panels 21 are realized, increasing the overall stability of the operation panel 21.

[0049] Even further, the electric telescopic rod 34 is controlled to expand and contract through the operating rod 29, and then the display screen 32 is driven to be adjusted to any angular position through the connecting block 33. On the one hand, it facilitates the driver to enter and exit the seat body 1, and on the other hand, it facilitates the driver to adjust the display screen 32 to a suitable position and angle, realizing a flexible switch between viewing the information on the display screen 32 and observing the external environment of the aircraft.

[0050] In summary, although the embodiments of the present invention have been shown and described, those of ordinary skill in the art can understand that various changes, modifications, substitutions, and variations can be made to these embodiments without departing from the principles and purposes of the present invention. The scope of the present invention is defined by the claims and their equivalents.

Claims

1. A novel seat-type operating indicator device, comprising a seat body (1), characterized in that: Control systems (2) are slidably provided on the armrests on both sides of the seat body (1), and a display system (3) is rotatably connected to the seat body (1); The control system (2) comprises an operation panel (21), a bottom surface of the operation panel (21) is provided with a slide groove (22), a rack (23) is arranged in the slide groove (22), the slide groove (22) cooperates with a slide rail (24) arranged on the armrests on both sides of the seat body (1), a gear (25) is arranged in the slide rail (24), the gear (25) is meshed with the rack (23), and one end of the gear (25) is connected to a motor (26); The control system (2) further comprises a joystick (29) arranged on the armrests on both sides of the seat body (1), wherein the joystick (29) is used to control the angle adjustment of the display system (3); The display system (3) comprises a connecting rod (31) rotatably connected to the armrests on both sides of the seat body (1), one end of the connecting rod (31) being fixedly connected to a display screen (32), the other end of any of the connecting rods (31) being fixedly connected to a connecting block (33), the connecting block (33) being rotatably connected to an electric telescopic rod (34), and the electric telescopic rod (34) being rotatably connected to the seat body (1).

2. A novel seat-type operating indicator device according to claim 1, characterized in that: A connecting sleeve (27) is provided at the end of any one of the operating panels (21), and a connecting column (28) is provided at the end of the other operating panel (21), wherein the connecting column (28) is sleeve-connected with the connecting sleeve (27).

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