Tablet computer support for aircraft cabin simulator
By designing a bracket joint assembly and a tablet stand with a silicone protective case suitable for aircraft cockpit simulators, the problem of the lack of brackets for aircraft cockpit simulators has been solved, enabling convenient installation and a wide range of angle adjustments to meet the operational needs of pilots.
Patent Information
- Application Number
- CN202423267211.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-12-30
- Publication Date
- 2025-11-18
- Estimated Expiration
- 2034-12-30
AI Technical Summary
Existing aircraft cockpit simulators lack suitable tablet holders, failing to meet the needs of pilots, especially the need for real-time operational reminders in the context of intelligent development.
A tablet stand including a support joint assembly and a silicone protective cover was designed. The angle of the tablet is controlled by a multi-segment adjustable arm, and the installation and adjustment are achieved by bolt connection. The support joint assembly consists of a windshield frame connector, multiple joints and lever arms. The silicone protective cover is easy to disassemble through a slot design.
A tablet computer holder with a simple structure, wide adjustment range, and convenient operation is provided. It is adapted to the usage habits of pilots, is lightweight and small in size, and is easy to assemble, meeting the needs of aircraft cockpit simulators.
Smart Images

Figure CN223563938U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to the field of aircraft cabin simulator, especially a tablet computer support for aircraft cabin simulator. BACKGROUND
[0002] At present, aircraft simulation cabin develops more and more towards the direction of intelligence, and users put forward more use requirements, among which the requirement of reminding pilots to operate at any time by means of tablet computer is more and more clear. Most aircraft cabin simulators do not design similar tablet computer support structure because of no similar requirement. SUMMARY
[0003] The utility model aims at overcoming the insufficient of prior art, adapting to the actual need, provide a kind of tablet computer support for aircraft cabin simulator, including support joint assembly and silica gel protective sleeve;The support joint assembly one end can be detached and installed on windshield frame, and the windshield frame is fixedly installed on cabin body;The support joint assembly other end is equipped with silica gel protective sleeve, and the silica gel protective sleeve is used to install tablet computer.
[0004] The support joint assembly includes windshield frame connecting piece, first joint, first force arm, second joint, second force arm, third joint and silica gel protective sleeve connecting piece;The windshield frame connecting piece, first force arm, second force arm and silica gel protective sleeve connecting piece are sequentially connected;The windshield frame connecting piece and first force arm are connected by first joint;First force arm and second force arm are connected by second joint;Second force arm and silica gel protective sleeve connecting piece are connected by third joint.
[0005] The silica gel protective sleeve connecting piece and silica gel protective sleeve are connected by bolt.
[0006] The windshield frame connecting piece section is U-shaped, and the middle groove is clamped into windshield frame and fixed by sequentially screwing bolt.
[0007] The utility model has the advantages that:
[0008] The utility model provides a tablet computer support suitable for aircraft simulation cabin, the structure of the support is simple, the angle of tablet is controlled by multiple adjusting arms, the adjusting range is large, and the use habit of pilot is adapted. By bolt pre-tightening, general spanner is used for adjusting, and assembly is convenient. The tablet computer support for aircraft cabin simulator has the advantages of small weight and volume, simple structure, convenient operation and the like. BRIEF DESCRIPTION OF DRAWINGS
[0009] The utility model will be further described below in connection with the drawings and embodiment.
[0010] Fig. 1 ,2 The utility model discloses a structure schematic view.
[0011] Fig. 3 Support joint assembly schematic view. Specific implementation
[0012] The utility model is further explained below in connection with the drawings and examples:
[0013] Reference Figs. 1-3 .
[0014] The utility model discloses a kind of tablet computer support for aircraft cabin simulator, including support joint assembly 1-2 and silica gel protective sleeve 1-3;The support joint assembly 1-2 one end can be detachably mounted on windshield frame 1-1, the windshield frame 1-1 is fixedly installed on cabin body 1-4;The support joint assembly 1-2 other end is equipped with silica gel protective sleeve 1-3, and the silica gel protective sleeve 1-3 is used to install tablet computer.
[0015] The support joint assembly 1-2 includes, windshield frame connecting piece 2-1, first joint 2-2, first force arm 2-3, second joint 2-4, second force arm 2-5, third joint 2-6, silica gel protective sleeve connecting piece 2-7;The windshield frame connecting piece 2-1, first force arm 2-3, second force arm 2-5, silica gel protective sleeve connecting piece 2-7 are sequentially connected;The windshield frame connecting piece 2-1 and first force arm 2-3 are connected by first joint 2-2;First force arm 2-3 and second force arm 2-5 are connected by second joint 2-4;Second force arm 2-5 and silica gel protective sleeve connecting piece 2-7 are connected by third joint 2-6.
[0016] The silica gel protective sleeve connecting piece 2-7 and silica gel protective sleeve 1-3 are connected by bolt.
[0017] The windshield frame connecting piece 2-1 section is U-shaped, and the middle groove is clamped into windshield frame 1-1, and is fixed by bolt in sequence.
[0018] It is mainly composed of support joint assembly and silica gel protective sleeve by bolt fastening installation on windshield frame. Support joint assembly is composed of multiple joints, force arm, guarantees that support is adjusted in pilot visual range, adapts to pilot operation demand. The main part of silica gel protective sleeve is formed by silica gel material mold, when tablet computer is installed, it can be realized tablet computer dismounting by manual extrusion protective sleeve edge.
[0019] The support joint assembly is mainly composed of a windscreen frame connecting piece, a first joint, a first force arm, a second joint, a second force arm, a third joint and a silica gel protective sleeve connecting piece. The windscreen frame connecting piece is mainly provided with a bolt to ensure that the support is fixed on the windscreen frame; the first joint, the first force arm, the second joint, the second force arm and the third joint together constitute the adjusting mechanism of the support, and the joints and the force arms are connected through the hexagonal head screw and the damping provided by the wave-shaped metal gasket to move or stop. The silica gel protective sleeve connecting piece is provided with a clamping groove to quickly disassemble the silica gel protective sleeve, which is convenient for the maintenance of the tablet computer. If the damping of the joints is gradually weakened during long-term operation, the hexagonal head screw can be adjusted by a common wrench to adjust the damping of the joints, so that the tablet computer can be stopped within the adjusting range.
[0020] The silica gel protective sleeve has a streamlined design, a simple and elegant appearance and a bright black color. The back of the silica gel protective sleeve is provided with a metal connecting piece which is matched with the clamping groove of the support joint assembly to quickly disassemble the silica gel protective sleeve.
[0021] The above description is only an embodiment of the present application, and does not limit the patent range of the present application. Any equivalent transformation or direct or indirect application in the related technical field according to the content of the present application is also included in the patent protection range of the present application.
Claims
1. A tablet computer holder for an aircraft cockpit simulator, characterized in that: It includes a support joint assembly (1-2) and a silicone protective sleeve (1-3); one end of the support joint assembly (1-2) is detachably mounted on a windshield frame (1-1), and the windshield frame (1-1) is fixedly mounted on the cabin body (1-4); the other end of the support joint assembly (1-2) is equipped with a silicone protective sleeve (1-3), which is used to mount a tablet computer.
2. A tablet computer holder for an aircraft cockpit simulator according to claim 1, characterized in that: The bracket joint assembly (1-2) includes a windshield frame connector (2-1), a first joint (2-2), a first lever arm (2-3), a second joint (2-4), a second lever arm (2-5), a third joint (2-6), and a silicone protective sleeve connector (2-7). The windshield frame connector (2-1), the first lever arm (2-3), the second lever arm (2-5), and the silicone protective sleeve connector (2-7) are connected in sequence. The windshield frame connector (2-1) and the first lever arm (2-3) are connected through the first joint (2-2). The first lever arm (2-3) and the second lever arm (2-5) are connected through the second joint (2-4). The second lever arm (2-5) and the silicone protective sleeve connector (2-7) are connected through the third joint (2-6).
3. A tablet computer holder for an aircraft cockpit simulator according to claim 2, characterized in that: The silicone protective sleeve connector (2-7) and the silicone protective sleeve (1-3) are connected by bolts.
4. A tablet computer holder for an aircraft cockpit simulator according to claim 2, characterized in that: The windshield frame connector (2-1) has a U-shaped cross section, with a central groove that fits into the windshield frame (1-1) and is fixed by screwing in bolts in sequence.