Wire management structure, base and flight simulator

Abstract

This utility model discloses a cable management structure for positioning a wire harness within the inner cavity of a rotating cylinder. The cable management structure includes a cable management base and a cable tie. The cable management base is positioned against the inner wall of the rotating cylinder; the cable tie is connected to the cable management base and is used to position the wire harness within the base. The wire harness rotates with the rotating cylinder relative to the rotating frame, preventing loosening or shifting of the wire harness; preventing poor contact, signal fluctuations or interruptions, and ensuring the control precision and display accuracy of the flight simulator. This utility model also discloses a base equipped with the cable management structure and a flight simulator equipped with the base.

Description

Technical Field

[0001] This utility model relates to the field of cable management technology for flight simulators, and more particularly to a cable management structure, a base provided with the cable management structure, and a flight simulator provided with the base. Background Technology

[0002] Existing flight simulators typically have wiring harnesses running through the inner cavity of their rotating shafts. These harnesses lack proper positioning within the shaft cavity, making them prone to loosening or shifting during operation. Loose wiring harnesses can lead to poor contact, causing signal fluctuations or interruptions, affecting the control precision and display accuracy of the flight simulator. Secondly, in high-vibration environments, the wiring harness may rub against other components, causing wear on the insulation layer and increasing the risk of short circuits or circuit failures. Furthermore, loose wiring harnesses are more susceptible to damage during daily use, requiring frequent inspection and maintenance, increasing operating costs and time. Finally, problems with wiring harness securing can lead to a decrease in overall system reliability, affecting the flight simulator's performance and user experience. Utility Model Content

[0003] The purpose of this utility model is to provide a cable management structure, a base with the cable management structure, and a flight simulator with the base.

[0004] This utility model provides a wire management structure for positioning wire bundles in the inner cavity of a rotating shaft cylinder. The wire management structure includes a wire management seat and a wire tie. The wire management seat is positioned on the inner wall of the rotating shaft cylinder. The wire tie is connected to the wire management seat and is used to position the wire bundle on the wire management seat.

[0005] This utility model also provides a base, which includes a rotating frame, a rotating cylinder, and a wire management structure. One end of the rotating cylinder is rotatably connected to the rotating frame. The wire management structure includes a wire management seat and a wire tie. The wire management seat is positioned on the inner wall of the rotating cylinder, and the wire tie is connected to the wire management seat.

[0006] This utility model also provides a flight simulator, which includes a base.

[0007] The cable management structure of this application features a cable management base positioned within the inner wall of the rotating cylinder. The cable harnesses running through the inner cavity of the rotating cylinder are fixedly connected to the cable management base via cable ties. During the operation of the flight simulator, the cable harnesses rotate with the rotating cylinder relative to the rotating frame, preventing loosening or shifting of the cable harnesses. This prevents poor wiring contact, signal fluctuations or interruptions, and ensures the control precision and display accuracy of the flight simulator. Even in high-vibration environments, the cable harnesses will not rub against other components, preventing wear on the insulation layer and reducing the risk of short circuits or circuit failures. Because the cable harnesses are positioned within the inner cavity of the rotating cylinder through the cable management structure, the flight simulator is less prone to damage during daily use, requiring less frequent inspection and maintenance, thus reducing operating costs and maintenance time. The cable harness positioning ensures the overall reliability of the system, improving the performance of the flight simulator and the user experience. Attached Figure Description

[0008] To more clearly illustrate the technical solution of this utility model, the accompanying drawings used in the embodiments will be briefly introduced below.

[0009] Figure 1 This is a three-dimensional structural diagram of the base provided in one embodiment of the present utility model.

[0010] Figure 2 yes Figure 1 A three-dimensional structural diagram of the rotating frame, rotating cylinder, and cable management structure.

[0011] Figure 3 yes Figure 2 A three-dimensional structural diagram of the rotating frame, rotating cylinder, and cable management structure from another perspective.

[0012] Figure 4 yes Figure 2 A three-dimensional structural exploded view of the rotating frame, rotating cylinder, and cable management structure.

[0013] Figure 5 yes Figure 3 A three-dimensional structural exploded view of the rotating frame, rotating cylinder, and cable management structure.

[0014] Figure 6 yes Figure 4 A three-dimensional structural diagram of the rotating frame, rotating cylinder, and cable management structure from another perspective.

[0015] Figure 7 yes Figure 4 Enlarged three-dimensional structure diagram of the cable management seat.

[0016] Figure 8 yes Figure 5 Enlarged three-dimensional structure diagram of the cable management seat.

[0017] Figure 9 yes Figure 2 A three-dimensional structural diagram of the rotating frame, rotating cylinder, and cable management structure from another perspective.

[0018] Figure 10 yes Figure 9 A side view of the rotating frame, rotating cylinder, and cable management structure.

[0019] Figure 11 yes Figure 10 A cross-sectional view along line XI-XI.

[0020] Figure 12 This is a three-dimensional structural diagram of a flight simulator provided in one embodiment of the present invention. Detailed Implementation

[0021] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some, not all, of the embodiments of the present utility model. All other embodiments obtained by those skilled in the art based on the embodiments of the present utility model without creative effort should fall within the protection scope of the present utility model.

[0022] It should be noted that, in this document, the reference to "embodiment" or "implementation" means that a specific feature, structure, or characteristic described in connection with an embodiment or implementation may be included in at least one embodiment of the present invention. The appearance of this phrase in various places in the specification does not necessarily refer to the same embodiment, nor is it a mutually exclusive, independent, or alternative embodiment. Those skilled in the art will understand, explicitly and implicitly, that the embodiments described herein can be combined with other embodiments.

[0023] The terms "first" and "second" used in this utility model are for descriptive purposes only and should not be construed as indicating or implying relative importance or implicitly specifying the number of indicated technical features. Therefore, a feature defined as "first" or "second" may explicitly or implicitly include one or more of the stated features. In the description of this utility model, "multiple" means two or more, unless otherwise explicitly specified. It should be noted in the description of this utility model that, unless otherwise explicitly specified and limited, the terms "installed," "connected," "linked," and "set on" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection; they can refer to a direct connection or an indirect connection through an intermediate medium; they can refer to the internal connection of two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model based on the specific circumstances.

[0024] Please see Figures 1 to 6 One embodiment of this utility model provides a base 100 for use in a flight simulator. The base 100 includes a rotating frame 20, a support frame 30, a rotating cylinder 40, and a cable management structure 50. The rotating frame 20 is rotatably connected to the support frame 30, one end of the rotating cylinder 40 is rotatably connected to the rotating frame 20, and the cable management structure 50 is connected to the rotating cylinder 40. The cable management structure 50 is used to position the wire bundle 60 in the inner cavity of the rotating cylinder 40. The cable management structure 50 includes a cable management seat 52 and a cable tie 54. The cable management seat 52 is positioned on the inner wall of the rotating cylinder 40, and the cable tie 54 is connected to the cable management seat 52. The cable tie 54 is used to position the wire bundle 60 in the inner cavity of the rotating cylinder 40 in the cable management seat 52.

[0025] The cable management structure 50 of this application has a cable management base 52 positioned within the inner wall of the rotating cylinder 40. The cable harness 60 passing through the rotating cylinder 40 is fixedly connected to the cable management base 52 by a cable tie 54. During the operation of the flight simulator, the cable harness 60 rotates with the rotating cylinder 40 relative to the rotating frame 20, preventing the cable harness 60 from becoming loose or shifting. This prevents poor wiring contact, signal fluctuations or interruptions, and ensures the control precision and display accuracy of the flight simulator. Even in high-vibration environments, the cable harness 60 will not rub against other components, preventing wear on the insulation layer of the cable harness 60 and reducing the risk of short circuits or circuit failures. Because the cable harness 60 is positioned within the inner cavity of the rotating cylinder 40 through the cable management structure 50, the flight simulator is less prone to damage during daily use, requiring less frequent inspection and maintenance, thus reducing operating costs and maintenance time. The positioning of the cable harness 60 does not affect the overall reliability of the system, improving the performance of the flight simulator and the user experience. In addition, the cable management structure 50 of this application has a simple structure, is easy to install, and has low processing costs.

[0026] Optionally, the rotating frame 20 includes a first rotating plate 22, a second rotating plate 24, and two end plates 25. The first rotating plate 22 and the second rotating plate 24 are spaced apart and face each other. The two end plates 25 are respectively connected to the opposite ends of the first rotating plate 22 and the second rotating plate 24. A clearance groove 26 is provided between the first rotating plate 22 and the second rotating plate 24, that is, the first rotating plate 22, the second rotating plate 24, and the two end plates 25 together form a clearance groove. One end of the rotating shaft cylinder 40 is located in the clearance groove 26, and the rotating shaft cylinder 40 is rotatably connected to the first rotating plate 22 and the second rotating plate 24. Specifically, the first rotating plate 22 and the second rotating plate 24 are both strip plates, and the end plates 25 are rectangular plates. The opposite ends of the end plates 25 are respectively connected to the first rotating plate 22 and the second rotating plate 24. The width of the clearance groove 26 is greater than the outer diameter of the rotating shaft cylinder 40. During the rotation of the rotating shaft cylinder 40 relative to the rotating frame 20, the rotating shaft cylinder 40 swings in the clearance groove 26. The first rotating plate 22 has a first rotating hole 220, which is connected to the clearance groove 26; the second rotating plate 24 has a second rotating hole 240, which is connected to the clearance groove 26, and the first rotating hole 220 and the second rotating hole 240 are coaxial.

[0027] The support frame 30 includes a first support member 32 and a second support member 34, which are spaced apart and directly opposite each other. A rotating frame 20 is located between the first support member 32 and the second support member 34, and is rotatably connected to the first support member 32 and the second support member 34. The first support member 32 and the second support member 34 support the rotating frame 20. Specifically, one end plate 25 of the rotating frame 20 is rotatably connected to the first support member 32, and the other end plate 25 of the rotating frame 20 is rotatably connected to the second support member 34. The axis of rotation between the first support member 32 and the end plate 25 is collinear with the axis of rotation between the second support member 34 and the end plate 25. In this embodiment, each of the two end plates 25 is provided with a rotating shaft 253. The first support member 32 is provided with a first shaft hole 323 facing the rotating shaft 253, and the second support member 34 is provided with a second shaft hole 343 facing the rotating shaft 253. The two rotating shafts 253 are rotatably inserted into the first shaft hole 323 and the second shaft hole 343, respectively. Optionally, bearings are respectively provided in the first shaft hole 323 and the second shaft hole 343, and the two rotating shafts 253 are respectively inserted into the inner cavities of the two bearings.

[0028] In other embodiments, the first shaft hole on the first support member 32 and the rotating shaft on the corresponding end plate 25 can be interchanged, that is, the first support member 32 is provided with a rotating shaft, and the end plate 25 is provided with a first shaft hole facing the rotating shaft, and the rotating shaft is rotatably inserted into the first shaft hole; the second shaft hole on the second support member 34 and the rotating shaft on the corresponding end plate 25 can be interchanged, that is, the second support member 34 is provided with a rotating shaft, and the end plate 25 is provided with a second shaft hole facing the rotating shaft, and the rotating shaft is rotatably inserted into the second shaft hole.

[0029] The base 100 also includes a first rotating shaft 72 and a second rotating shaft 74. The rotating shaft cylinder 40 is transportably connected to the first rotating plate 22 via the first rotating shaft 72, and the rotating shaft cylinder 40 is rotatably connected to the second rotating plate 24 via the second rotating shaft 74. The first rotating shaft 72 and the second rotating shaft 74 are coaxial. The rotating shaft cylinder 40 includes a cylinder body 42 and a handle head 44 disposed at one end of the cylinder body 42. The end of the cylinder body 42 away from the handle head 44 is accommodated in a relief groove 26, and the end of the cylinder body 42 away from the handle head 44 is rotatably connected to the first rotating plate 22 and the second rotating plate 24. The rotating shaft cylinder 40 has a first positioning hole 421 on the side facing the first rotating plate 22 and a second positioning hole 423 on the side facing the second rotating plate 24. The first positioning hole 421 and the second positioning hole 423 are coaxial. The opposite ends of the first rotating shaft 72 are respectively connected to the first rotating hole 220 and the first positioning hole 421. The opposite ends of the second rotating shaft 74 are respectively connected to the second rotating hole 240 and the second positioning hole 423. The first rotating shaft 72 and the second rotating shaft 74 are coaxial. The rotating shaft cylinder 40 and the rotating frame 20 rotate along the first rotating shaft 72 and the second rotating shaft 74.

[0030] Specifically, a first positioning surface 424 is provided on the side of the cylinder 42 facing the first rotating plate 22 away from the handle head 44, and a second positioning surface 425 is provided on the side of the cylinder 42 facing the second rotating plate 24 away from the handle head 44. Both the first positioning surface 424 and the second positioning surface 425 are parallel to the axis of the rotating shaft cylinder 40. A first positioning hole 421 is located at the end of the first positioning surface 424 away from the handle head 44 and connects to the inner cavity 401 of the rotating shaft cylinder 40. A second positioning hole 423 is located at the end of the second positioning surface 425 away from the handle head 44 and connects to the inner cavity 401 of the rotating shaft cylinder 40. A plurality of first connecting holes 426 are provided around the first positioning surface 424 and the first positioning hole 421. The inner wall of the rotating shaft cylinder 40 is provided with at least two fixing holes 402, which are arranged along the axial direction of the rotating shaft cylinder 40. Each fixing hole 402 connects to the inner cavity 401 of the rotating shaft cylinder 40. In this embodiment, the end of the cylinder 42 near the hand-held head 44 is provided with two mutually spaced fixing holes 402, which are arranged along the axial direction of the cylinder 42 and both of them connect to the inner cavity of the cylinder 42. A receiving groove 404 is provided on the side of the cylinder 42 away from the fixing holes 402. The receiving groove 404 connects to the inner cavity 401 of the cylinder 42. The axis of the fixing holes 402 is located in the receiving groove 404, and the length direction of the receiving groove 404 is parallel to the axial direction of the cylinder 42. One end face of the rotating shaft cylinder 40 is provided with a wire harness hole 442 along its axial direction, and the wire harness hole 442 connects to the inner cavity 401 of the rotating shaft cylinder 40; specifically, the wire harness hole 442 is located in the middle of the end face of the handheld head 44 away from the cylinder body 42. The end face of the handheld head 44 away from the cylinder body 42 is provided with a snap-fit ​​groove 444, which connects to the wire harness hole 442 and is located around the wire harness hole 442. The bottom surface of the handheld head 44 is provided with a second connecting hole 445.

[0031] like Figures 4-8As shown, the cable management base 52 includes a connecting portion 521 and a cable clamping portion 523. The cable clamping portion 523 is connected to the connecting portion 521, and the connecting portion 521 is connected to the inner wall of the rotating shaft cylinder 40. The cable tie 54 is connected to the cable clamping portion 523. The cable management base 52 is located in the inner cavity 401 of the rotating shaft cylinder 40. The connecting portion 521 and the rotating shaft cylinder 40 can be connected by, but not limited to, screws, clamps, or adhesives. In this embodiment, the cable management structure 50 also includes a locking fastener 56, which is used to lock the connecting portion 521 to the rotating shaft cylinder 40. The connecting portion 521 is provided with a locking hole 524, and the locking fastener 56 passes through the locking hole 524 and is locked into one of the fixing holes 402. Since the multiple fixing holes 402 on the rotating cylinder 40 are arranged along the axial direction of the rotating cylinder 40, the locking fastener 56 can selectively lock the cable management seat 52 into one of the fixing holes 402. By adjusting the different positions of the cable management seat 52 in the axial direction of the rotating cylinder 40, a better position can be selected to position the wire harness 60, achieving a better cable management effect. In this embodiment, the locking hole 524 is located at the end of the connecting portion 521 away from the wire clamping portion 523. In other embodiments, the locking hole 524 may also be located at the end of the connecting portion 521 closer to the wire clamping portion 523. In this embodiment, the cable tie 54 is a cable tie.

[0032] In this embodiment, the connecting part 521 is a strip plate, the wire-clamping part 523 is a wire-clamping block located at one end of the strip plate, the locking hole 524 is located at the end of the strip plate away from the wire-clamping block, the wire-clamping block is provided with a through groove 525, and the wire tie 54 passes through the through groove 525. Specifically, the length direction of the through groove 525 is perpendicular to the length direction of the connecting part 521, and the opposite ends of the through groove 525 respectively penetrate the opposite sides of the wire-clamping block. The cable management base 52 can be made of, but is not limited to, hard plastic, hard rubber, or hard metal in one piece.

[0033] In other embodiments, the length direction of the through groove 525 may be parallel to the length direction of the connecting portion 521, and the opposite ends of the through groove 525 respectively penetrate the opposite end faces of the wire-clamping block. In other embodiments, the length direction of the through groove 525 is inclined to the length direction of the connecting portion 521, and the opposite ends of the through groove 525 respectively penetrate the outer peripheral surface of the wire-clamping block. In other embodiments, the connecting portion 521 may be omitted, and the wire-clamping portion 523 may be directly fixedly connected to the inner cavity wall of the rotating shaft cylinder 40.

[0034] In this embodiment, the wire-locking part 523 is a rectangular wire-locking block; in other embodiments, the wire-locking part 523 may be, but is not limited to, a circular wire-locking block, a polygonal wire-locking block, an elliptical wire-locking block, etc., and the two opposite ends of the through groove 525 respectively penetrate the outer peripheral surface of the wire-locking block.

[0035] like Figures 4-6As shown, the first rotating shaft 72 has a first rotating section 721 and a first positioning section 723 located at its opposite ends. The first rotating section 721 is rotatably inserted into the first rotating hole 220 of the rotating frame 20, and the first positioning section 723 is positioned in the first positioning hole 421 of the rotating shaft cylinder 40. Specifically, the first rotating shaft 72 includes a connecting flange 722 and a first connecting shaft 724. The first connecting shaft 724 is fixedly inserted into the inner cavity of the connecting flange 722. The opposite ends of the first rotating shaft 72 extend out of the opposite sides of the connecting flange 722 to form the first rotating section 721 and the first positioning section 723, respectively. A plurality of through holes 725 are provided around the connecting flange 722, and the plurality of through holes 725 surround the circumference of the connecting flange 722. The second rotating shaft 74 has a second rotating section 741 and a second positioning section 743 located at opposite ends. The second rotating section 741 is rotatably inserted into the second rotating hole 240 of the rotating frame 20, and the second positioning section 743 is positioned in the second positioning hole 423 of the rotating shaft cylinder 40. The second rotating shaft 74 also has an isolation cam 745 located between the second rotating section 741 and the second positioning section 743. The outer diameter of the isolation cam 745 is larger than the outer diameter of the second rotating section 741 and the outer diameter of the second positioning section 743.

[0036] Optionally, the base 100 further includes a first bearing 82 and a second bearing 84. The first bearing 82 is positioned in a first rotating hole 220, and the second bearing 84 is positioned in a second rotating hole 240. The first bearing 82 has a first inner cavity 820, and the second bearing 84 has a second inner cavity 840. The cable management structure 50 also includes a cable harness connector seat 55, which is connected to the cable harness hole 442 of the rotating shaft cylinder 40. One end of the cable harness 60 is connected to the cable harness connector seat 55. The cable harness connector seat 55 includes a plug 551, a wiring portion 552, and a mounting portion 554. The plug 551 is disposed on the mounting portion 554, and the wiring portion 552 is connected to the end of the plug 551 facing away from the mounting portion 554. The mounting portion 554 is provided with a mounting hole 5542.

[0037] like Figures 1-6 and Figures 9-11As shown, when assembling the base 100, the first bearing 82 is positioned in the first rotating hole 220 of the first rotating plate 22, the first connecting shaft 724 of the first rotating shaft 72 is fixedly inserted into the first inner cavity 820 of the first bearing 82, the connecting flange 722 is located in the clearance groove 26 of the rotating frame 20, the end of the cylinder 42 of the rotating shaft cylinder 40 away from the hand-held head 44 is inserted into the clearance groove 26, the first positioning section 723 is positioned in the first positioning hole 421 of the rotating shaft cylinder 40, and multiple fasteners (such as screws) pass through multiple through holes 725 of the connecting flange 722 and are locked to the cylinder. Multiple first connecting holes 426 of body 42; the second rotating section 741 of the second rotating shaft 74 is positioned in the second inner cavity 840 of the second bearing 84 until the second bearing 84 abuts against the isolation cam 745; the second rotating shaft 74 and the second bearing 84 are inserted from the outside of the rotating frame 20 into the second rotating hole 240 of the second rotating plate 24 until the second positioning section 743 of the second rotating shaft 74 is inserted into the second positioning hole 423 of the cylinder 42, and the second bearing 84 is positioned in the second rotating hole 240 of the second rotating plate 24, and the first rotating shaft 72 and the second rotating shaft 74 are coaxial. Insert the wire tie 54 into the through slot 525 of the wire holder 52. Place the wire holder 52 and the wire tie 54 from the receiving slot 404 of the cylinder 42 into the inner cavity 401, so that the locking hole 524 of the wire holder 52 is aligned with one of the fixing holes 402. The locking fastener 56 passes through the locking hole 524 and locks itself into the fixing hole 402, thereby positioning the wire holder 52 and the wire tie 54 on the inner wall of the rotating cylinder 40. Electrically connect one end of the wire harness 60. The wiring portion 552, connected to the wire harness connector 55, allows the end of the wire harness 60 away from the wire harness connector 55 to pass through the wire harness hole 442 and the inner cavity 401 of the rotating shaft cylinder 40 until the wiring portion 552 is positioned in the wire harness hole 442. The mounting portion 554 is positioned in the snap-fit ​​groove 444, so that the mounting hole 5542 is aligned with the second connecting hole 445. A locking fastener (such as a screw) passes through the mounting hole 5542 and locks it into the second connecting hole 445. The wire tie 54 positions the wire harness 60 in the wire management seat 52, thus fixing the wire harness 60 to the inner cavity wall of the rotating shaft cylinder 40. The rotating shafts 253 on the two end plates 25 of the rotating frame 20 are respectively inserted into the first shaft hole 323 of the first support member 32 and the second shaft hole 343 of the second support member 34.

[0038] The base 100 is assembled into the flight simulator. When the flight simulator is working, the rotating cylinder 40 rotates relative to the rotating frame 20, and the cylinder 42 swings within the clearance groove 26. The wiring harness 60 rotates with the rotating cylinder 40 relative to the rotating frame 20. The rotating frame 20 and the rotating cylinder 40 rotate together relative to the support frame 30, and the wiring harness 60 rotates with the rotating cylinder 40 relative to the support frame 30. The wiring harness 60 will not move relative to the rotating cylinder 40 to avoid loosening or shifting of the wiring harness 60. This prevents poor wiring contact, signal fluctuations or interruptions, and ensures the control precision and display accuracy of the flight simulator. Secondly, the wiring harness 60 will not rub against other components, avoiding wear on the insulation layer of the wiring harness 60 and reducing the risk of short circuits or circuit failures. The positioning of the wiring harness 60 improves the overall reliability of the flight simulator system, enhances the performance of the flight simulator, and improves the user experience. The base 100 has a simple structure, is easy to install, and has low processing costs.

[0039] like Figure 12 As shown, this application also provides a flight simulator 200, which includes a base 100, a base plate 210, a circuit board 230, a first drive assembly 250, and a second drive assembly 260. The base 100 includes a rotating frame 20, a support frame 30, a rotating shaft cylinder 40, and a cable management structure 50. The support frame 30 includes a first support member 32 and a second support member 34, which are disposed on the base plate 210 at a relative interval. The circuit board 230 is disposed on the base plate 210 and electrically connected to the first drive assembly 260. The driving components of the moving component 250 and the second driving component 260 are rotatably connected to the first support 32 and the second support 34 at opposite ends of the rotating frame 20 of the base 100. The first driving component 250 is disposed between the support frame 30 and the rotating frame 20, and the second driving component 260 is disposed between the rotating frame 20 and the rotating shaft cylinder 40. The driving component works to drive the first driving component 250 to drive the rotating frame 20 to rotate relative to the support frame 30, and the second driving component 260 to drive the rotating shaft cylinder 40 to rotate relative to the rotating frame 20.

[0040] The wiring harness inside the rotating cylinder 40 of the flight simulator 200 of this application is positioned by a wiring management structure. During the operation of the flight simulator 200, the wiring harness is positioned relative to the rotating cylinder 40, preventing the wiring harness from becoming loose or shifting; preventing poor wiring contact, preventing signal fluctuations or interruptions, and ensuring the control precision and display accuracy of the flight simulator 200; even in high vibration environments, the wiring harness will not rub against other components, avoiding wear on the wiring harness insulation layer and reducing the risk of short circuits or circuit failures; ensuring the overall system reliability of the flight simulator 200, and improving the performance and user experience of the flight simulator 200.

[0041] The embodiments of this utility model have been described in detail above. Specific examples have been used in this article to illustrate the principle and implementation of this utility model. The description of the above embodiments is only for the purpose of helping to understand the method and core idea of ​​this utility model.

Claims

1. A wire routing structure for positioning a wire bundle in an inner cavity of a rotating shaft cylinder, characterized by, The thread arrangement structure includes: A cable management seat, wherein the cable management seat is positioned on the inner wall of the rotating shaft cylinder; and A wire tie is connected to the wire management base and is used to position the wire bundle on the wire management base.

2. The wire management structure of claim 1, wherein, The cable management seat includes a connecting part and a cable clamping part. The cable clamping part is connected to the connecting part, and the connecting part is connected to the inner wall of the rotating shaft cylinder. The cable tie is connected to the cable clamping part.

3. The wire management structure of claim 2, wherein, The connecting part is provided with a locking hole, and the inner wall of the rotating shaft cylinder is provided with at least two fixing holes, which are arranged along the axial direction of the rotating shaft cylinder; the cable management structure also includes a locking member, which passes through the locking hole and is locked in one of the fixing holes.

4. The wire management structure of claim 3, wherein, The connecting part is a strip plate, the wire clamping part is a wire clamping block located at one end of the strip plate, and the locking hole is located at the end of the strip plate away from the wire clamping block; the wire clamping block is provided with a through groove, and the wire tie is inserted through the through groove.

5. The wire management structure of claim 3, wherein, One end face of the rotating shaft cylinder is provided with a wire harness hole along its axial direction. The wire harness hole communicates with the inner cavity of the rotating shaft cylinder. The wire management structure also includes a wire harness connector seat, which is connected to the wire harness hole, and one end of the wire harness is connected to the wire harness connector seat.

6. A susceptor, characterized by, The base includes a rotating frame, a rotating cylinder, and a cable management structure as described in any one of claims 1-5. One end of the rotating cylinder is rotatably connected to the rotating frame, the cable management seat of the cable management structure is positioned on the inner wall of the rotating cylinder, and the cable tie is connected to the cable management seat.

7. The susceptor of claim 6, wherein The rotating frame includes a first rotating plate, a second rotating plate, a first rotating shaft, and a second rotating shaft. The first rotating plate and the second rotating plate are directly opposite each other with a gap. There is a clearance groove between the first rotating plate and the second rotating plate. One end of the rotating shaft cylinder is located in the clearance groove. The rotating shaft cylinder is connected to the first rotating plate through the first rotating shaft, and the rotating shaft cylinder is connected to the second rotating plate through the second rotating shaft. The first rotating shaft and the second rotating shaft are coaxial.

8. The base of claim 7, wherein, The first rotating plate has a first rotating hole, and the second rotating plate has a second rotating hole. The first rotating hole and the second rotating hole are coaxial. The rotating shaft cylinder has a first positioning hole on the side facing the first rotating plate and a second positioning hole on the side facing the second rotating plate. The first positioning hole and the second positioning hole are coaxial. The opposite ends of the first rotating shaft are respectively connected to the first rotating hole and the first positioning hole, and the opposite ends of the second rotating shaft are respectively connected to the second rotating hole and the second positioning hole.

9. The susceptor of claim 8, wherein, The base further includes a first bearing and a second bearing, the first bearing being positioned in the first rotating hole and the second bearing being positioned in the second rotating hole; the first rotating shaft has a first rotating section and a first positioning section located at opposite ends thereof, the first rotating section being inserted into the first inner cavity of the first bearing and the first positioning section being positioned in the first positioning hole; the second rotating shaft has a second rotating section and a second positioning section located at opposite ends thereof, the second rotating section being inserted into the second inner cavity of the second bearing and the second positioning section being positioned in the second positioning hole.

10. A flight simulator, characterized by The flight simulator comprises a base as claimed in any one of claims 6-9.

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