A cable movement and stroke scaling system

CN120473906BActive Publication Date: 2026-10-09SHENYANG SHENFEI WIRE HARNESS TECH CO LTD
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Patent Information

Application Number
CN202510578309.7
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2025-05-07
Publication Date
2026-10-09
Estimated Expiration
2045-05-07

AI Technical Summary

Technical Problem

[0003]针对现有产品无法满足大角度、偏转轴、大行程的运动需求,本发明的目的在于提供一种电缆运动及行程缩放系统

Benefits of technology

[0016] This invention has the advantages of being able to meet the requirements of large angles, multi-curvature composite motion, scalable motion stroke, including a large number of cables, and being able to be arranged off-center from the motion area. It solves the shortcomings of existing products and provides a brand-new solution for the electrical connection between moving parts.

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Abstract

The present application belongs to the technical field of aircraft EWIS product design, in particular to a cable movement and stroke scaling system, which comprises a support structure part, a movement scaling driving part and a movement cable part, the support structure part comprises a side wall plate assembly A, a side wall plate assembly B, a bottom plate and a top support assembly, and the support structure is used for supporting and fixing the scaling system; the movement scaling driving part comprises a push rod assembly transmission scaling assembly, and is used for transmitting movement, changing the movement trajectory and direction, and amplifying the movement stroke, so that the movement cable assembly can move along the specified direction, and the movement allowance meets the movement demand; the movement cable part comprises a plurality of movement cable assemblies, which are used for providing the required movement allowance and maintaining the optical and electrical signal connection with the docking equipment. The present application has the advantages of being able to meet large-angle, multi-curvature composite movement, scalable movement stroke, containing a large number of cables, being able to be arranged away from the movement area and the like.
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Description

Technical Field

[0001] This invention belongs to the field of aircraft EWIS (Electrical Wiring Interconnection System) product design technology, specifically a cable movement and stroke scaling system. Background Technology

[0002] Optical and electrical components in moving parts of an aircraft need to maintain optical and electrical signal connections with other parts to ensure safe operation. In specific areas, such as flaps, landing gear, folding wings, and tiltrotors, simple cables cannot meet the motion requirements; therefore, products with corresponding functions are needed to achieve both motion and optical / electrical connectivity. Existing products typically achieve this through helicals or motion guides; however, these products cannot meet the motion requirements of large angles, deflection axes, and long strokes. Therefore, a new motion system needs to be invented to meet these motion requirements. Summary of the Invention

[0003] To address the limitations of existing products in meeting the demands for large-angle, deflection-axis, and long-stroke motion, this invention aims to provide a cable motion and stroke scaling system. This system enables large-angle, deflection-axis, and long-stroke motion, and can integrate various cables such as low-frequency conductors, coaxial cables, and optical fibers for motion. It features the ability to accommodate a large number of cables, shorten or amplify the motion stroke, and deviate from the main motion area, while maintaining continuous and uninterrupted signal transmission.

[0004] The objective of this invention is achieved through the following technical solution:

[0005] This invention includes a support structure, a motion scaling drive, and a motion cable. The support structure includes side panel assembly A, side panel assembly B, a bottom plate, a top support assembly, and a cable bracket. The bottom plate is a fixed component. Side panel assembly A and side panel assembly B are mounted opposite each other on the bottom plate. The top support assembly is fixed to the top of side panel assembly A and side panel assembly B. The cable bracket is fixedly connected to the bottom plate. The motion scaling drive includes a push rod assembly, a transmission scaling assembly, and an isolation transmission component. The transmission scaling assembly includes a transmission rack, a gear transmission assembly, and a toothed worm gear. The transmission rack is slidably mounted on side panel assembly A. One end of the push rod assembly is connected to a moving part on the aircraft, and the other end is connected to the transmission rack. The toothed worm gear is rotatably mounted on... On the top support assembly, the isolation transmission component is threadedly connected to the toothed worm gear, and the transmission rack is connected to the toothed worm gear through a gear transmission assembly. The motion cable section includes multiple bundles of motion cable assemblies, each bundle of which passes through the isolation transmission component. One end of each bundle of motion cable assemblies is fixed to a cable bracket, and the other end of each bundle of motion cable assemblies is connected to a moving part on the aircraft. Under the movement of the moving part, the push rod assembly drives the transmission rack to slide back and forth. The transmission rack converts the sliding motion into the rotational motion of the toothed worm gear through the gear transmission assembly. The lifting and lowering of the isolation transmission component is achieved through the helical pair between the toothed worm gear and the isolation transmission component. During the movement of the moving part, each bundle of motion cable assemblies provides the required movement margin and is limited by the lifting and lowering of the isolation transmission component.

[0006] Wherein: there are two toothed worm gears, namely toothed worm gear A and toothed worm gear B. Toothed worm gear A and toothed worm gear B have the same structure, each having a beveled tooth, a smooth shaft, and a helical shaft. The smooth shafts of toothed worm gear A and toothed worm gear B are rotatably connected to the top support assembly. The beveled tooth is located at the bottom of toothed worm gear A and toothed worm gear B. The beveled tooth of toothed worm gear A and toothed worm gear B are respectively engaged with the gear transmission assembly for transmission. The isolation transmission component is threadedly connected to the helical shaft of toothed worm gear A and toothed worm gear B respectively.

[0007] The thread of the helical rod of the toothed worm A is set counterclockwise, and the thread of the helical rod of the toothed worm B is set clockwise. The number of teeth on the bevel teeth of the toothed worm A and the toothed worm B is the same.

[0008] The gear transmission assembly includes a compound gear and a transmission rod. The two ends of the transmission rod are rotatably connected to side wall plate assembly A and side wall plate assembly B, respectively. The compound gear is mounted on the transmission rod and moves in conjunction with the transmission rod. One side of the compound gear is a straight tooth that meshes with a transmission rack, and the other side of the compound gear is a bevel tooth that meshes with a toothed worm gear.

[0009] There are two toothed worm gears, namely toothed worm gear A and toothed worm gear B. The compound gear is located at one end of the transmission rod. The bevel gear meshes with toothed worm gear A for transmission. A bevel gear is installed at the other end of the transmission rod. The bevel gear is linked to the transmission rod and meshes with toothed worm gear B for transmission. The number of teeth of the bevel gear is the same as the number of teeth of the bevel gear on the other side of the compound gear.

[0010] The bevel teeth on the other side of the compound gear mesh with the bevel teeth at the bottom of the toothed worm gear. The number of spur teeth and bevel teeth of the compound gear is set according to a gear ratio of 1:6, and the number of bevel teeth and bevel teeth of the toothed worm gear is set according to a gear ratio of 3:1. The toothed worm gear has a helical rod that is threadedly connected to the isolation transmission component. The pitch of the helical rod is 3.5mm, thereby amplifying the motion stroke of the isolation transmission component compared to the push rod assembly.

[0011] The side wall panel assembly A includes a side wall panel A, a mounting base A, and a side sliding groove. The side wall panel A has a bottom mounting surface for assembling with the bottom plate. The outer side of the side wall panel A is provided with the mounting base A, and the side wall panel A is fixed to the bottom plate by the mounting base A. The inner side of the side wall panel A is provided with a side sliding groove, and the transmission spur rack can be slidably accommodated in the side sliding groove. The lower middle part of the side wall panel A has a mounting hole A, and the mounting hole A has a bushing A for connecting with the gear transmission assembly. The middle and top parts of the side wall panel A both have mounting holes B. The mounting hole B in the middle part is fixedly connected to the side wall support assembly B, and the toothed worm gear is rotatably connected to the side wall support assembly B. The mounting hole B in the top part is fixedly connected to the top bracket assembly.

[0012] The side wall panel assembly B includes a side wall panel B and a mounting base B. The side wall panel B has a bottom mounting surface for assembling with a bottom plate. The mounting base B is provided on the outer side of the side wall panel B, and the side wall panel B is fixed to the bottom plate by the mounting base B. A mounting hole C is provided in the lower middle part of the side wall panel B, and a bushing C for connecting with a gear transmission assembly is provided in the mounting hole C. Mounting holes D are provided in the middle and top of the side wall panel B. The mounting hole D in the middle is fixedly connected to a side wall support assembly A, and the toothed worm gear is rotatably connected to the side wall support assembly A. The mounting hole D in the top is fixedly connected to a top support assembly.

[0013] The push rod assembly includes a push rod, with bushings D at both ends. Bushing D at one end of the push rod is connected to a moving part on the aircraft, and bushing D at the other end of the push rod is connected to a transmission rack via an adapter. The adapter has a double-ear connector with two pairs of orthogonal lugs on both sides. Bushing E is provided on each pair of lugs on one side. Bushing E is hinged to bushing D at the other end of the push rod via a cotter pin, nut, washer, and bolt. A connecting seat is provided at one end of the transmission rack, with bushing B on the connecting seat. Bushing F is provided on each pair of lugs on the other side. Bushing F is hinged to bushing B on the connecting seat via a cotter pin, nut, washer, and bolt.

[0014] The top support assembly includes a top support, the two ends of which are fixedly connected to the tops of side wall panel assembly A and side wall panel assembly B, respectively. The top support is provided with a bushing G for rotatably connecting with the toothed worm gear. The isolation transmission component is provided with through holes and helical holes, the helical holes for threaded connection with the toothed worm gear, and the number of through holes is the same as the bundle amount of the motion cable assembly, corresponding one-to-one. Each bundle of the motion cable assembly passes through the corresponding through hole.

[0015] The advantages and positive effects of this invention are as follows:

[0016] This invention has the advantages of being able to meet the requirements of large angles, multi-curvature composite motion, scalable motion stroke, including a large number of cables, and being able to be arranged off-center from the motion area. It solves the shortcomings of existing products and provides a brand-new solution for the electrical connection between moving parts. Attached Figure Description

[0017] Figure 1A This is one of the three-dimensional structural schematic diagrams of the present invention;

[0018] Figure 1B This is a second three-dimensional structural schematic diagram of the present invention;

[0019] Figure 1C This is the third three-dimensional structural schematic diagram of the present invention;

[0020] Figure 2 This is an exploded view of the present invention;

[0021] Figure 3 for Figure 2 Exploded view of the middle sidewall panel assembly A;

[0022] Figure 4 for Figure 2 Exploded view of the middle sidewall panel assembly B;

[0023] Figure 5 for Figure 2 Schematic diagram of the middle and bottom plates;

[0024] Figure 6 for Figure 2 Schematic diagram of the structure of the motion cable assembly;

[0025] Figure 7 for Figure 2 Exploded view of the push rod assembly;

[0026] Figure 8 for Figure 2 Exploded view of the transfer joint;

[0027] Figure 9 for Figure 2 Exploded view of the top support assembly;

[0028] Figure 10A for Figure 2 Schematic diagram of the structure of the intermediate isolation transmission component;

[0029] Figure 10B for Figure 2 Cross-sectional view of the internal structure of the intermediate isolation transmission component;

[0030] Figure 11A for Figure 2 Exploded view of the middle sidewall support assembly A;

[0031] Figure 11B for Figure 2 Exploded view of the middle sidewall support assembly B;

[0032] Figure 12 This is a three-dimensional structural schematic diagram of the transmission scaling component of the present invention;

[0033] Figure 13 for Figure 12 Exploded view of the compound gear, transmission rod, and bevel gear;

[0034] Figure 14 This is an exploded view of the push rod assembly, adapter, and transmission spur rack of the present invention;

[0035] Figure 15A This is one of the structural schematic diagrams of the composite gear of the present invention;

[0036] Figure 15B This is the second schematic diagram of the composite gear of the present invention;

[0037] Figure 16A This is one of the structural schematic diagrams of the bevel gear of the present invention;

[0038] Figure 16B This is the second schematic diagram of the bevel gear of the present invention;

[0039] Figure 17 This is a schematic diagram of the transmission rod of the present invention;

[0040] Figure 18 This is a schematic diagram of the structure of the present invention in its installed state;

[0041] Figure 19 This is a schematic diagram of the structure of the present invention in motion;

[0042] Wherein: 1 is side wall panel assembly A, 101 is side wall panel, 102 is bushing A, 103 is transmission spur rack, 104 is bushing B, 105 is mounting base A, 106 is side slide groove, 107 is mounting hole A, 108 is mounting hole B, and 109 is connecting base.

[0043] 2 is side wall panel assembly B, 201 is side wall panel, 202 is bushing C, 203 is mounting base B, 204 is mounting hole C, and 205 is mounting hole D;

[0044] 3 represents the bottom plate, and 301 represents the fastener mounting hole;

[0045] 4 is the motion cable assembly, 401 is the motion harness, 402 is the connector, and 403 is the tail accessory;

[0046] 5 is the push rod assembly, 501 is the push rod, and 502 is the bushing D;

[0047] 6 is an adapter, 601 is a double-ear adapter, 602 is bushing E, and 603 is bushing F;

[0048] 7 is the top support assembly, 701 is the top support, and 702 is the bushing G;

[0049] 8 is an isolation transmission component, 801 is a through hole, and 802 is a spiral hole;

[0050] 9 is the side wall support assembly A, 901 is the side wall short support, and 902 is the bushing H;

[0051] 10 is the side wall support assembly B, 1001 is the side wall long support, and 1002 is the bushing I;

[0052] 11 is toothed worm A, 12 is toothed worm B, 13 is flat key pin A, and 14 is flat key pin B;

[0053] 15 is a compound gear, 1501 is a spur gear, 1502 is a bevel gear, and 1503 is a keyway A;

[0054] 16 represents a bevel gear, and 1601 represents keyway B;

[0055] 17 is a cable support;

[0056] 18 is the transmission rod, and 1801 is the keyway C;

[0057] 19 is a clamp, 20 is a cotter pin, 21 is a nut, 22 is a washer, 23 is a bolt, 24 is a moving part, and 25 is a fixed part. Detailed Implementation

[0058] The invention will now be described in further detail with reference to the accompanying drawings.

[0059] like Figures 1A-1C and Figure 2 As shown, the present invention includes a support structure, a motion scaling drive, and a motion cable. The support structure supports and fixes the scaling system, allowing the scaling system to maintain its shape in different environments. The support structure includes a side panel assembly A1, a side panel assembly B2, a bottom plate 3, a top support assembly 7, and a cable bracket 17. The bottom plate 3 is a fixing part 25 fixed to the aircraft. The side panel assembly A1 and the side panel assembly B2 are mounted opposite each other on the bottom plate 3. The top support assembly 7 is fixed to the top of the side panel assembly A1 and the side panel assembly B2. The cable bracket 17 is fixed to the bottom plate 3. The motion scaling drive section is used to transmit motion, change the motion trajectory and direction, and amplify the motion stroke so that the motion cable assembly 4 can move along the specified direction and the motion margin meets the motion requirements. The motion scaling drive section includes a push rod assembly 5, a transmission scaling assembly and an isolation transmission component 8. The transmission scaling assembly includes a transmission rack 103, a gear transmission assembly and a toothed worm gear. The transmission rack 103 can be slidably mounted on the side wall panel assembly A1. One end of the push rod assembly 5 is connected to the moving part 24 on the aircraft, and the other end of the push rod assembly 5 is connected to the transmission rack 103. The toothed worm gear is rotatably mounted on the top bracket assembly 7. The isolation transmission component 8 is threadedly connected to the toothed worm gear. The transmission rack 103 is connected to the toothed worm gear through the gear transmission assembly. The motion cable section is used to provide the required motion margin and maintain the optical and electrical signal connection with the docking equipment; the motion cable section includes multiple motion cable assemblies 4, each of which is passed through an isolation transmission member 8, one end of each motion cable assembly 4 is fixed on a cable bracket 17, and the other end of each motion cable assembly 4 is connected to the moving part 24 on the aircraft.

[0060] like Figures 1A-1C and Figure 2 , Figure 3 , Figure 11BAs shown, the side wall panel assembly A1 in this embodiment includes a side wall panel A101, mounting bases A105, and a side sliding groove 106. The side wall panel A101 has a bottom mounting surface for assembling with the bottom plate 3. Three mounting bases A105 are provided on the bottom of the outer side of the side wall panel A101. The side wall panel A101 is fixed to the bottom plate 3 by the mounting bases A105. The inner side of the side wall panel A101 is provided with a side sliding groove 106. The transmission rack 103 is housed in the side sliding groove 106 and can slide along the side sliding groove under the drive of the push rod assembly 5. The groove 106 slides; the lower middle part of the side wall plate A101 is provided with a mounting hole A107, which is used to accommodate the bushing A102 connected to the gear transmission assembly and to provide the transmission rod 108 for fixing and rotational movement; the middle and top of the side wall plate A101 are each provided with two mounting holes B108, the two mounting holes B108 in the middle are fixedly connected to the side wall support assembly B10, the toothed worm gear is rotatably connected to the side wall support assembly B10, and the two mounting holes B108 in the top are fixedly connected to the top bracket assembly 7.

[0061] The side wall support assembly B10 of this embodiment includes a side wall long support 1001 and a bushing I1002. The side wall long support 1001 is L-shaped. The vertical side of the L-shape is installed at two mounting holes B108 in the middle of the side wall plate A101 by rivets and is located inside the side wall plate A101. The horizontal side of the L-shape is provided with a bushing I1002. The smooth rod on the toothed worm gear is rotatably connected to the bushing I1002.

[0062] like Figures 1A-1C and Figure 2 , Figure 4 , Figure 11A As shown, the side wall panel assembly B2 of this embodiment includes a side wall panel B201 and mounting bases B203. The side wall panel B201 has a bottom mounting surface for assembling with the bottom plate 3. Three mounting bases B203 are provided on the bottom of the outer side of the side wall panel B201. The side wall panel B201 is fixed to the bottom plate 3 by the mounting bases B203. A mounting hole C204 is provided in the lower middle part of the side wall panel B201. The mounting hole C204 is used to accommodate the bushing C202 connected to the gear transmission assembly and to provide the transmission rod 108 for fixing and rotational movement. Two mounting holes D205 are provided in the middle and top of the side wall panel B201. The two mounting holes D205 in the middle are fixed to the side wall support assembly A9. The toothed worm gear is rotatably connected to the side wall support assembly A9. The two mounting holes D205 in the top are fixed to the top bracket assembly 7.

[0063] The side wall support assembly A9 of this embodiment includes a side wall short support 901 and a bushing H902. The side wall short support 901 is L-shaped. The vertical side of the L-shape is installed at two mounting holes D205 in the middle of the side wall plate B201 by rivets and is located inside the side wall plate B201. The horizontal side of the L-shape is provided with a bushing H902. The smooth rod on the toothed worm gear is rotatably connected to the bushing H902.

[0064] like Figures 1A-1C and Figure 2 , Figure 5 As shown, the bottom plate 3 in this embodiment is a rectangular plate with fastener mounting holes 301 on its outer perimeter for mounting to the side wall plates A101 and B201 and the cable bracket 17. It is designed for lightweight construction and also prevents liquid accumulation. The cable bracket 17 is fixed to one end of the bottom plate 3 by rivets, and the cable bracket 17 has clamps 19 that correspond one-to-one with the bundle amount of the motion cable assembly 4.

[0065] like Figures 1A-1C and Figure 2 , Figure 7 , Figure 8 , Figure 14 As shown, the push rod assembly 5 of this embodiment includes a push rod 501. Both ends of the push rod 501 are provided with bushings D502. One bushing D502 of the push rod 502 is connected to the moving part 24 on the aircraft, and moves under the drive of the moving part 24, transmitting the motion to the transmission rack 103. The other bushing D502 of the push rod 501 is connected to the transmission rack 103 via an adapter 6. The adapter 6 of this embodiment has a double-ear connector 601. The double-ear connector 601 has two pairs of orthogonal lugs on each side, meaning that a pair of lugs is provided on each side of the double-ear connector 601. The axial center line of the bushing E602 on one pair of lugs is vertical. On the other side, the axial centerline of the bushing F603 on the pair of lugs is horizontal; each of the pair of lugs on one side is provided with a bushing E602, which is hinged to the bushing D502 at the other end of the push rod 501 via a cotter pin 20, nut 21, washer 22, and bolt 23; one end of the transmission rack 103 is provided with a connecting seat 109, on which a bushing B104 is provided; on the other side, each of the pair of lugs is provided with a bushing F603, which is hinged to the bushing B104 on the connecting seat 109 via a cotter pin 20, nut 21, washer 22, and bolt 23. Through this configuration, the transmission rack 103 slides along the side groove 106 under the drive of the push rod assembly 5, achieving a nonlinear composite trajectory relative motion between the push rod assembly 5 and the transmission rack 103 to meet the motion requirements of the moving part 24.

[0066] like Figures 1A-1C and Figure 2 , Figure 3 , Figure 4 , Figure 9 As shown, the top support assembly 7 in this embodiment includes a top support 701. One end of the top support 701 is fixedly connected to two mounting holes B108 on the top of the side wall plate A101, and the other end of the top support 701 is fixedly connected to two mounting holes D205 on the top of the side wall plate B201. Bushings G702 for rotatably connecting with the toothed worm gear A11 and the toothed worm gear B12 are respectively provided on the top support 701 near both ends.

[0067] like Figures 1A-1C and Figure 2 , Figure 3 , Figure 4 , Figure 10A , Figure 10B As shown, the isolation transmission component 8 in this embodiment is a cuboid. Through holes 801 and spiral holes 802 are respectively provided on the isolation transmission component 8. The number of through holes 801 corresponds one-to-one with the number of bundles of motion cable assemblies 4. Each bundle of motion cable assemblies 4 passes through the corresponding through hole 801. In this embodiment, there are three through holes 801, used for isolation between different bundles of the motion cable assemblies 4 and to drive the motion cable assemblies 4 to move. Spiral holes 802 are provided on both sides of the three through holes 801. The spiral holes 802 are used for threaded connection with the spiral rods on the toothed worm gear A11 and toothed worm gear B12, and move up and down along the spiral rods under the rotational motion of the toothed worm gear A11 and toothed worm gear B12.

[0068] like Figures 1A-1C and Figure 2 , Figure 6 , Figure 10A , Figure 10B As shown, the motion cable assembly 4 in this embodiment is designed with a three-wire harness to meet the triple redundancy requirements of the aircraft system. The motion cable assembly 4 is existing technology and includes a motion harness 401, a connector 402, and a tail accessory 403. Both ends of the motion harness 401 are connected to the tail accessory 403, and a connector 402 is installed on each end of the tail accessory 403. One end of the motion cable assembly 4 is fixed to the moving part 24 of the aircraft and moves with the moving part 24. The other end of the motion cable assembly 4 passes through the through hole 801 on the isolation transmission component 8 and is then fixed to the cable bracket 17 by a clamp 19.

[0069] like Figures 1A-1C and Figure 2 , Figure 3 , Figure 4 , Figure 9 , Figure 10A , Figure 10B , Figure 11A , Figure 11BAs shown, this embodiment has two toothed worm gears, namely toothed worm gear A11 and toothed worm gear B12. Toothed worm gear A11 and toothed worm gear B12 have the same structure, both having a beveled tooth head, a smooth shaft, and a helical shaft. Toothed worm gear A11 has two smooth shafts, located at the top and bottom respectively, with a helical shaft between the two smooth shafts. The smooth shaft at the top of toothed worm gear A11 is installed in a bushing G702 of the top bracket 701, and the smooth shaft at the bottom of toothed worm gear A11 is installed in a bushing I100 on the side wall long support 1001. In section 2, the toothed worm gear A11 achieves both fixed and rotational movement. The toothed worm gear B12 has two smooth rods, located at the top and bottom respectively, with a helical rod between them. The smooth rod at the top of the toothed worm gear B12 is installed in another bushing G702 of the top support 701, and the smooth rod at the bottom of the toothed worm gear B12 is installed in bushing H902 on the side wall short support 901, thus achieving both fixed and rotational movement of the toothed worm gear B12. The conical teeth of both toothed worm gears A11 and B12 are located below the bottom smooth rod. The thread of the helical rod of toothed worm gear A11 is counterclockwise, while the thread of the helical rod of toothed worm gear B12 is clockwise. The conical teeth of both toothed worm gears A11 and B12 have the same number of teeth, achieving synchronous movement.

[0070] like Figures 1A-1C and Figure 2 , Figure 3 , Figure 4 , Figure 12 , Figure 13 , Figure 15A , Figure 15B , Figure 16A , Figure 16B , Figure 17As shown, the gear transmission assembly of this embodiment includes a compound gear 15, a transmission rod 18, and a bevel gear 16. One end of the transmission rod 18 is installed in a bushing A102 on the side wall plate A101, and the other end of the transmission rod 18 is installed in a bushing C202 on the side wall plate B201, thereby enabling the transmission rod 18 to rotate relative to the side wall plates A101 and B201. The compound gear 15 is connected to one end of the transmission rod 18 through a flat key pin A13, and the bevel gear 16 is connected to the other end of the transmission rod 18 through a flat key pin B14. Both the compound gear 15 and the bevel gear 16 are linked with the transmission rod 18 and lock the axial movement trend, thereby realizing the synchronous movement of the compound gear 15 and the bevel gear 16 and converting the linear motion of the transmission spur rack 103 into rotational motion. In this embodiment, both ends of the transmission rod 18 are provided with keyways C1801 to accommodate the flat key pins A13 and B14. Stepped sections are provided at both ends of the transmission rod 18 to ensure that the compound gear 15 and bevel gear 16 are maintained in the correct positions. One side of the compound gear 15 in this embodiment has a spur tooth 1501 that meshes with the transmission rack 103, and the other side has a bevel tooth 1502 that meshes with the bottom bevel tooth of the toothed worm A11. The bevel teeth cooperate with the toothed worm A11 to change the motion angle and transmit motion. The number of spur teeth 1501 and bevel teeth 1502 is set according to a gear ratio of 1:6, and the number of bevel teeth 1502 and the bevel tooth of the toothed worm A11 is set according to a gear ratio of 3:1. The screw pitch of the toothed worm A11 is 3.5mm. Through the above arrangement, the motion stroke of the isolation transmission component 8 is amplified compared to the push rod assembly 5, thereby obtaining the required motion margin. The compound gear 15 has a keyway A1503, which engages with a flat key pin A13 to lock the transmission rod 18. The bevel gear 16 meshes with the bottom bevel teeth of the worm gear B12, changing the motion angle and transmitting motion. The bevel gear 16 has a keyway B1601, which engages with a flat key pin B14 to lock the transmission rod 18. The number of teeth on the bevel gear 16 is the same as the number of teeth on the other side of the compound gear 15 (the bevel teeth 1502) to maintain synchronous movement.

[0071] The working principle of this invention is as follows:

[0072] like Figure 18As shown, the bottom plate 3 is fixed to the fixed part 25 on the aircraft, and the other end of each bundle of motion cable assemblies 4 is connected to the moving part 24 on the aircraft. When the moving part 24 moves, the push rod assembly 5 drives the transmission rack 103 to slide back and forth under the action of the moving part 24. The transmission rack 103 meshes with the spur teeth 1501 in the compound gear 15, the bevel teeth 1502 in the compound gear 15 mesh with the bevel teeth of the toothed worm A11, and the bevel gear 16 meshes with the bevel teeth of the toothed worm B12, converting the linear motion of the transmission rack 103 into the rotational motion of the toothed worm A11 and the toothed worm B12. The lifting and lowering of the isolation transmission component 8 is achieved through the helical pairs between the toothed worm A11 and the toothed worm B12 and the isolation transmission component 8, respectively. During the movement of the moving part 24, each bundle of motion cable assemblies 4 provides the required motion margin and is limited by the lifting and lowering of the isolation transmission component 8.

[0073] Although the embodiments of the present invention have been described in detail above with reference to the accompanying drawings, the present invention is not limited to the above embodiments. For those skilled in the art, various changes, modifications, substitutions and variations can be made to the content and embodiments of the present invention without departing from the principles and spirit of the present invention. The scope of the present invention is defined by the appended solutions, claims and their equivalents.

Claims

1. A cable motion and stroke scaling system, characterized in that: The system includes a support structure, a motion scaling drive, and a motion cable. The support structure includes a side wall panel assembly A (1), a side wall panel assembly B (2), a bottom plate (3), a top support assembly (7), and a cable bracket (17). The bottom plate (3) is a fixing component. The side wall panel assembly A (1) and the side wall panel assembly B (2) are mounted opposite each other on the bottom plate (3). The top support assembly (7) is fixed to the top of the side wall panel assembly A (1) and the side wall panel assembly B (2). The bottom plate (3) is fixed with... A cable bracket (17) is connected; the motion scaling drive part includes a push rod assembly (5), a transmission scaling assembly and an isolation transmission component (8), the transmission scaling assembly includes a transmission rack (103), a gear transmission assembly and a toothed worm gear, the transmission rack (103) is slidably mounted on the side wall panel assembly A (1), one end of the push rod assembly (5) is connected to the moving part (24) on the aircraft, the other end of the push rod assembly (5) is connected to the transmission rack (103), and the toothed worm gear rotates... The device is mounted on the top support assembly (7). The isolation transmission component (8) is threadedly connected to the toothed worm gear. The transmission rack (103) is connected to the toothed worm gear through the gear transmission assembly. The motion cable part includes multiple bundles of motion cable assemblies (4). Each bundle of motion cable assemblies (4) passes through the isolation transmission component (8). One end of each bundle of motion cable assemblies (4) is fixed on the cable bracket (17). The other end of each bundle of motion cable assemblies (4) is connected to the moving part (24) on the aircraft. The push rod assembly (5) drives the transmission rack (103) to slide back and forth under the action of the moving part (24). The transmission rack (103) converts the sliding motion into the rotational motion of the toothed worm gear through the gear transmission assembly. The lifting and lowering of the isolation transmission component (8) is realized through the helical pair between the toothed worm gear and the isolation transmission component (8). During the movement of the moving part (24), each bundle of motion cable assemblies (4) provides the required motion margin and is limited by the lifting and lowering of the isolation transmission component (8).

2. The cable movement and stroke scaling system according to claim 1, characterized in that: There are two toothed worms, namely toothed worm A (11) and toothed worm B (12). Toothed worm A (11) and toothed worm B (12) have the same structure, both having a beveled tooth, a smooth rod and a helical rod. The smooth rod of toothed worm A (11) and toothed worm B (12) is rotatably connected to the top support assembly (7). The beveled tooth is located at the bottom of toothed worm A (11) and toothed worm B (12). The beveled tooth of toothed worm A (11) and toothed worm B (12) meshes with the gear transmission assembly. The isolation transmission component (8) is threadedly connected to the helical rod of toothed worm A (11) and toothed worm B (12).

3. The cable movement and stroke scaling system according to claim 2, characterized in that: The thread of the helical rod of the toothed worm A (11) is set counterclockwise, and the thread of the helical rod of the toothed worm B (12) is set clockwise. The number of teeth on the bevel teeth of the toothed worm A (11) and the toothed worm B (12) is the same.

4. The cable movement and stroke scaling system according to claim 1, characterized in that: The gear transmission assembly includes a compound gear (15) and a transmission rod (18). The two ends of the transmission rod (18) are rotatably connected to the side wall plate assembly A (1) and the side wall plate assembly B (2), respectively. The compound gear (15) is mounted on the transmission rod (18) and moves in conjunction with the transmission rod (18). One side of the compound gear (15) is a straight tooth (1501) that meshes with the transmission rack (103), and the other side of the compound gear (15) is a bevel tooth (1502) that meshes with the toothed worm gear.

5. The cable movement and stroke scaling system according to claim 4, characterized in that: There are two toothed worms, namely toothed worm A (11) and toothed worm B (12). The compound gear (15) is located at one end of the transmission rod (18). The bevel gear (1502) meshes with the toothed worm A (11) for transmission. A bevel gear (16) is installed at the other end of the transmission rod (18). The bevel gear (16) is connected to the transmission rod (18). The bevel gear (16) meshes with the toothed worm B (12) for transmission. The number of teeth of the bevel gear (16) is the same as the number of teeth of the bevel gear (1502) on the other side of the compound gear (15).

6. The cable movement and stroke scaling system according to claim 4, characterized in that: The bevel tooth (1502) on the other side of the compound gear (15) meshes with the bevel tooth at the bottom of the toothed worm gear. The number of straight teeth (1501) and bevel teeth (1502) of the compound gear (15) is set according to a gear ratio of 1:

6. The number of bevel teeth (1502) and the number of bevel teeth at the bottom of the toothed worm gear are set according to a gear ratio of 3:

1. The toothed worm gear has a helical rod that is threadedly connected to the isolation transmission component (8). The pitch of the helical rod is 3.5mm, thereby amplifying the motion stroke of the isolation transmission component (8) compared to the push rod assembly (5).

7. The cable movement and stroke scaling system according to claim 1, characterized in that: The side wall panel assembly A (1) includes a side wall panel A (101), a mounting base A (105), and a side sliding groove (106). The side wall panel A (101) has a bottom mounting surface for assembling with the bottom plate (3). The mounting base A (105) is provided on the outer side of the side wall panel A (101). The side wall panel A (101) is fixed to the bottom plate (3) by the mounting base A (105). The side wall panel A (101) has a side sliding groove (106) on its inner side. The transmission rack (103) can be slidably accommodated on the side wall panel. Inside the chute (106); the lower middle part of the side wall plate A (101) is provided with a mounting hole A (107), and a bushing A (102) for connecting with the gear transmission assembly is provided in the mounting hole A (107); the middle and top of the side wall plate A (101) are provided with mounting holes B (108), the mounting hole B (108) in the middle is fixedly connected to the side wall support assembly B (10), the toothed worm is rotatably connected to the side wall support assembly B (10), and the mounting hole B (108) in the top is fixedly connected to the top bracket assembly (7).

8. The cable movement and stroke scaling system according to claim 1, characterized in that: The side wall panel assembly B (2) includes a side wall panel B (201) and a mounting base B (203). The side wall panel B (201) has a bottom mounting surface for assembling with the bottom plate (3). The mounting base B (203) is provided on the outer side of the side wall panel B (201). The side wall panel B (201) is fixed to the bottom plate (3) by the mounting base B (203). The lower middle part of the side wall panel B (201) is provided with a mounting hole C (204). The mounting hole C (204) is provided with a bushing C (202) for connecting with the gear transmission assembly. The middle and top parts of the side wall panel B (201) are provided with mounting holes D (205). The mounting hole D (205) in the middle part is fixedly connected to the side wall support assembly A (9). The toothed worm gear is rotatably connected to the side wall support assembly A (9). The mounting hole D (205) in the top part is fixedly connected to the top bracket assembly (7).

9. The cable movement and stroke scaling system according to claim 1, characterized in that: The push rod assembly (5) includes a push rod (501), both ends of which are provided with bushings D (502). One bushing D (502) of the push rod (501) is connected to a moving part (24) on the aircraft, and the other bushing D (502) of the push rod (501) is connected to a transmission spur rack (103) via an adapter (6). The adapter (6) has a double-ear connector (601), and the double-ear connector (601) has two pairs of orthogonal lugs on both sides. Each pair of lugs on one side is provided with a bushing E (602). The sleeve E (602) is hinged to the bushing D (502) at the other end of the push rod (501) by a cotter pin (20), nut (21), washer (22) and bolt (23); one end of the transmission rack (103) is provided with a connecting seat (109), the connecting seat (109) is provided with a bushing B (104), and a pair of lugs on the other side are provided with bushings F (603). The bushing F (603) is hinged to the bushing B (104) on the connecting seat (109) by a cotter pin (20), nut (21), washer (22) and bolt (23).

10. The cable movement and stroke scaling system according to claim 1, characterized in that: The top support assembly (7) includes a top support (701), the two ends of which are fixedly connected to the top of the side wall panel assembly A (1) and the side wall panel assembly B (2) respectively. The top support (701) is provided with a bushing G (702) for rotating connection with the toothed worm gear. The isolation transmission component (8) is provided with a through hole (801) and a spiral hole (802) respectively. The spiral hole (802) is used for threaded connection with the toothed worm gear. The number of through holes (801) is the same as the number of bundles of motion cable assemblies (4) and corresponds one-to-one. Each bundle of motion cable assemblies (4) passes through the corresponding through hole (801).

Citation Information

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