Steering engine performance automatic testing device
By designing the feeding, receiving, and testing mechanisms in the automatic testing device, the problems of inconvenient loading and unloading of servo motors and low testing efficiency in the existing technology have been solved, realizing automated loading and unloading and efficient testing of servo motors.
Patent Information
- Application Number
- CN202520031034.0
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-01-07
- Publication Date
- 2025-11-21
- Estimated Expiration
- 2035-01-07
AI Technical Summary
Existing helicopter servo motor performance testing equipment suffers from inconvenience and inefficiency in terms of loading and unloading and testing efficiency.
An automatic testing device was designed, comprising a feeding mechanism, a receiving mechanism, and a detection mechanism. It utilizes a cylinder and a belt conveyor to achieve automatic loading and unloading of the servo motor, and achieves efficient detection through an infrared heating lamp.
It enables automated loading and unloading and efficient inspection of servo motors, improving operating comfort and inspection efficiency.
Smart Images

Figure CN223581408U_ABST
Abstract
Description
TECHNICAL FIELD
[0001] The utility model relates to rudder performance test technical field, concretely is a rudder performance automatic testing device. BACKGROUND
[0002] The rudder is a kind of big deck machinery on ship. The size of rudder is determined by the outside outfit according to the specification of ship classification society, and the torque size is mainly considered when selecting type. How to carefully select the rudder of economy and in line with demand is also a kind of knowledge that cannot be ignored.
[0003] The application number CN202022806340.7 discloses a kind of helicopter rudder performance automatic testing device, including base structure etc., the utility model design novel, can be lifted out of test container with the helicopter rudder of finished testing, it is convenient to collect the helicopter rudder of finished testing, practicality is higher, it is easy to operate, and higher convenience. The application is specific when using, not only inconvenient feeding and discharging, but also lower detection efficiency. UTILITY MODEL CONTENT
[0004] The utility model aims at solving one of the technical problems in prior art or related art.
[0005] Therefore, the technical scheme adopted by the utility model is as follows:
[0006] A kind of rudder performance automatic testing device, including feeding mechanism, material receiving mechanism and detection mechanism, the feeding mechanism includes table frame, with the two belt conveyors of the table frame top connection, material receiving mechanism, the material receiving mechanism includes with the two slide rails of the table frame top connection, two material receiving plates slidingly connected between two slide rails, with the cylinder of the table frame top connection, with the lift rod of the cylinder movement connection, two transmission plates are movably connected between the material receiving plate and lift rod, detection mechanism, the detection mechanism includes the push plate that is transversely through the table frame top, with the two box bodies of the push plate both ends connection, with the infrared heating lamp of the box body inner chamber top connection, two openings are opened in the table frame.
[0007] By adopting the above technical scheme, the maximum degree contraction of the movable end of cylinder each time, and the material receiving plate indirectly connected with the movable end of cylinder will touch the control switch of belt conveyor, then the rudder on the belt conveyor falls on the material receiving plate, then when the movable end of cylinder is maximally elongated, the material receiving plate will be moved to the bottom of push plate, and the push plate pushes the rudder on the material receiving plate, then it falls to the bottom through the opening, thereby achieving the purpose of self feeding and discharging, and improving the comfort of the device.
[0008] The utility model discloses in a preferable example can be further configured as: the table frame is by desktop, two chassis and top block constitute, the desktop is installed between two chassis, the top block bottom and desktop top fixedly connected, two belt conveyors are located two chassis top respectively, the cylinder bottom end and top block top fixedly connected.
[0009] The utility model discloses in a preferable example can be further configured as: two material receiving plates are located inside two belt conveyors respectively, and the top of the belt conveyor is higher than the top of the material receiving plate.
[0010] The utility model discloses in a preferable example can be further configured as: a plurality of infrared heating lamps are connected in series, and the infrared heating lamps are electrically connected with the external power supply.
[0011] The utility model discloses in a preferable example can be further configured as: two openings are located at both ends of the push plate and are located at the bottom of the two boxes respectively, and the openings are arranged between the two slide rails.
[0012] The utility model discloses in a preferable example can be further configured as: end covers are rotatably connected to both ends of the lifting rod, and a plurality of transmission plates are located between the two lifting rods.
[0013] By adopting the above technical scheme, the utility model has the beneficial effects that:
[0014] 1. In the utility model, the maximum contraction of the movable end of the cylinder each time makes the material receiving plate indirectly connected with the movable end of the cylinder abut the control switch of the belt conveyor, and then the rudder on the belt conveyor falls on the material receiving plate, and when the movable end of the cylinder is maximally elongated, the material receiving plate moves to the bottom of the push plate, the push plate pushes the rudder on the material receiving plate down, and then the rudder falls to the bottom through the opening, thereby achieving the purpose of self feeding and discharging, and improving the use comfort of the device.
[0015] 2. In the utility model, the two material receiving plates indirectly connected with the movable end of the cylinder each time are moved to the bottom of the two boxes, and then this also means that two rudders are moved to the bottom of the infrared heating lamps, thereby achieving heat resistance detection, and the detection is carried out two by two each time, effectively improving the detection efficiency. BRIEF DESCRIPTION OF DRAWINGS
[0016] Figure 1 It is the overall structure perspective drawing of the utility model;
[0017] Figure 2 It is the feeding mechanism schematic view of the utility model;
[0018] Figure 3 It is the material receiving mechanism schematic view of the utility model;
[0019] Figure 4 It is the detection mechanism schematic view of the utility model;
[0020] Figure 5 Figure 1 is a perspective view of the table frame of the utility model.
[0021] Reference signs:
[0022] 100, feeding mechanism; 110, table frame; 111, table top; 112, bottom frame; 113, top block; 120, belt conveyor;
[0023] 200, material receiving mechanism; 210, sliding rail; 220, material receiving plate; 230, air cylinder; 240, lifting rod; 250, transmission plate;
[0024] 300, detection mechanism; 310, push plate; 320, box body; 330, infrared heating lamp; 340, opening; 400, end cover. DETAILED DESCRIPTION
[0025] To make the purpose, technical scheme and advantages of the utility model clearer and more apparent, the utility model is further described in detail below in combination with specific implementation manners and with reference to the drawings. It should be noted that the embodiments of the utility model and the features in the embodiments can be combined with each other without conflict.
[0026] It is understood that the above description is only exemplary and is not intended to limit the scope of the utility model.
[0027] Some embodiments of the utility model provide a rudder performance automatic testing device, which is described below in combination with the drawings.
[0028] Embodiment one:
[0029] In combination with Figures 1-5 the drawings, the utility model provides a rudder performance automatic testing device, which comprises a feeding mechanism 100, a material receiving mechanism 200 and a detection mechanism 300, the feeding mechanism 100 comprises a table frame 110, two belt conveyors 120 connected with the top of the table frame 110;
[0030] The material receiving mechanism 200 comprises two sliding rails 210 connected with the top of the table frame 110, two material receiving plates 220 slidingly connected between the two sliding rails 210, an air cylinder 230 connected with the top of the table frame 110, a lifting rod 240 movably connected with the air cylinder 230, and two transmission plates 250 movably connected between the material receiving plates 220 and the lifting rod 240;
[0031] A detection mechanism 300 is arranged on the top of the table frame 110, which comprises a push plate 310 arranged transversely on the top of the table frame 110, two box bodies 320 connected to the two ends of the push plate 310, an infrared heating lamp 330 connected to the top of the inner cavity of the box body 320, and two openings 340 arranged on the table frame 110.
[0032] Further, the table frame 110 is composed of a table top 111, two bottom frames 112 and a top block 113. The table top 111 is arranged between the two bottom frames 112, and the bottom of the top block 113 is fixedly connected to the top of the table top 111. Two belt conveyors 120 are arranged on the top of the two bottom frames 112 respectively. The bottom end of the air cylinder 230 is fixedly connected to the top end of the top block 113. The structural design of the table frame 110 provides fixing conditions for the belt conveyors 120 and installation conditions for the air cylinder 230 and the push plate 310.
[0033] Further, two material receiving plates 220 are arranged on the inner sides of the two belt conveyors 120 respectively. The top of the belt conveyor 120 is higher than the top of the material receiving plate 220. The layout design of the material receiving plate 220 enables the material receiving plate 220 to successfully contact the control switch of the belt conveyor 120, and also enables the steering engine on the belt conveyor 120 to smoothly fall on the material receiving plate 220.
[0034] Further, two openings 340 are arranged at the two ends of the push plate 310 and at the bottom of the two box bodies 320 respectively. The openings 340 are arranged between the two slide rails 210. The arrangement of the openings 340 provides conditions for the steering engine to smoothly fall to the bottom of the table frame 110.
[0035] Embodiment Two
[0036] In combination with Figure 4 Fig. 2, on the basis of Embodiment One, a plurality of infrared heating lamps 330 are connected in series. The infrared heating lamps 330 are electrically connected to an external power supply. The connection and control mode of the plurality of infrared heating lamps 330 facilitate the operator to turn on the plurality of infrared heating lamps 330, thereby improving the comfort of using the device.
[0037] Embodiment Three
[0038] In combination with Figure 1 and Figure 3 Fig. 3, in the above embodiments, end caps 400 are rotatably connected to the two ends of the lifting rods 240. A plurality of transmission plates 250 are arranged between the two lifting rods 240. The arrangement of the end caps 400 can prevent the transmission plates 250 from falling off the lifting rods 240.
[0039] The working principle and use process of the utility model: when the device is put into practical use, the movable end of the cylinder 230 contracts each time, then the lifting rod 240 is lowered, then the transmission plate 250 on the lifting rod 240 pushes two material receiving plates 220 to both ends of the table frame 110, when the movable end of the cylinder 230 contracts to the maximum extent, the material receiving plate 220 is squeezed to the card of the belt conveyor 120, then the belt conveyor 120 works, and the rudder machine to be detected is conveyed to the material receiving plate 220, then the movable end of the cylinder 230 is controlled to elongate, under the same principle, the material receiving plate 220 slides to the bottom of the infrared heating lamp 330, then the infrared heating lamp 330 carries out heat resistance detection on the rudder machine, then the movable end of the cylinder 230 is controlled to elongate to the maximum extent, then the material receiving plate 220 is received into the bottom of the push plate 310, the push plate 310 pushes the rudder machine on the material receiving plate 220, then the rudder machine falls to the bottom of the table frame 110 through the opening 340, thereby the purpose of self feeding and discharging is realized, in addition, detection is carried out two by two each time, and the detection efficiency is effectively improved.
[0040] Although the embodiments of the utility model have been shown and described, those skilled in the art can understand that various changes, modifications, replacements and variations can be made to these embodiments without departing from the principles and purposes of the utility model, and the scope of the utility model is defined by the claims and its equivalents.
Claims
1. An automatic servo motor performance testing device, characterized in that, include: The feeding mechanism (100) includes a table frame (110) and two belt conveyors (120) connected to the top of the table frame (110); The receiving mechanism (200) includes two slide rails (210) connected to the top of the table frame (110), two receiving plates (220) slidably connected between the two slide rails (210), a cylinder (230) connected to the top of the table frame (110), a lifting rod (240) movably connected to the cylinder (230), and two transmission plates (250) movably connected between the receiving plate (220) and the lifting rod (240). The testing mechanism (300) includes a push plate (310) that runs horizontally through the top of the table frame (110), two boxes (320) connected to both ends of the push plate (310), an infrared heating lamp (330) connected to the top of the inner cavity of the box (320), and two openings (340) on the table frame (110).
2. The automatic servo motor performance testing device according to claim 1, characterized in that, The table frame (110) consists of a tabletop (111), two base frames (112) and a top block (113). The tabletop (111) is installed between the two base frames (112). The bottom of the top block (113) is fixedly connected to the top of the tabletop (111). Two belt conveyors (120) are located on the top of the two base frames (112) respectively. The bottom of the cylinder (230) is fixedly connected to the top of the top block (113).
3. The automatic servo motor performance testing device according to claim 1, characterized in that, Two receiving plates (220) are located inside two belt conveyors (120), with the top of the belt conveyor (120) higher than the top of the receiving plate (220).
4. The automatic servo motor performance testing device according to claim 1, characterized in that, Multiple infrared heating lamps (330) are connected in series, and the infrared heating lamps (330) are electrically connected to an external power supply.
5. The automatic servo motor performance testing device according to claim 1, characterized in that, Two openings (340) are located at both ends of the push plate (310) and at the bottom of the two boxes (320), respectively. The openings (340) are located between the two slide rails (210).
6. The automatic servo motor performance testing device according to claim 1, characterized in that, Both ends of the lifting rod (240) are screwed with end caps (400), and multiple transmission plates (250) are located between the two lifting rods (240).
Citation Information
Patent Citations
Helicopter steering engine performance automatic testing device
CN213544035U