Model airplane paddle torsion connecting piece
By designing the torque connector of the model aircraft blade and using the combination of resistor coil and reinforcement frame plate, the blade instability problem caused by the motor shaft torque mismatch is solved, and efficient torque transmission and stability improvement is achieved to prevent the model aircraft from falling.
Patent Information
- Application Number
- CN202420845951.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-04-22
- Publication Date
- 2024-12-27
- Estimated Expiration
- 2034-04-22
AI Technical Summary
The torque of the model aircraft blade seat is due to the high torque rotation of the motor shaft, which is not matched with the high-efficiency motor, resulting in low-speed torque. The blades are instable due to excessive airflow pressure during liftoff and are prone to falling.
A torque connector for the model aircraft blade is designed, including wires, resistor coils, reinforcement frame plates, disc connecting frame seats, inner clamping rings and outer frame housing seats. The resistor coils are electrically connected to the disc connecting frame seats, combined with reinforcement The ribbed frame plate and carbon brush plate form a synchronous electromagnetic movement with high torque matching, improving the flexibility and stability of the torque connector.
It ensures a stable connection between the motor shafts of various high and low frequencies and the blades, improves the flexibility of the blade torque connector and the torque pressure bearing value, prevents desistance, and improves the stability and safety of the model aircraft.
Smart Images
Figure CN222260684U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of model airplanes, in particular to a model airplane blade torsion connector. Background Art
[0002] Aviation model is a general term for various aircraft models, including model airplanes and other model aircraft. Aviation model activities have aroused people's strong interest in exploring the sky from the very beginning, and have flourished for thousands of years. The main reason is that it plays a very important role in the development of aviation industry and the cultivation of scientific and technological talents.
[0003] The torque of the propeller seat of the model aircraft is often unable to be used due to the high-torque rotation of the motor shaft, which makes it mismatched with the high-efficiency motor and leads to the use of a low-speed torque motor. When the model aircraft is launched, the propeller blades are prone to accidental falling and damage due to excessive wind pressure in the airflow layer, which makes it impossible for the propeller blades to stabilize the torque model aircraft body. Utility Model Content
[0004] In view of the deficiencies in the prior art, the utility model provides a model aircraft blade torsion connector to solve the problem that the torque of the model aircraft blade seat is often unable to be used due to the high torque rotation of the motor shaft, which causes the blade to be mismatched with the high-efficiency motor and cannot be used, resulting in the use of a low-speed torque motor. When the model aircraft is launched, the blade is prone to accidental falling and damage due to excessive wind pressure in the airflow layer, which makes it impossible for the blade to stabilize the torque model aircraft fuselage.
[0005] To achieve the above purpose, the utility model is implemented through the following technical solutions: a model aircraft blade torsion connector, including a wire, a resistance coil, a reinforcing rib frame plate, a disk connection frame seat, an inner hoop ring, and an outer frame shell seat. The wire is inserted into the left side of the outer frame shell seat, and five reinforcing rib frame plates are fixed in the outer frame shell seat. The five reinforcing rib frame plates are welded into one around the axis of the disk connection frame seat, and the disk connection frame seat and the inner hoop ring are nested into one. The wire is electrically connected to the disk connection frame seat through the resistance coil, and the disk connection frame seat is provided with a bearing seat, a rivet, an inner shaft ring mouth, a strip sheet metal, and a carbon brush plate. The bearing seat is equipped with an inner shaft ring mouth and a strip sheet metal. The carbon brush plate is provided with eight and is tightly attached to the outer ring edge of the bearing seat around the axis of the inner shaft ring mouth. The strip sheet metal is locked with the bearing seat through rivets, and the carbon brush plate is electrically connected to the resistance coil.
[0006] Preferably, the resistance coil is provided with an upper fixing seat, a coil body, a resistance block, and a lower fixing seat. The upper fixing seat and the lower fixing seat are respectively welded to the upper and lower sides of the resistance block. The resistance block is installed inside the coil body. The coil body and the resistance block are interference fit. The coil body is electrically connected to the carbon brush plate through the resistance block.
[0007] Preferably, the inner shaft ring has a wide shaft ring structure with a centrally locked axis and a thick wheel surface, which facilitates the combination of the inner shaft ring and the sheet metal strip to lift and press-fit the model aircraft blade base stably and efficiently, thereby improving the flexible adaptability and bearing performance of the torque connector.
[0008] Preferably, the strip of sheet metal is a sheet metal structure with through holes at both ends and a long strip in the middle, which facilitates the combination of the inner shaft ring and the strip of sheet metal to lift and press-fit the model aircraft blade base stably and efficiently, thereby improving the flexible adaptability and bearing performance of the torsion connector.
[0009] Preferably, the carbon brush plate has a composite carbon brush plate surface structure with an upper curved arc with a wide extension and a lower narrow opening, which facilitates the carbon brush plate and the coil body to form the stability of the motor's high and low frequency matching torque synchronous electromagnetic motion under the relay transition of the resistance block.
[0010] Preferably, the coil body has a spiral coil structure in which narrow copper core wires are obliquely pulled and centrally wound to widen the upper left and lower right corners, so as to facilitate the carbon brush plate and the coil body to form the stability of the motor's high and low frequency matching torque synchronous electromagnetic motion under the relay transition of the resistance block.
[0011] The utility model provides a torsion connector for a model airplane blade, which has the following beneficial effects:
[0012] In this aircraft model propeller blade torsion connector, workers assemble the coil body and the resistor block of the wire series resistor coil, let the resistor block cooperate with the reinforcing rib frame plate to surround the bearing seat built into the disk connection frame seat, and then form the load-bearing of the aircraft model propeller blade base torsion connection through the inner clamp ring and the outer frame shell seat, let the high-efficiency motor shaft rotate on the inner shaft ring to drive the strip sheet metal and the carbon brush plate to work together, so that the rivet reinforced stable carbon brush plate and the resistor coil can achieve high torque matching and synchronous working effect, ensure the stability of various high and low frequency motor shafts connecting the aircraft model propeller blades, improve the flexibility of the blade torsion connector, let the coil body and the resistor block be distributed in multiple groups to improve the voltage pressure and torque pressure bearing value, and the inner shaft ring and the strip sheet metal are superimposed and pressed to prevent the shaft from coming off efficiently. BRIEF DESCRIPTION OF THE DRAWINGS
[0013] Figure 1 This is a schematic diagram of a top view of the structure of a torsion connector for a model airplane blade according to the utility model;
[0014] Figure 2 This is a schematic diagram of the top view of the disk connection frame of the utility model;
[0015] Figure 3 This is a schematic diagram of the perspective structure of the disk connecting frame seat of the utility model from above;
[0016] Figure 4 It is a schematic diagram of the top view structure of the resistance coil of the utility model.
[0017] In the figure: wire 1, resistance coil 2, reinforcing rib frame plate 3, disk connecting frame seat 4, inner hoop ring 5, outer frame shell seat 6, upper fixing seat 21, coil body 22, resistance block 23, lower fixing seat 24, bearing seat 41, rivet 42, inner shaft ring mouth 43, sheet metal strip 44, carbon brush plate 45. DETAILED DESCRIPTION
[0018] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.
[0019] See also Figure 1-Figure 4 The utility model provides a model aircraft blade torsion connector, including a wire 1, a resistance coil 2, a reinforcing rib frame plate 3, a disk connection frame seat 4, an inner hoop ring 5, and an outer frame shell seat 6. The wire 1 is inserted into the left side of the outer frame shell seat 6. Five reinforcing rib frame plates 3 are fixed in the outer frame shell seat 6. The five reinforcing rib frame plates 3 are welded into one around the axis of the disk connection frame seat 4. The disk connection frame seat 4 and the inner hoop ring 5 are nested into one. The wire 1 is electrically connected to the disk connection frame seat 4 through the resistance coil 2.
[0020] Because the torque of the propeller seat of the model aircraft is often caused by the high torque rotation of the motor shaft, it is not matched with the high-efficiency motor and cannot be used, resulting in the use of a low-speed torque motor. When the model aircraft is launched, the propeller blades are prone to accidental falling and damage due to excessive wind pressure in the airflow layer, which makes the propeller blades unable to stabilize the torque model aircraft body.
[0021] The disk connecting frame seat 4 is provided with a bearing seat 41, a rivet 42, an inner shaft ring opening 43, a strip sheet metal 44, and a carbon brush plate 45. The inner shaft ring opening 43 and the strip sheet metal 44 are installed in the bearing seat 41. There are eight carbon brush plates 45 and they are tightly attached to the outer ring edge of the bearing seat 41 around the axis of the inner shaft ring opening 43. The strip sheet metal 44 is locked with the bearing seat 41 by the rivet 42, and the carbon brush plate 45 is electrically connected to the resistance coil 2.
[0022] The resistance coil 2 is provided with an upper fixing seat 21, a coil body 22, a resistance block 23, and a lower fixing seat 24. The upper fixing seat 21 and the lower fixing seat 24 are respectively welded to the upper and lower sides of the resistance block 23. The resistance block 23 is installed inside the coil body 22. The coil body 22 and the resistance block 23 are interference fit. The coil body 22 is electrically connected to the carbon brush plate 45 through the resistance block 23.
[0023] The inner shaft ring opening 43 is a wide shaft ring opening structure with a centrally locked axis and a thick wheel surface, which facilitates the inner shaft ring opening 43 and the strip sheet metal 44 to be combined to lift and press the model aircraft blade base stably and efficiently, and improves the flexible adaptability and bearing performance of the torsion connector. The strip sheet metal 44 is a sheet metal structure with through holes at both ends and a long strip in the middle, which facilitates the inner shaft ring opening 43 and the strip sheet metal 44 to be combined to lift and press the model aircraft blade base stably and efficiently, and improves the flexible adaptability and bearing performance of the torsion connector.
[0024] The carbon brush plate 45 has a composite carbon brush plate surface structure with a wide upper curved leg and a narrow lower end, which facilitates the carbon brush plate 45 and the coil body 22 to form the stability of the motor's high and low frequency matching torque synchronous electromagnetic movement under the relay transition of the resistor block 23. The coil body 22 has a spiral coil structure with narrow copper core wires obliquely pulled and centrally wound and widened at the upper left and lower right corners, which facilitates the carbon brush plate 45 and the coil body 22 to form the stability of the motor's high and low frequency matching torque synchronous electromagnetic movement under the relay transition of the resistor block 23.
[0025] The staff assembles the coil body 22 and the resistor block 23 of the resistor coil 2 connected in series with the wire 1, and allows the resistor block 23 to cooperate with the reinforcing rib frame plate 3 to surround the bearing seat 41 built into the disk connecting frame seat 4, and then forms the load-bearing of the torsional connection of the model aircraft blade base through the inner clamp ring 5 and the outer frame shell seat 6, so that the high-efficiency motor shaft moves in the inner shaft ring 43 to rotate and drive the strip sheet metal 44 and the carbon brush plate 45 to work in conjunction, so that the rivet 42 reinforces and stabilizes the carbon brush plate 45 and the resistor coil 2 to perform high torque matching and synchronous working effects, ensuring the stability of various high and low frequency motor shafts connecting the model aircraft blades, and improving the flexibility of the blade torsional connectors, so that the coil body 22 and the resistor block 23 are distributed in multiple groups to increase the voltage and torque bearing values, and the inner shaft ring 43 and the strip sheet metal 44 are superimposed and pressed to prevent the shaft from coming off efficiently.
[0026] The above description is only a specific implementation manner of the present application, but the protection scope of the present application is not limited thereto. Any technician familiar with the technical field can easily think of changes or substitutions within the technical scope disclosed in the present application, which should be included in the protection scope of the present application.
Claims
1. A model aircraft blade torsion connector, characterized in that: The invention comprises a conductor (1), a resistance coil (2), a reinforcing rib frame plate (3), a disk connection frame seat (4), an inner hoop ring (5), and an outer frame shell seat (6); the conductor (1) is inserted into the left side of the outer frame shell seat (6); five reinforcing rib frame plates (3) are fixedly arranged in the outer frame shell seat (6); the five reinforcing rib frame plates (3) are welded together around the axis of the disk connection frame seat (4); the disk connection frame seat (4) and the inner hoop ring (5) are nested together; the conductor (1) is electrically connected to the disk connection frame seat (4) through the resistance coil (2); The disk connecting frame seat (4) is provided with a bearing seat (41), a rivet (42), an inner shaft ring opening (43), a sheet metal strip (44), and a carbon brush plate (45). The inner shaft ring opening (43) and the sheet metal strip (44) are installed in the bearing seat (41). Eight carbon brush plates (45) are provided and are tightly attached to the outer ring edge of the bearing seat (41) around the axis of the inner shaft ring opening (43). The sheet metal strip (44) is locked with the bearing seat (41) by the rivet (42). The carbon brush plate (45) is electrically connected to the resistance coil (2).
2. The aircraft model propeller blade torsion connector according to claim 1, characterized in that: The resistance coil (2) is provided with an upper fixing seat (21), a coil body (22), a resistance block (23), and a lower fixing seat (24); the upper fixing seat (21) and the lower fixing seat (24) are respectively welded to the upper and lower sides of the resistance block (23); the resistance block (23) is installed inside the coil body (22); the coil body (22) and the resistance block (23) are interference fit; the coil body (22) is electrically connected to the carbon brush plate (45) through the resistance block (23).
3. The aircraft model propeller blade torsion connector according to claim 1, characterized in that: The inner shaft ring opening (43) is a wide shaft ring opening structure with a centrally locked shaft center and a thick wheel surface.
4. The aircraft model propeller blade torsion connector according to claim 1, characterized in that: The strip of sheet metal (44) is a sheet metal structure with through holes at both ends and a long strip in the middle.
5. The aircraft model propeller blade torsion connector according to claim 1, characterized in that: The carbon brush plate (45) presents a composite carbon brush plate surface structure with an upper curved arc with a wide extension and a lower narrow opening.
6. The aircraft model propeller blade torsion connector according to claim 2, characterized in that: The coil body (22) has a spiral coil structure in which a narrow copper core wire is obliquely pulled and centrally wound to increase width at both the upper left corner and the lower right corner.