A tail thrust ducted motor
By adopting a combination design of thermal conductivity ring, heat dissipation scale and heat insulation plate in the tail push duct motor, the problem of heat conduction of the duct motor is solved, and the heat dissipation efficiency of the motor and the safety of the drone are improved.
Patent Information
- Application Number
- CN202421161181.1
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-05-27
- Publication Date
- 2025-04-11
- Estimated Expiration
- 2034-05-27
AI Technical Summary
The heat generated by existing duct motors during high-speed operation is easily transmitted to the drone through the shell, resulting in fusion at the connection.
A tail push duct motor is designed, using a fixed shell, a rotating shaft, a fixing mechanism and a mounting mechanism. The heat generated by the motor body is quickly spread to the inside of the fixed shell through the thermal conduction ring and the heat dissipation scale, and heat is prevented from being transmitted to the drone through the thermal insulation plate.
It effectively improves the heat dissipation efficiency of the motor body, avoids heat transmission to the drone, reduces the risk of drone damage, and improves the safety of drone operation.
Smart Images

Figure CN222750234U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to a ducted motor, in particular to a tail thrust ducted motor, belonging to the technical field of motors. Background Art
[0002] A motor is a device that converts electrical energy into mechanical energy. It uses an energized coil to generate a rotating magnetic field and acts on the rotor to form a magnetic-electrical power rotation torque. Electric motors are divided into DC motors and AC motors according to the power source used. Most of the motors in the power system are AC motors. The working principle of the motor is that the magnetic field acts on the force of the current to make the motor rotate.
[0003] The utility model with patent number CN219204254U discloses a brushless ducted motor, including a housing, a rotating shaft is arranged inside the housing, and a fan blade is installed at the first end of the rotating shaft. In the utility model, the outer side of the fixed base is zero-matched with the housing, and the fixed base and the inner housing can be installed together by pressing the fixed base into the inner housing during installation, and it is not necessary to use fasteners such as bolts to connect, which is convenient for installation; the first bearing and the second bearing are distributed at the end of the rotating shaft or near the end, and the exposed parts at both ends of the rotating shaft are shorter, thereby reducing the amplitude of the swing, so as to reduce the vibration of the motor, and further reduce the noise of the motor.
[0004] In order to save costs and reduce the weight of the drone industry, a large amount of plastic materials are used. Ducted motors generate more heat when running at high speeds. Although the device in the above patent improves the stability of the motor operation, the heat generated by the motor can easily be transferred to the drone through the outer casing, causing fusion of the joints. For this reason, we provide a tail thrust ducted motor to solve the above problem. Utility Model Content
[0005] 1. Technical issues to be resolved
[0006] The purpose of the present utility model is to provide a tail thrust ducted motor in order to solve the above-mentioned problem, so as to solve the problem in the reference document that the heat generated by the motor operation is easily transferred to the UAV.
[0007] (II) Technical solution
[0008] The utility model is realized through the following technical scheme: a tail thrust ducted motor.
[0009] It includes a fixed shell, a rotating shaft is arranged inside the fixed shell, a fixing mechanism is arranged inside the fixed shell, the fixing mechanism includes a fixing cylinder and a sealing cover, a first bearing is rotatably connected to the middle of the fixing cylinder, a mounting mechanism is arranged above the fixed shell, the mounting mechanism includes a heat insulation board, a connecting frame is fixedly connected to the middle of the heat insulation board, and the bottom end of the connecting frame is fixedly connected to the fixed shell.
[0010] Preferably, a motor body for controlling the rotation of a rotating shaft is provided inside the fixed cylinder, one end of the rotating shaft is fixedly connected to a turbine blade, the rotating shaft is rotatably connected to a first bearing, and the rotation of the rotating shaft is controlled by the motor body, so that the rotating shaft drives the turbine blade to rotate, thereby generating backward thrust.
[0011] Preferably, a second bearing is rotatably connected to the middle of the sealing cover, and the second bearing is rotatably connected to the rotating shaft. A protective cover plate is fixedly connected to the surface of the sealing cover, and the rotating shaft is secondarily fixed through the second bearing.
[0012] Preferably, a connecting plate is fixedly connected to the surface of the fixing tube, and one end of the connecting plate away from the fixing tube is fixedly connected to the fixing shell, and the fixing tube is fixed in the middle of the fixing shell through the connecting plate.
[0013] Preferably, a mounting column is fixedly connected to the surface of the fixed cylinder, and one end of the mounting column passes through the sealing cover and is slidably connected to the sealing cover, a nut is threadedly connected to the surface of the mounting column, and the nut is rotatably connected to the sealing cover, a sealing gasket is clamped on the surface of the nut, and the sealing cover and the fixed cylinder are fixed together by the mounting column and the nut.
[0014] Preferably, a heat-conducting ring is fixedly connected to the interior of the fixed tube, and the inner wall of the heat-conducting ring is in contact with the motor body, and a heat-dissipating fin is fixedly connected to the surface of the heat-conducting ring, and the heat-dissipating fin passes through the fixed tube and is fixedly connected to the fixed tube, and the heat generated by the motor body is quickly diffused to the interior of the fixed shell through the heat-conducting ring and the heat-dissipating fin.
[0015] Preferably, an anti-slip pad is fixedly connected to the surface of the insulation board, a fixing bolt is slidably connected to the middle of the insulation board, and the top end of the fixing bolt passes through the anti-slip pad and is slidably connected to the anti-slip pad, and the insulation board is fixed to the tail of the drone through the fixing bolt.
[0016] The utility model provides a tail thrust ducted motor, which has the following beneficial effects:
[0017] 1. The tail thrust ducted motor supports and fixes the position of the rotating shaft through the first bearing to prevent the rotating shaft from swinging when rotating at high speed, thereby improving the stability of the rotating shaft operation. The position of the motor body is fixed through the fixing tube and the sealing cover to keep the motor body in a stable operating state. The fixed shell is fixed together with the heat insulation board through the connecting frame. The heat insulation board prevents the heat generated by the motor body from being transferred to the UAV, thereby improving the safety of the UAV operation.
[0018] 2. The tail thrust ducted motor controls the rotation of the rotating shaft through the motor body, so that the rotating shaft drives the turbine fan blades to rotate, generates backward thrust, and moves the UAV forward. The rotating shaft is fixed for a second time through the second bearing to improve the stability of the rotating shaft operation. The second bearing and the rotating shaft are protected by the protective cover to prevent foreign objects from touching the second bearing and the rotating shaft. The fixed cylinder is fixed in the middle of the fixed shell through the connecting plate to keep the fixed cylinder stable during operation. The position of the sealing cover is limited by the mounting column to prevent the sealing cover from rotating back and forth.
[0019] 3. The tail thrust ducted motor fixes the sealing cover and the fixing tube together through the mounting column and the nut. The mounting column and the nut are protected by the sealing gasket to prevent the humid air from corroding the mounting column and the nut. The heat generated by the motor body is quickly diffused into the fixed shell through the heat conduction ring and the heat dissipation scales to improve the heat dissipation efficiency of the motor body. The heat insulation board is fixed to the tail of the drone through the fixing bolts. The friction between the heat insulation board and the drone is increased through the anti-slip pad, so that the thrust generated by the ducted motor can be better transmitted to the drone. BRIEF DESCRIPTION OF THE DRAWINGS
[0020] Figure 1 It is a schematic diagram of the overall structure of the utility model;
[0021] Figure 2 This is a schematic diagram of the internal structure of the fixed housing of the utility model;
[0022] Figure 3 This is a schematic diagram of the fixing mechanism structure of the utility model;
[0023] Figure 4 It is a schematic diagram of the exploded structure of the installation mechanism of the utility model.
[0024]
Main component symbol description
[0025] 1. Fixed housing; 2. Motor body; 3. Rotating shaft; 4. Turbine blades;
[0026] 5. Fixing mechanism; 501. Fixing cylinder; 502. Connecting plate; 503. First bearing; 504. Sealing cover; 505. Second bearing; 506. Mounting column; 507. Nut; 508. Sealing pad; 509. Protective cover;
[0027] 6. Installation mechanism; 601. Heat insulation board; 602. Connecting frame; 603. Anti-skid pad; 604. Fixing bolt;
[0028] 7. Thermal conductive ring; 8. Heat dissipation fins. DETAILED DESCRIPTION
[0029] An embodiment of the utility model provides a tail thrust ducted motor.
[0030] See also Figure 1 , Figure 2 and Figure 3 , including a fixed shell 1, a rotating shaft 3 is arranged inside the fixed shell 1, a fixing mechanism 5 is arranged inside the fixed shell 1, the fixing mechanism 5 includes a fixing cylinder 501 and a sealing cover 504, the middle part of the fixing cylinder 501 is rotatably connected with a first bearing 503, the position of the rotating shaft 3 is supported and fixed by the first bearing 503, so as to avoid the rotating shaft 3 from swinging when rotating at a high speed, and improve the stability of the operation of the rotating shaft 3, and the position of the motor body 2 is fixed by the fixing cylinder 501 and the sealing cover 504, so that the motor body 2 maintains a stable operating state.
[0031] The interior of the fixed cylinder 501 is provided with a motor body 2 for controlling the rotation of the rotating shaft 3. One end of the rotating shaft 3 is fixedly connected to the turbine blade 4. The rotating shaft 3 is rotatably connected to the first bearing 503. The rotation of the rotating shaft 3 is controlled by the motor body 2, so that the rotating shaft 3 drives the turbine blade 4 to rotate, thereby generating backward thrust and moving the drone forward.
[0032] The motor body 2 is a prior art, and this application will not go into detail on its detailed parameters and models.
[0033] The middle part of the sealing cover 504 is rotatably connected to a second bearing 505, and the second bearing 505 is rotatably connected to the rotating shaft 3. A protective cover plate 509 is fixedly connected to the surface of the sealing cover 504. The rotating shaft 3 is fixed for a second time through the second bearing 505 to improve the stability of the operation of the rotating shaft 3. The second bearing 505 and the rotating shaft 3 are protected through the protective cover plate 509 to prevent foreign matter from touching the second bearing 505 and the rotating shaft 3.
[0034] A connecting plate 502 is fixedly connected to the surface of the fixed cylinder 501, and one end of the connecting plate 502 away from the fixed cylinder 501 is fixedly connected to the fixed shell 1. The fixed cylinder 501 is fixed in the middle of the fixed shell 1 through the connecting plate 502, so that the fixed cylinder 501 remains stable during operation.
[0035] A mounting post 506 is fixedly connected to the surface of the fixed cylinder 501, and one end of the mounting post 506 passes through the sealing cover 504 and is slidably connected to the sealing cover 504, a nut 507 is threadedly connected to the surface of the mounting post 506, and the nut 507 is rotatably connected to the sealing cover 504, a sealing gasket 508 is clamped on the surface of the nut 507, and the position of the sealing cover 504 is limited by the mounting post 506 to prevent the sealing cover 504 from rotating back and forth, and the sealing cover 504 and the fixed cylinder 501 are fixed together by the mounting post 506 and the nut 507, and the mounting post 506 and the nut 507 are protected by the sealing gasket 508 to prevent the mounting post 506 and the nut 507 from being corroded by external humid air.
[0036] A heat-conducting ring 7 is fixedly connected to the interior of the fixed cylinder 501, and the inner wall of the heat-conducting ring 7 is in contact with the motor body 2. A heat-dissipating fin 8 is fixedly connected to the surface of the heat-conducting ring 7, and the heat-dissipating fin 8 penetrates the fixed cylinder 501 and is fixedly connected to the fixed cylinder 501. Through the heat-conducting ring 7 and the heat-dissipating fin 8, the heat generated by the motor body 2 is quickly diffused into the interior of the fixed shell 1, thereby improving the heat dissipation efficiency of the motor body 2.
[0037] See also Figure 4 A mounting mechanism 6 is provided above the fixed shell 1, and the mounting mechanism 6 includes a heat insulation board 601, a connecting frame 602 is fixedly connected to the middle of the heat insulation board 601, and the bottom end of the connecting frame 602 is fixedly connected to the fixed shell 1. The heat insulation board 601 is used to prevent the heat generated by the motor body 2 from being transferred to the drone, thereby improving the safety of the device operation. The fixed shell 1 and the heat insulation board 601 are fixed together through the connecting frame 602.
[0038] The surface of the heat insulation board 601 is fixedly connected with an anti-skid pad 603, the middle part of the heat insulation board 601 is slidably connected with a fixing bolt 604, and the top end of the fixing bolt 604 passes through the anti-skid pad 603 and is slidably connected with the anti-skid pad 603. The heat insulation board 601 is fixed to the tail of the UAV through the fixing bolt 604, and the friction between the heat insulation board 601 and the UAV is increased through the anti-skid pad 603, so that the thrust generated by the ducted motor can be better transmitted to the UAV.
[0039] When the utility model is in use: the heat insulation board 601 is fixed to the tail of the UAV by the fixing bolt 604, and the heat insulation board 601 is used to prevent the heat generated by the motor body 2 from being transferred to the UAV, thereby improving the safety of the device operation. The rotation of the rotating shaft 3 is controlled by the motor body 2, so that the rotating shaft 3 drives the turbine blades 4 to rotate, thereby generating a backward thrust, and the UAV moves forward. At the same time, the heat generated by the motor body 2 is quickly diffused into the fixed shell 1 by the heat conductive ring 7 and the heat dissipation fins 8. The turbine blades 4 blow air backwards to cool the heat dissipation fins 8, thereby preventing the high temperature generated by the motor body 2 from being transferred out. At the same time, the rotating shaft 3 is supported by the first bearing 503 and the second bearing 505, thereby preventing the rotating shaft 3 from swinging and improving the rotation stability of the turbine blades 4. Through the above device, the ducted motor can better generate tail thrust for the UAV, and avoids heat conduction to the UAV to cause damage to the UAV, thereby improving the safety of the UAV operation.
[0040] The above shows and describes the basic principle and main features of the utility model and the advantages of the utility model. Those skilled in the art should understand that the utility model is not limited by the above embodiments. The above embodiments and descriptions are only for explaining the principle of the utility model. Without departing from the spirit and scope of the utility model, the utility model may have various changes and improvements, which fall within the scope of the utility model to be protected. The scope of protection claimed by the utility model is defined by the attached claims and their equivalents.
Claims
1. A tail thrust ducted motor, comprising a fixed housing (1), characterized in that: A rotating shaft (3) is arranged inside the fixed shell (1), and a fixing mechanism (5) is arranged inside the fixed shell (1). The fixing mechanism (5) comprises a fixing cylinder (501) and a sealing cover (504). The middle part of the fixing cylinder (501) is rotatably connected to a first bearing (503). An installation mechanism (6) is arranged above the fixed shell (1), and the installation mechanism (6) comprises a heat insulation board (601). The middle part of the heat insulation board (601) is fixedly connected to a connecting frame (602), and the bottom end of the connecting frame (602) is fixedly connected to the fixed shell (1).
2. The tail thrust ducted motor according to claim 1, characterized in that: The interior of the fixed cylinder (501) is provided with a motor body (2) for controlling the rotation of a rotating shaft (3); one end of the rotating shaft (3) is fixedly connected to a turbine blade (4); and the rotating shaft (3) is rotatably connected to a first bearing (503).
3. The tail thrust ducted motor according to claim 1, characterized in that: The middle part of the sealing cover (504) is rotatably connected to a second bearing (505), and the second bearing (505) is rotatably connected to the rotating shaft (3), and the surface of the sealing cover (504) is fixedly connected to a protective cover plate (509).
4. The tail thrust ducted motor according to claim 1, characterized in that: A connecting plate (502) is fixedly connected to the surface of the fixed cylinder (501), and one end of the connecting plate (502) away from the fixed cylinder (501) is fixedly connected to the fixed housing (1).
5. The tail thrust ducted motor according to claim 1, characterized in that: The surface of the fixed cylinder (501) is fixedly connected with a mounting column (506), and one end of the mounting column (506) passes through the sealing cover (504) and is slidably connected to the sealing cover (504), the surface of the mounting column (506) is threadedly connected with a nut (507), and the nut (507) is rotatably connected to the sealing cover (504), and the surface of the nut (507) is clamped with a sealing gasket (508).
6. The tail thrust ducted motor according to claim 1, characterized in that: A heat-conducting ring (7) is fixedly connected to the interior of the fixed tube (501), and the inner wall of the heat-conducting ring (7) contacts the motor body (2). A heat-dissipating fin (8) is fixedly connected to the surface of the heat-conducting ring (7), and the heat-dissipating fin (8) passes through the fixed tube (501) and is fixedly connected to the fixed tube (501).
7. The tail thrust ducted motor according to claim 1, characterized in that: The surface of the heat insulation board (601) is fixedly connected with an anti-skid pad (603), the middle part of the heat insulation board (601) is slidably connected with a fixing bolt (604), and the top end of the fixing bolt (604) passes through the anti-skid pad (603) and is slidably connected to the anti-skid pad (603).
Citation Information
Patent Citations
Brushless ducted motor
CN219204254U