WO2021017004A1 - Structure de verrouillage, hélice, dispositif d'alimentation, ensemble d'alimentation, et véhicule aérien sans pilote - Google Patents

Structure de verrouillage, hélice, dispositif d'alimentation, ensemble d'alimentation, et véhicule aérien sans pilote Download PDF

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Publication number
WO2021017004A1
WO2021017004A1 PCT/CN2019/098923 CN2019098923W WO2021017004A1 WO 2021017004 A1 WO2021017004 A1 WO 2021017004A1 CN 2019098923 W CN2019098923 W CN 2019098923W WO 2021017004 A1 WO2021017004 A1 WO 2021017004A1
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WO
WIPO (PCT)
Prior art keywords
stopper
propeller
coupling portion
movable part
locking structure
Prior art date
Application number
PCT/CN2019/098923
Other languages
English (en)
Chinese (zh)
Inventor
邱健达
都涛
Original Assignee
深圳市大疆创新科技有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 深圳市大疆创新科技有限公司 filed Critical 深圳市大疆创新科技有限公司
Priority to CN201980032122.XA priority Critical patent/CN112119009A/zh
Priority to PCT/CN2019/098923 priority patent/WO2021017004A1/fr
Publication of WO2021017004A1 publication Critical patent/WO2021017004A1/fr

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • B64C27/14—Direct drive between power plant and rotor hub
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/02—Hub construction
    • B64C11/04—Blade mountings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/20—Transmission of mechanical power to rotors or propellers

Definitions

  • This application relates to the field of mechanical technology, and in particular to a locking structure, a propeller, a power device, a power component and an unmanned aerial vehicle.
  • the propeller is an important part of the multi-rotor UAV, and due to the need to reduce the storage space and facilitate the replacement of the propeller, the multi-rotor UAV often uses a propeller locking mechanism that can be quickly assembled and disassembled.
  • the locking is usually realized by a rotating action, so that the operator is required to simultaneously hold the motor rotor and the propeller and rotate relative to each other in order to realize the assembly and disassembly. In this way, the tension and torque that the locking structure bears during the operation of the motor tends to loosen the locking mechanism, and the reliability is not high.
  • This application provides a locking structure, a propeller, a power plant, a power assembly and an unmanned aerial vehicle.
  • the locking structure of the embodiment of the present application is used to detachably connect the propeller to the power plant.
  • the locking structure includes a mounting seat and a locking assembly, the locking assembly includes a movable part and a stopper, the mounting seat and the One of the movable parts is used for mechanical coupling with the propeller, and the other is used for mechanical coupling with the power device.
  • the mounting seat is provided with a first coupling part, and the movable part is provided with a second coupling part.
  • the stopper is movably connected with the movable part and can be switched back and forth between the locked position and the unlocked position;
  • the stopper When the stopper is in the locked position, the stopper abuts at least one of the first coupling portion and the second coupling portion, so that the first coupling portion and the second coupling portion ⁇ ; Part joint connection;
  • the stopper When the stopper is located in the unlocking position, the stopper provides a movable space for at least one of the first coupling portion and the second coupling portion, so that the first coupling portion and the second coupling portion The two joints can be separated.
  • the first coupling part and the second coupling part can be connected and separable respectively.
  • the locking and unlocking can be realized only by controlling the position of the stopper, without rotating the propeller and/or the power unit, which facilitates the disassembly and assembly process of the propeller and the power unit.
  • the propeller of the embodiment of the present application is used to provide flight power to the drone.
  • the propeller includes a movable part, a stopper, and a hub connected to the stopper, and the movable part is used for installation with a power device
  • the mounting seat is provided with a first coupling part
  • the movable part is provided with a second coupling part
  • the stopper is movably connected with the movable part, and can be moved back and forth between the locked position and the unlocked position Switch
  • the stopper When the stopper is in the locked position, the stopper abuts at least one of the first coupling portion and the second coupling portion, so that the first coupling portion and the second coupling portion ⁇ ; Part joint connection;
  • the stopper When the stopper is located in the unlocking position, the stopper provides a movable space for at least one of the first coupling portion and the second coupling portion, so that the first coupling portion and the second coupling portion The two joints can be separated.
  • the stopper since the stopper is in the locked position and the unlocked position, the first joint part and the second joint part can be connected and detached respectively. In this way, when disassembling the propeller and the power unit, the locking and unlocking can be realized only by controlling the position of the stopper, without rotating the propeller and/or the power unit, which facilitates the disassembly and assembly process of the propeller and the power unit.
  • the power plant of the embodiment of the present application includes a rotor and a mounting seat that rotates with the rotor.
  • the mounting seat is used to cooperate with the movable part of the propeller.
  • the mounting seat is provided with a first coupling portion.
  • the propeller is provided with a second joining part, the propeller includes the movable part and a stopper, and the stopper is movably connected with the movable part and can be switched back and forth between a locked position and an unlocked position;
  • the stopper When the stopper is in the locked position, the stopper abuts at least one of the first coupling portion and the second coupling portion, so that the first coupling portion and the second coupling portion ⁇ ; Part joint connection;
  • the stopper When the stopper is located in the unlocking position, the stopper provides a movable space for at least one of the first coupling portion and the second coupling portion, so that the first coupling portion and the second coupling portion The two joints can be separated.
  • the stopper since the stopper is in the locked position and the unlocked position, the first coupling part and the second coupling part can be connected and separated respectively. In this way, when disassembling the propeller and the power unit, the locking and unlocking can be realized only by controlling the position of the stopper, without rotating the propeller and/or the power unit, which facilitates the disassembly and assembly process of the propeller and the power unit.
  • the power assembly of the embodiment of the present application includes a power device, a propeller, and the locking structure described in the foregoing embodiment, the mounting seat is installed on the power device, and the movable part is connected to the propeller.
  • the stopper since the stopper is in the locked position and the unlocked position, the first coupling part and the second coupling part can be connected and separable respectively. In this way, when disassembling the propeller and the power unit, the locking and unlocking can be realized only by controlling the position of the stopper, without rotating the propeller and/or the power unit, which facilitates the disassembly and assembly process of the propeller and the power unit.
  • the drone of the embodiment of the present application includes a fuselage and an arm, the arm is connected to the fuselage, and the power assembly described in the above embodiment is installed on the arm.
  • the stopper since the stopper is in the locked position and the unlocked position, the first joint part and the second joint part can be connected and detached respectively. In this way, when disassembling the propeller and the power unit, the locking and unlocking can be realized only by controlling the position of the stopper, without rotating the propeller and/or the power unit, which facilitates the disassembly and assembly process of the propeller and the power unit.
  • FIG. 1 is a perspective structural view of a locking structure in a locked state according to an embodiment of the present application
  • FIG. 2 is a front view of a locking structure of an embodiment of the present application in a locked state
  • FIG. 3 is a top view of a locking structure in a locked state according to an embodiment of the present application.
  • Figure 4 is a cross-sectional view of Figure 3 along the section line A-A;
  • Figure 5 is an enlarged view of part V in Figure 4.
  • FIG. 6 is a perspective structural diagram of a locking structure in an unlocked state according to an embodiment of the present application.
  • FIG. 7 is a front view of a locking structure of an embodiment of the present application in an unlocked state
  • FIG. 8 is a top view of a locking structure of an embodiment of the present application in an unlocked state
  • Figure 9 is a cross-sectional view of Figure 8 along the section line B-B;
  • Fig. 10 is an enlarged view of part X in Fig. 9;
  • Figure 11 is a perspective structural view of another locking structure in a locked state according to an embodiment of the present application.
  • FIG. 12 is a front view of another locking structure of the embodiment of the present application in a locked state
  • Figure 13 is a top view of another locking structure of the embodiment of the present application in a locked state
  • Figure 14 is a cross-sectional view of Figure 13 along the section line C-C;
  • Figure 15 is an enlarged view of part XV in Figure 14;
  • FIG. 16 is a perspective structural diagram of another locking structure in an unlocked state according to an embodiment of the present application.
  • FIG. 17 is a front view of another locking structure of the embodiment of the present application in an unlocked state
  • FIG. 18 is a top view of another locking structure in an unlocked state according to the embodiment of the present application.
  • Figure 19 is a cross-sectional view of Figure 18 along the section line D-D;
  • Figure 20 is an enlarged view of part XX in Figure 19;
  • FIG. 21 is a partial enlarged view of a locking structure of an embodiment of the present application in an unlocked state
  • FIG. 22 is a partial enlarged view of a locking structure in a locked state according to an embodiment of the present application.
  • FIG. 23 is a cross-sectional view of a locking structure of an embodiment of the present application in a locked state
  • 24 is a cross-sectional view of a locking structure in an unlocked state according to an embodiment of the present application.
  • Fig. 25 is a perspective structural view of an unmanned aerial vehicle according to an embodiment of the present application.
  • first and second are only used for descriptive purposes, and cannot be understood as indicating or implying relative importance or implicitly indicating the number of indicated technical features. Therefore, the features defined with “first” and “second” may explicitly or implicitly include one or more of the features. In the description of this application, “multiple” means two or more than two, unless otherwise specifically defined.
  • connection should be interpreted broadly unless otherwise clearly specified and limited.
  • it can be a fixed connection or a detachable connection.
  • Connect, or connect in one piece It can be a mechanical connection or an electrical connection.
  • It can be directly connected, or indirectly connected through an intermediate medium, and it can be a communication between two elements or an interaction relationship between two elements.
  • the "on” or “under” of the first feature of the second feature may include the first and second features in direct contact, or may include the first and second features Not in direct contact but through other features between them.
  • “above”, “above” and “above” the second feature of the first feature include the first feature being directly above and obliquely above the second feature, or it simply means that the level of the first feature is higher than the second feature.
  • the “below”, “below” and “beneath” the first feature of the second feature include the first feature directly below and obliquely below the second feature, or it simply means that the level of the first feature is smaller than the second feature.
  • the locking structure 100 of the embodiment of the present application is used to detachably connect the propeller 200 and the power device 300.
  • the locking structure 100 includes a mounting base 10 and a locking assembly 20.
  • the locking assembly 20 includes a movable part 22 and a stop part 24.
  • One of the mounting base 10 and the movable part 22 is used for mechanical coupling with the propeller 200, and the other is used for mechanical coupling with the power device 300.
  • the mounting base 10 is provided with a first coupling portion 12, and the movable member 22 is provided with a second coupling portion 222.
  • the stopper 24 can be movably connected with the movable member 22, and can be switched back and forth between a locked position and an unlocked position.
  • the stopper 24 may be provided on the mounting base 10 or on the hub 210 of the propeller 200.
  • the stopper 24 and the mounting base 24 form an independent quick-release assembly;
  • the stopper 24 and The movable part 22 forms an independent quick-release assembly.
  • the stopper 24 When the stopper 24 is in the locked position, the stopper 24 abuts at least one of the first coupling portion 12 and the second coupling portion 222, so that the first coupling portion 12 and the second coupling portion 222 are coupled and connected.
  • the stopper 24 When the stopper 24 is in the unlocked position, the stopper 24 provides a movable space for at least one of the first coupling portion 12 and the second coupling portion 222 so that the first coupling portion 12 and the second coupling portion 222 can be separated.
  • the movable member 22 is mechanically coupled with the propeller 200
  • the mounting base 10 is mechanically coupled with the power device 300.
  • Mechanical coupling may refer to the two directly fixedly connected, indirectly fixedly connected through other components, or detachably connected.
  • the fixed connection includes integral molding or multiple components assembled together.
  • the mounting base 10 may be fixedly installed on the power device 300 by a fixing member, which includes fixing elements such as screws and pins.
  • the power device 300 may be a motor, and the motor may be an outer rotor motor or an inner rotor motor.
  • the mounting base 10 is installed on the rotor of the motor and can rotate with the following rotor. In this way, the locking structure 100 can drive the propeller 200 to rotate when the power device 300 rotates.
  • the movable part 22 may be mechanically coupled with the power device 300
  • the mounting base 10 may be mechanically coupled with the propeller 200.
  • the stopper 24 may be provided on the hub 210 of the propeller 200. Specifically, in the illustrated embodiment, the stopper 24 is slidably provided on the hub 210 of the propeller 200. Specifically, the middle of the hub 210 of the propeller 200 is provided with a through hole, and the middle of the stopper 24 passes through the through hole of the hub 210 and is slidable in the through hole of the hub 210. The through hole extends along the rotation axis parallel to the hub 210 of the propeller 200.
  • the stopper 24 may be provided on the mounting base 10. Please refer to FIGS. 23 and 24. Specifically, in the illustrated embodiment, the stopper 24 is slidably mounted on the mounting base 10. Specifically, the mounting base 10 is provided with a guide post 10 a, and the stopper is slidably sleeved on the guide post 10 a of the mounting base 10.
  • the guide post 10a may be a motor shaft, or the guide post 10a may be a convex post extending parallel to the rotation axis of the hub 210 of the propeller 200.
  • one of the mounting base 10 and the movable part 22 is the rotor shell of the motor or a component that rotates with the rotor of the motor, and the other is the hub 210 of the propeller 200 or the hub 210. There are no restrictions on the specific setting of the components that rotate together.
  • the locking structure 100 includes a locked state and an unlocked state. Please refer to FIGS. 1 to 5 and 11 to 15, when the locking structure 100 is in the locked state, the stopper 24 is in the locked position, and the stopper 24 abuts the second coupling portion 222 so that the first coupling portion 12 and The second coupling portion 222 is combined and connected to connect the movable part 22 and the mounting base 10. At this time, the stopper 24 abuts the movable part 22 to restrict the movement of the movable part 22. Please refer to FIGS. 6-10 and 16-20.
  • the stopper 24 When the locking structure 100 is in the unlocked state, the stopper 24 is in the unlocked position, and the stopper 24 is separated from the second coupling portion 222 to provide the second coupling portion 222 Activity space. As a result, the movable member 22 can be separated from the mounting base 10, and the propeller 200 is in a detachable state. In other embodiments, when the stopper 24 is in the locked position, it can resist the first coupling portion 12 or simultaneously the first coupling portion 12 and the second coupling portion 222. When the stopper 24 is in the unlocked position, it can provide a movable space for the movement of the first joining portion 12 or the movement of the first joining portion 12 and the second joining portion 222.
  • the stopper 24 when the propeller 200 is installed, the stopper 24 can be moved to the unlocked position, and the propeller 200 can be installed in the mounting base 10 so that the second coupling portion 222 of the movable member 22 and the second joint 222 of the mounting base 10 A coupling part 12 cooperates, and then the stopper 24 returns to the locked position, and the propeller 200 is locked against the movable part 22.
  • the stopper 24 can be moved to the unlocked position.
  • the movable member 22 can be moved, and the second coupling portion 222 of the movable member 22 can be separated from the first coupling portion 12 of the mounting seat 10, so that the propeller 200 can be separated. Remove from the mounting base 10.
  • the stopper 24 since the stopper 24 is in the locked position and the unlocked position, the first coupling portion 12 and the second coupling portion 222 can be connected and separable respectively. In this way, when disassembling the propeller 200 and the power unit 300, only need to control the position of the stopper 24 to achieve locking and unlocking, without rotating the propeller and/or the power unit 300, which facilitates the disassembly and assembly of the propeller 200 and the power unit 300 process.
  • the first coupling portion 12 is provided with protrusions and/or depressions
  • the second coupling portion 222 is provided with depressions and/or protrusions.
  • the protrusion is at least partially contained in the recess.
  • first joining portion 12 and the second joining portion 222 are connected through the cooperation of the protrusion and the recess, and the protrusion and the recess can be fitted with each other.
  • first coupling portion 12 is provided with recesses
  • second coupling portion 222 is provided with protrusions.
  • the first coupling portion 12 may be provided with protrusions
  • the second coupling portion 222 may be provided with recesses.
  • the first coupling portion 12 is provided with protrusions and depressions
  • the second coupling portion 222 is provided with depressions and protrusions.
  • the movement of the stopper 24 includes sliding or rotating.
  • the stopper 24 can be switched back and forth between the locked position and the unlocked position by sliding or rotating.
  • the stopper 24 can slide along the axial direction of the propeller 200 to resist or disengage the second coupling portion 222.
  • the stopper 24 can rotate about the central axis of the propeller 200 as the rotation axis 228.
  • the mounting seat 10 is provided with a threaded hole
  • the stopper 24 is provided with a threaded part that matches with the threaded hole.
  • the hub 210 of the propeller 200 is provided with a threaded hole
  • the stopper 24 is provided with a threaded part matching the threaded hole. The stopper 24 rotates with the central axis of the propeller 200 as the rotating shaft 228 so that the threaded part and the threaded hole are tightened or loosened to resist or disengage the second coupling part 222.
  • the mounting base 10 is provided with a receiving groove 14.
  • the stopper 24 is at least partially located in the receiving groove 14, and the stopper 24 can move in the receiving groove 14.
  • the receiving slot 14 provides a movable space for the stopper 24 to move, so that the stopper 24 can resist the second coupling portion 222 or separate from the second coupling portion 222.
  • an opening 16 is opened at the top of the receiving groove 14.
  • the movable member 22 penetrates through the opening 16, and the edge of the opening 16 is provided with a downward slope 18.
  • the edge of the opening 16 of the mounting seat 10 is provided with a downwardly inclined inclined surface 18, so that the upper end of the receiving groove 14 has a larger radial dimension, which is convenient for the movable part 22 to pass through the opening 16 so that the movable part 22 is at least partially located in the receiving groove. 14 in.
  • the movable part 22 is mechanically coupled with the propeller 200.
  • the inclined surface 18 functions as a guide, that is, the movable member 22 can slide into the receiving groove 14 along the inclined surface 18.
  • the propeller 200 is provided with an opening 230.
  • the opening 230 is used to provide a space for operating the movable part 22.
  • the opening 230 can be inserted into a tool to operate the movable part 22.
  • the opening 230 is opened in the hub 210.
  • a tool can be inserted into the inclined surface 18 from the opening 230 to push the movable member 22 away, thereby separating the first coupling portion 12 from the second coupling portion 222.
  • the movable member 22 has elasticity.
  • the stopper 24 abuts at least one of the second coupling portion 222 and the first coupling portion 12, it can restrict at least one of the second coupling portion 222 and the first coupling portion 12 from being elastically deformed.
  • the second coupling portion 222 and/or the first coupling portion 12 provide elastic force so that the stopper 24 can resist the movable part 22 to limit the movement of the movable part 22.
  • the stopper 24 abuts the second coupling portion 222, and the second coupling portion 222 can be elastically deformed. In other embodiments, the stopper 24 abuts the first coupling portion 12, and the first coupling portion 12 can be elastically deformed. Of course, it is also possible that the stopper 24 simultaneously resists the first joining portion 12 and the second joining portion 222, and both the first joining portion 12 and the second joining portion 222 can be elastically deformed.
  • the movable member 22 is used for fixed connection with the propeller 200. In the example of FIGS. 11-20, the movable part 22 is used to movably connect with the propeller 200.
  • the movable member 22 includes a first member 224 and a second member 226 that are connected.
  • the stopper 24 When the stopper 24 is in the locked position, the stopper 24 abuts one of the first member 224 and the second member 226 to connect the first joining portion 12 and the second joining portion 222 together.
  • the stopper 24 When the stopper 24 is in the unlocked position, the stopper 24 abuts the other of the first member 224 and the second member 226 to separate the first joining portion 12 and the second joining portion 222.
  • the second piece 226 can slide into the receiving slot 14 along the inclined surface 18.
  • the second member 226 includes the second coupling portion 222.
  • the first member 224 includes the second coupling portion 222.
  • the stopper 24 when the stopper 24 is in the locked position, in the example of FIG. 5, the stopper 24 abuts the second member 226 to connect the first coupling portion 12 and the second coupling portion 222; In the example, the stopper 24 abuts the first member 224 to connect the first joining portion 12 and the second joining portion 222 together.
  • the stopper 24 is in the unlocked position, in the example of FIG. 10
  • the stopper 24 abuts the first piece 224 to separate the first joining portion 12 and the second joining portion 222; in the example of FIG. 20, the stop The stopper 24 abuts the second member 226 to separate the first coupling portion 12 and the second coupling portion 222.
  • a rotating shaft 228 is formed at the joint of the first piece 224 and the second piece 226.
  • the stopper 24 is used to drive the movable member 22 to rotate around the rotating shaft 228 when switching back and forth between the locked position and the unlocked position.
  • the movable member 22 can be moved through rotation.
  • the movable member 22 can be moved by elastic deformation, as shown in FIGS. 1 to 10.
  • the movable member 22 can also be moved by sliding.
  • the locking assembly 20 includes a mount 26.
  • the mounting member 26 is provided with a mounting hole 262, and the stop member 24 is penetrated with a mounting hole 262.
  • the stopper 24 penetrates the mounting hole 262 of the mounting member 26, and the mounting member 26 can guide the movement of the stopper 24.
  • the stopper 24 can slide or rotate on the mounting member 26.
  • the mounting part 26 and the movable part 22 are integrally connected. More specifically, the mounting member 26 and the movable member 22 are integrated with the hub 210 of the propeller 200.
  • the locking structure 100 includes a retaining member 30 for keeping the stopper 24 in the locked position or the unlocked position.
  • the holding member 30 is connected to the mounting member 26.
  • the holding member 30 includes at least one of the following structures: an elastic member 32 and a magnetic member. That is, the holding member 30 may only include the elastic member 32, may only include the magnetic member, or may include both the elastic member 32 and the magnetic member.
  • the elastic member 32 can use its own elastic force to keep the stopper 24 in the locked position or the unlocked position.
  • the magnetic parts can use the magnetic poles of the same name to repel each other, and the principle that the magnetic poles of different names are mutually attracted to keep the stopper 24 in the locked position or the unlocked position.
  • the retaining member 30 includes an elastic member 32. One end of the elastic member 32 abuts the mounting member 26, and the other end abuts the stop member 24 to keep the stop member 24 in the locked position or the unlocked position.
  • the wall of the mounting hole 262 is provided with a receiving space 264
  • the top of the stopper 24 is provided with a first bump 242
  • the elastic member 32 is partially received in the receiving space 264.
  • the elastic member 32 abuts the bottom surface of the receiving space 264 and the bottom surface of the first protrusion 242 to keep the stopper 24 in the locked position or the unlocked position.
  • the elastic member 32 may be a compression spring, and the elastic member 32 keeps the stopper 24 in the locked position.
  • the elastic member 32 can be compressed by pressing the first protrusion 242 on the top of the stopper 24 , The stopper 24 is switched from the locked position to the unlocked position.
  • the elastic member 32 can be a tension spring, and the elastic member 32 can keep the stopper 24 in the unlocked position.
  • the first protrusion 242 on the top of the stopper 24 can be pulled up to stretch the elastic member 32.
  • a spacer is added between the first protrusion 242 and the movable part 22 or the mounting part 26 to switch the stopper 24 from the unlocked position to the locked position.
  • the bottom of the stopper 24 is provided with a second protrusion 244, and the elastic member 32 abuts the bottom surface of the mounting member 26 and the top surface of the second protrusion 244 to keep the stopper 24 in the locked position Or unlock position.
  • the elastic member 32 is located in the receiving groove 14 of the mounting base 10.
  • the elastic member 32 may be a compression spring, and the elastic member 32 may keep the stopper 24 in the unlocked position.
  • the first protrusion 242 on the top of the stopper 24 can be pulled up to compress the elastic member 32 and A spacer is added between the first protrusion 242 and the movable part 22 to switch the stopper 24 from the unlocked position to the locked position.
  • the elastic member 32 can be a tension spring, and the elastic member 32 can keep the stopper 24 in the locked position.
  • the elastic member 32 can be stretched by pressing the first protrusion 242 on the top of the stopper 24, The stopper 24 is switched from the locked position to the unlocked position.
  • the elastic member 32 is located in the receiving groove 14 of the mounting base 10, and the elastic member 32 abuts the bottom surface of the stopper 24 and the bottom surface of the receiving groove 14 to keep the stopper 24 in the locked position or the unlocked position .
  • the bottom surface of the stopper 24 can be provided with a first mounting post 40
  • the bottom surface of the receiving groove 14 can be provided with a second mounting post 50.
  • Two ends of the elastic member 32 are respectively sleeved on the first mounting post 40 and the second mounting post 50 to prevent the elastic member 32 from being displaced.
  • the interval setting between the first mounting post 40 and the second mounting post 50 must ensure that the stopper 24 can be switched back and forth between the locked position and the unlocked position, or at least one of the first mounting post 40 and the second mounting post 50 can be set It is hollow, so that the first mounting post 40 and the second mounting post 50 can be sleeved with each other to ensure that the stopper 24 can switch back and forth between the locked position and the unlocked position.
  • the elastic member 32 can be a compression spring, and the elastic member 32 can keep the stopper 24 in the locked position.
  • the elastic member 32 can be compressed by pressing the first protrusion 242 on the top of the stopper 24.
  • the stopper 24 is switched from the locked position to the unlocked position.
  • the elastic member 32 can be a tension spring, and the elastic member 32 can keep the stopper 24 in the unlocked position.
  • the first protrusion 242 on the top of the stopper 24 can be pulled up to stretch the elastic member 32.
  • a spacer is added between the first protrusion 242 and the movable part 22 to switch the stopper 24 from the unlocked position to the locked position.
  • the locking assembly 20 includes a connector.
  • the connecting piece connects the stop piece 24 and the movable piece 22, and the stop piece 24 is used to drive the movable piece 22 to move through the connecting piece when switching back and forth between the locked position and the unlocked position to make the first joining portion 12 and the second joining portion 222 Combine connection and separation.
  • the stopper 24 is connected to the movable member 22 through the connecting member, and the stopper 24 drives the movable member 22 to move through the connecting member.
  • the mounting base 10 and the propeller 200 will cooperate with other structures to transmit the torque of the power device 300.
  • the mounting base 10 is provided with a positioning protrusion
  • the locking assembly 20 is provided with a positioning protrusion.
  • a matching positioning groove, or a positioning groove is provided on the mounting base 10
  • the locking assembly 20 is provided with a positioning protrusion that matches the positioning groove, and the positioning protrusion is matched with the positioning groove to transmit torque.
  • the second coupling portion 222 of the movable member 22 and the first coupling portion 12 of the mounting seat 10 cooperate to transmit only the pulling force of the propeller 200.
  • the propeller 200 in the embodiment of the present application is used to provide flight power for the drone 1000.
  • the propeller 200 includes a movable part 22, a stopper 24 and a propeller hub 210 connected with the stopper 24.
  • the movable part 22 is used to cooperate with the mounting seat 10 of the power device 300.
  • the mounting base 10 is provided with a first coupling portion 12, and the movable member 22 is provided with a second coupling portion 222.
  • the stopper 24 is movably provided on the movable member 22 and can be switched back and forth between the locked position and the unlocked position.
  • the stopper 24 When the stopper 24 is in the locked position, the stopper 24 abuts at least one of the first coupling portion 12 and the second coupling portion 222, so that the first coupling portion 12 and the second coupling portion 222 are coupled and connected.
  • the stopper 24 When the stopper 24 is in the unlocked position, the stopper 24 provides a movable space for at least one of the first coupling portion 12 and the second coupling portion 222 so that the first coupling portion 12 and the second coupling portion 222 can be separated.
  • the stopper 24 since the stopper 24 is in the locked position and the unlocked position, the first coupling portion 12 and the second coupling portion 222 can be coupled, connected, and separable, respectively. In this way, when disassembling the propeller 200 and the power unit 300, only need to control the position of the stopper 24 to achieve locking and unlocking without rotating the propeller and/or power unit 300, which facilitates the disassembly and assembly of the propeller 200 and the power unit 300 process.
  • the movable member 22, the stopper 24, and the mounting seat 10 are the movable member 22, the stopper 24, and the mounting seat 10 in the locking structure 100 of the above embodiment.
  • the movable part 22 is fixedly connected to the hub 210 or movably connected.
  • the propeller 200 further includes the mounting member 26, the holding member 30, and the connecting member in the locking structure 100 of the above embodiment.
  • the propeller 200 also includes a blade 220 connected to a hub 210.
  • the power device 300 of the embodiment of the present application includes a rotor and a mounting seat 10 that rotates with the rotor.
  • the mounting base 10 is used to cooperate with the movable part 22 of the propeller 200.
  • the mounting base 10 is provided with a first coupling portion 12, and the movable member 22 is provided with a second coupling portion 222.
  • the propeller 200 includes a movable part 22 and a stopper 24.
  • the stopper 24 is movably provided on the movable member 22 and can be switched back and forth between the locked position and the unlocked position.
  • the stopper 24 When the stopper 24 is in the locked position, the stopper 24 abuts at least one of the first coupling portion 12 and the second coupling portion 222, so that the first coupling portion 12 and the second coupling portion 222 are coupled and connected.
  • the stopper 24 When the stopper 24 is in the unlocked position, the stopper 24 provides a movable space for at least one of the first coupling portion 12 and the second coupling portion 222 so that the first coupling portion 12 and the second coupling portion 222 can be separated.
  • the stopper 24 since the stopper 24 is in the locked position and the unlocked position, the first coupling portion 12 and the second coupling portion 222 can be coupled, connected and separable, respectively. In this way, when disassembling the propeller 200 and the power unit 300, only need to control the position of the stopper 24 to achieve locking and unlocking, without rotating the propeller and/or the power unit 300, which facilitates the disassembly and assembly of the propeller 200 and the power unit 300 process.
  • the movable member 22, the stopper 24, and the mounting seat 10 are the movable member 22, the stopper 24, and the mounting seat 10 in the locking structure 100 of the above embodiment.
  • the propeller 200 further includes the mounting member 26, the holding member 30, and the connecting member in the locking structure 100 of the above embodiment.
  • the explanations and beneficial effects of the locking structure 100 of the above embodiment are also applicable to the power device 300 of the embodiment of the present application. To avoid redundancy, detailed explanations are omitted here.
  • the power assembly of the embodiment of the present application includes a power plant 300, a propeller 200, and the locking structure 100 of the above embodiment.
  • the mounting base 10 is installed on the power plant 300, and the movable part 22 is connected with the propeller 200.
  • the stopper 24 since the stopper 24 is in the locked position and the unlocked position, the first coupling portion 12 and the second coupling portion 222 can be coupled, connected and separable, respectively. In this way, when disassembling the propeller 200 and the power unit 300, only need to control the position of the stopper 24 to achieve locking and unlocking, without rotating the propeller and/or the power unit 300, which facilitates the disassembly and assembly of the propeller 200 and the power unit 300 process.
  • the drone 1000 of the embodiment of the present application includes a fuselage 400 and an arm 500.
  • the arm 500 is connected to the fuselage 400, and the power assembly of the above embodiment is installed on the arm 500.
  • the stopper 24 since the stopper 24 is in the locked position and the unlocked position, the first coupling portion 12 and the second coupling portion 222 can be coupled, connected and separable, respectively. In this way, when disassembling the propeller 200 and the power unit 300, only need to control the position of the stopper 24 to achieve locking and unlocking, without rotating the propeller and/or the power unit 300, which facilitates the disassembly and assembly of the propeller 200 and the power unit 300 process.
  • the drone 1000 includes a plurality of arms 500, and each arm 500 is equipped with a power unit including a propeller 200.
  • the power device 300 of the power unit rotates, the propeller 200 can be driven to rotate, thereby being the drone 1000.
  • the drone 1000 is a multi-rotor aircraft.
  • the number of power components is multiple, including a first power component 610 and a second power component 620.
  • the power device 300 of the first power component 610 is used to drive the propeller 200 to rotate in a clockwise direction
  • the power device 300 of the second power component 620 is used to drive the propeller 200 to rotate in a counterclockwise direction.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Seats For Vehicles (AREA)
  • Motor Power Transmission Devices (AREA)

Abstract

La présente invention concerne une structure de verrouillage (100), une hélice (200), un dispositif d'alimentation (300), un ensemble d'alimentation et un véhicule aérien sans pilote (1000). La structure de verrouillage (100) comprend une base de montage (10) et un ensemble de verrouillage (20). L'ensemble de verrouillage (20) comprend un élément mobile (22) et un élément de butée (24). La base de montage (10) ou l'élément mobile (22) est utilisé(e) pour être mécaniquement accouplé(e) à l'hélice (200), et l'autre est utilisé(e) pour être accouplé(e) mécaniquement au dispositif d'alimentation (300). La base de montage (10) est pourvue d'une première partie de combinaison (12) et l'élément mobile (22) est pourvu d'une second partie de combinaison (222). L'élément de butée (24) est relié de façon mobile à l'élément mobile (22) et peut commuter entre une position de verrouillage et une position de déverrouillage. Lorsque l'élément de butée (24) est dans la position de verrouillage, l'élément de butée (24) vient en butée contre la première partie de combinaison (12) et/ou la seconde partie de combinaison (222) de telle sorte que la première partie de combinaison (12) et la seconde partie de combinaison (222) sont combinées et reliées l'une à l'autre. Lorsque l'élément de butée (24) est dans la position de déverrouillage, l'élément de butée (24) fournit un espace mobile destiné à la première partie de combinaison (12) et/ou la seconde partie de combinaison de telle sorte que la première partie de combinaison (12) et la seconde partie de combinaison (222) sont séparables l'une de l'autre.
PCT/CN2019/098923 2019-08-01 2019-08-01 Structure de verrouillage, hélice, dispositif d'alimentation, ensemble d'alimentation, et véhicule aérien sans pilote WO2021017004A1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
CN201980032122.XA CN112119009A (zh) 2019-08-01 2019-08-01 锁定结构、螺旋桨、动力装置、动力组件和无人机
PCT/CN2019/098923 WO2021017004A1 (fr) 2019-08-01 2019-08-01 Structure de verrouillage, hélice, dispositif d'alimentation, ensemble d'alimentation, et véhicule aérien sans pilote

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/CN2019/098923 WO2021017004A1 (fr) 2019-08-01 2019-08-01 Structure de verrouillage, hélice, dispositif d'alimentation, ensemble d'alimentation, et véhicule aérien sans pilote

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WO2021017004A1 true WO2021017004A1 (fr) 2021-02-04

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