CN208233359U - Power suit - Google Patents

Power suit Download PDF

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Publication number
CN208233359U
CN208233359U CN201820655756.3U CN201820655756U CN208233359U CN 208233359 U CN208233359 U CN 208233359U CN 201820655756 U CN201820655756 U CN 201820655756U CN 208233359 U CN208233359 U CN 208233359U
Authority
CN
China
Prior art keywords
propeller
motor
card slot
blade
mounting base
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Fee Related
Application number
CN201820655756.3U
Other languages
Chinese (zh)
Inventor
胡奔
张圣鑫
莫颂权
王坤殿
李璐鑫
于建方
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shenzhen Dajiang Innovations Technology Co Ltd
Original Assignee
Shenzhen Dajiang Innovations Technology Co Ltd
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 Shenzhen Dajiang Innovations Technology Co Ltd filed Critical Shenzhen Dajiang Innovations Technology Co Ltd
Priority to CN201820655756.3U priority Critical patent/CN208233359U/en
Application granted granted Critical
Publication of CN208233359U publication Critical patent/CN208233359U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

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  • Connection Of Plates (AREA)

Abstract

The utility model provides a kind of power suit.The power of the utility model is set with, including at least one of mounting structure for propeller and propeller and motor, propeller are connected on motor by mounting structure for propeller;Wherein, mounting structure for propeller includes mounting base, locking piece and elastic component;Mounting base is fixed on the end face of motor, and mounting base passes through the motor shaft of motor, mounting base is used for and propeller rotation engaging, elastic component is connected with locking piece, and elastic component is used to apply elastic force to locking piece along the axial of motor shaft, so that locking piece is at least partly blocked on the outside of the engagement direction of propeller;Propeller includes the connection component and at least one blade for being mounted on the motor shaft of motor, and blade is arranged on connection component, and connection component includes for the circular connector with the mounting structure for propeller rotation engaging on motor.The utility model can be realized the reliable installation connection of propeller, and dismount relatively simple.

Description

Power suit
Technical field
The utility model relates to aircraft fields more particularly to a kind of power to be set with.
Background technique
With the continuous development of science and technology, the automatic control equipments such as unmanned vehicle more and more appear in the work and life of people In work.
Currently, unmanned vehicle usually utilizes motor driven propeller rotational, and by the rotary squeezing of propeller blade Air, so that unmanned vehicle be driven to realize lifting and flight operation.Wherein, in order to propeller to be fixed on to the motor shaft of motor On, it can be by the way of being threadedly coupled.Specifically, propeller can be pressed on using the threaded connection of nut and motor shaft On the motor shaft of motor, it is also possible to the axis hole of propeller threaded hole is made, and screws and realize connection on motor shaft.
However, current propeller connection type, threaded fastener may generate loosening, cause to penetrate paddle phenomenon, safety Property is lower.
Utility model content
The utility model provides a kind of power suit, can be realized the reliable installation connection of propeller, and dismounts more simple Just.
In a first aspect, the utility model provides a kind of mounting structure for propeller, for propeller to be detachably arranged in On motor, including mounting base, locking piece and elastic component;Mounting base is fixed on the end face of motor, and mounting base passes through motor Motor shaft, mounting base is used for and propeller rotation engaging, and elastic component is connected with locking piece, and elastic component is used for the axis along motor shaft Apply elastic force to locking piece, so that locking piece is at least partly blocked on the outside of the engagement direction of propeller.
Optionally, mounting base is the annular element for being disposed around the outside of motor shaft, and mounting base is circumferentially arranged at least one A first holding part, the first holding part is used for and propeller rotation engaging.
Optionally, the first holding part outwardly protrudes the outer wall in mounting base;Alternatively, the first holding part is inwardly projecting in installation The inner wall of seat.
Optionally, at least two first holding parts are provided in mounting base, and at least two first holding part intervals are arranged.
Optionally, at least two first holding parts are symmetrical relative to the axial centre of motor shaft.
Optionally, all first holding parts are respectively positioned on the sustained height along axial direction of mounting base.
Optionally, propeller has radially projecting snap-in structure, and the circumferential direction along mounting base is formed on the first holding part The first card slot extended, the first card slot is used for and snap-in structure rotation engaging.
Optionally, the first holding part is at least two, and the first card slot on different first holding parts has different sizes.
Optionally, the first card slot is unidirectional card slot;Alternatively, the first holding part is two, and the first card slot is two-way card slot.
Optionally, the first card slot includes the first rib on the first holding part, and first gear edge mounting base is circumferentially prolonged It stretches, when propeller and the rotation of the first card slot engage, the first rib is located at the side far from the motor of snap-in structure.
Optionally, the first card slot further includes the second rib connected with the first rib, and the second rib is located at the first rib One end and along the axially projecting of motor shaft, the second rib is for limiting rotation angle of the snap-in structure in the first card slot.
Optionally, each second rib is respectively positioned on the same end of corresponding first rib.
Optionally, mounting base has to the support division protruded far from motor drive direction, and support division is for supporting propeller.
Optionally, support division is the sleeve being set on the outside of motor shaft, and the end of support division is for supporting propeller.
Optionally, it is arranged fluted in mounting base, locking piece is located in groove and can be along the axial movement of motor shaft.
Optionally, the notch of groove is towards motor.
Optionally, locking piece has at least one for backstop in the stopper section of the notch of the first card slot.
Optionally, support division is the end face 12 away from motor side of mounting base.
Optionally, stopper section backstop is between two neighboring first holding part.
Optionally, stopper section backstop mutually abuts between stopper section and the first holding part in the notch of the first card slot.
Optionally, stopper section first holding part adjacent with the first holding part of the first card slot is formed mutually abuts.
Optionally, first holding part adjacent with the first holding part of the first card slot is formed has first wedge diagonally downward Shape face, the second lozenges being mutually matched with the first lozenges is provided on stopper section, and stopper section is acted in the elastic force of elastic component When abutting with the first holding part with the first lozenges, the first lozenges and the second lozenges are bonded to each other to limit blocking portion The position of notch relative to the first card slot.
Optionally, stopper section has multiple, and in the circumferentially-spaced distribution of locking piece.
Optionally, locking piece also has along the hand-held part of motor shaft extended radially out.
Optionally, the number of hand-held part is even number, and is symmetrical arranged relative to motor shaft.
Optionally, handgrip part is in groove.
Optionally, anti-skid structure is provided on hand-held part.
Optionally, one end of elastic component and the end face of motor connect, and the other end is connected with locking piece.
Optionally, elastic component and motor shaft coaxial arrangement.
Optionally, elastic component is spring.
Optionally, elastic component is tower-shaped spring.
Optionally, elastic component is Spring capable of diameter varying.
Second aspect, the utility model provide a kind of propeller, including the connection for being mounted on the motor shaft of motor Component and at least one blade, blade are arranged on connection component, and connection component includes for installing with the propeller on motor The circular connector of structure rotation engaging.
Optionally, at least one second holding part that circular connector has annular wall and is circumferentially arranged along annular wall, the Two holding parts are used for and mounting structure for propeller rotation engaging.
Optionally, the second holding part outwardly protrudes the outer wall in annular wall;Alternatively, the second holding part is inwardly projecting in annular The inner wall of wall.
Optionally, at least two second holding parts, and at least two second holding part intervals are provided on circular connector Setting.
Optionally, at least two second holding parts are symmetrical relative to the axial centre of circular connector.
Optionally, all second holding parts are respectively positioned on the sustained height along axial direction of circular connector.
Optionally, the snap-in structure of the radially protruding along motor shaft, the second holding part are provided on mounting structure for propeller Upper the second card slot for forming the circumferentially extending along circular connector, the second card slot is used for and snap-in structure rotation engaging.
Optionally, the second holding part is at least two, and the second card slot on different second holding parts has different sizes.
Optionally, the second card slot includes the third rib on the second holding part, third gear edge circular connector When circumferentially extending, snap-in structure and the rotation engaging of the second card slot, third rib is located at the side for closing on motor of snap-in structure.
Optionally, card slot further includes the fourth gear side connected with third rib, and fourth gear side is located at one end of third rib And along the axially projecting of circular connector, fourth gear side is for limiting rotation angle of the snap-in structure in the second card slot.
Optionally, each fourth gear side is respectively positioned on the same end of corresponding third rib.
Optionally, the axle sleeve for the motor axis connection with motor is additionally provided on circular connector.
Optionally, the axis hole edge of axle sleeve has chamfering.
Optionally, there is the second support division for protrude towards motor drive direction on circular connector, the second support division for from The motor shaft of motor axially supports mounting structure for propeller.
Optionally, the second support division is staggered in crosswise in the inside of circular connector.
Optionally, clamping part is provided on circular connector, the root of blade is fixed on the holder portion.
Optionally, connection component further includes upper clamping piece, and upper clamping piece is used to clamp the root of blade jointly with clamping part.
It optionally, is to be rotatably connected between blade and connection component.
Optionally, the root of blade has pin hole, and blade can be rotated around pin hole, with rotation to folded state or work shape State.
Optionally, connection component further includes that the matched locating piece of pin hole, upper clamping piece are provided with first positioning hole, clamping Portion is equipped with second location hole, the position reciprocal correspondence of first positioning hole and second location hole, and locating piece sequentially passes through the first positioning Hole, pin hole and second location hole, so that connection component and blade are fixed together.
Optionally, locating piece is pin shaft, plug screws or at least one of threaded fastener.
Optionally, second location hole is that unthreaded hole, threaded hole or counter sink are at least one.
Optionally, upper clamping piece includes the ontology with cavity and the cushion being arranged in cavity, and first positioning hole is set It sets on cushion.
Optionally, the quantity of cavity and cushion is identical as the quantity of blade.
Optionally, cushion is silicone rubber pad.
Optionally, locating piece is pin shaft, is interference fitted between first positioning hole and locating piece.
Optionally, locating piece is pin shaft, and the diameter of one end of the insertion first positioning hole of locating piece is greater than its of pin shaft The diameter of remaining part point.
Optionally, it is attached between upper clamping piece and circular connector by threaded fastener.
Optionally, locating piece is threaded fastener, is connected between upper clamping piece and circular connector by locating piece, and fixed Position part has smooth outer wall with the position of shaft hole matching.
Optionally, it is provided at least one boss parallel with motor shaft on upper clamping piece, is provided with threaded hole on boss, Mounting hole corresponding with threaded hole is provided on circular connector, threaded fastener is protruded into inside threaded hole by mounting hole, with Clamping piece and circular connector in connection.
Optionally, at least one between upper clamping piece and the root of blade and between clamping part and the root of blade It is provided with gasket, gasket and blade fitting.
Optionally, gasket is smooth abrasion-proof part.
Optionally, gasket is Teflon gasket.
Optionally, at least one limiting section is provided on upper clamping piece, limiting section is used to limit the rotational angle of blade.
Optionally, the bottom surface of upper clamping piece is arranged in limiting section, and protrudes towards motor.
Optionally, each blade is correspondingly arranged there are two limiting section, and two limiting sections are separately positioned on the rotation of blade Turn the two sides in direction.
Optionally, the quantity of blade is two, and two blades are symmetrical arranged.
The third aspect, the utility model provide a kind of power suit, including mounting structure for propeller as described above and such as At least one of upper described propeller and motor, propeller are connected on motor by mounting structure for propeller.
Fourth aspect, the utility model provide a kind of unmanned vehicle, including body moves as described above at least one Power suit, body include rack and the horn that connect with rack, and power suit setting is on horn.
The mounting structure for propeller, propeller, power suit and unmanned vehicle of the utility model, mounting structure for propeller For propeller to be detachably arranged in motor.The mounting structure for propeller specifically includes mounting base, locking piece and elasticity Part;Mounting base is fixed on the end face of motor, and mounting base passes through the motor shaft of motor, and mounting base is used for and propeller revotating card It closes, elastic component is connected with locking piece, and elastic component is used to apply elastic force to locking piece along the axial of motor shaft, so that locking piece is extremely Small part is blocked on the outside of the engagement direction of propeller.In this way propeller can rotation engaging by way of and motor realize phase To fixation, while connection is more reliable, can effectively avoid penetrating paddle phenomenon;It dismounts simultaneously relatively simple.
Detailed description of the invention
In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is Some embodiments of the utility model, for those of ordinary skill in the art, in the premise of not making the creative labor property Under, it is also possible to obtain other drawings based on these drawings.
Fig. 1 is the attachment structure schematic diagram of the mounting structure for propeller that the utility model embodiment one provides and motor;
Fig. 2 is the partial structural diagram of the mounting structure for propeller in Fig. 1;
Fig. 3 is the connection structure front view of the mounting structure for propeller that the utility model embodiment one provides and motor;
Fig. 4 is the partial structural diagram of mounting structure for propeller in Fig. 3;
Fig. 5 is the connection structure side view of the mounting structure for propeller that the utility model embodiment one provides and motor;
Fig. 6 is the connection structure top view of the mounting structure for propeller that the utility model embodiment one provides and motor;
Fig. 7 is the structural schematic diagram for another mounting structure for propeller that the utility model embodiment one provides;
Fig. 8 is a kind of front view for propeller that the utility model embodiment two provides;
Fig. 9 is the top view for the propeller that the utility model embodiment two provides;
Figure 10 is the top view for the propeller that the utility model embodiment two provides;
Figure 11 is the partial schematic diagram of connection component part in Figure 10;
Figure 12 is the structural schematic diagram for the connection component that the utility model embodiment two provides;
Figure 13 is the connection schematic diagram of upper clamping piece and blade in the connection component of the offer of the utility model embodiment two;
Figure 14 is the explosive view for the propeller that the utility model embodiment two provides;
Figure 15 is the scheme of installation for the blade that the utility model embodiment two provides;
Figure 16 is structural schematic diagram of the propeller of the offer of the utility model embodiment two when blade folds;
Figure 17 is the structural schematic diagram for another connection component that the utility model embodiment two provides;
Figure 18 is a kind of structural schematic diagram for power suit that the utility model embodiment three provides;
Figure 19 is the structural schematic diagram of the motor in the power suit of Figure 18.
Description of symbols:
1-mounting base;2-locking pieces;3-elastic components;4-blades;5-connection components;6-gaskets;10-motors; 11, the first holding part of 11a, 11b-;12-end faces;13-grooves;20-motor shafts;21-stopper sections;22-hand-held parts; 41-pin holes;51-circular connectors;52-upper clamping pieces;53,53a-threaded fastener;54-pin shafts;100-propellers Mounting structure;111-the first card slot;112-the first lozenges;200-propellers;211-the second lozenges;221-is anti-skidding Line;300-power suit;511-annular walls;512-the second holding part;513-axle sleeves;514-the second support division;515— Clamping part;516-mounting holes;521-boss;522-first positioning holes;523-cushions;524-limiting sections;5121-the Two draw-in groove;5122-third ribs;5123-fourth gear sides;5151-second location holes;A-chamfering.
Specific embodiment
It is practical new below in conjunction with this to keep the objectives, technical solutions, and advantages of the embodiments of the present invention clearer Attached drawing in type embodiment, the technical scheme in the utility model embodiment is clearly and completely described, it is clear that is retouched The embodiment stated is the utility model a part of the embodiment, instead of all the embodiments.Based on the implementation in the utility model Example, every other embodiment obtained by those of ordinary skill in the art without making creative efforts belong to The range of the utility model protection.
Fig. 1 is the attachment structure schematic diagram of the mounting structure for propeller that the utility model embodiment one provides and motor.Fig. 2 It is the partial structural diagram of the mounting structure for propeller in Fig. 1.Fig. 3 is the propeller peace that the utility model embodiment one provides The connection structure front view of assembling structure and motor.Fig. 4 is the partial structural diagram of mounting structure for propeller in Fig. 3.Fig. 5 is this The connection structure side view of mounting structure for propeller and motor that utility model embodiment one provides.Fig. 6 is the utility model reality The mounting structure for propeller of the offer of example one and the connection structure top view of motor are provided.As shown in Figures 1 to 6, the present embodiment provides Mounting structure for propeller, for propeller to be detachably arranged in motor 10.The mounting structure for propeller specifically includes Mounting base 1, locking piece 2 and elastic component 3;Mounting base 1 is fixed on the end face of motor 10, and mounting base 1 passes through the electricity of motor 10 Arbor 20, mounting base 1 is used for and propeller rotation engaging, and elastic component 3 and locking piece 2 connect, and elastic component 3 is used for along motor shaft 20 axial direction applies elastic force to locking piece 2, so that locking piece 2 is at least partly blocked on the outside of the engagement direction of propeller.
Specifically, mounting structure for propeller is implemented for the company between propeller and the motor 10 of unmanned vehicle It connects.The motor 10 of unmanned vehicle can drive propeller rotational, and such propeller can produce upward lift when rotating, because And unmanned vehicle can be driven to realize flight and landing operation.In general, unmanned vehicle can have multiple propellers, thus Correspondingly, mounting structure for propeller generally can also have multiple, and the quantity phase of the quantity of mounting structure for propeller and propeller Together.
In order to drive propeller rotational, motor 10 generally includes stator, rotor and motor shaft 20 etc., wherein motor shaft 20 It can be stretched out from a side end face of motor 10.In general, motor shaft 20 can be fixedly connected with the side end face on motor 10, in this way End face on motor shaft 20 and motor 10 can be rotated relative to 10 ontology of motor, and propeller can be installed by propeller Connection is realized between structure and the rotatable end face of motor 10, and the end face is followed to rotate together.Motor 10 and spiral in this way More reliable power transmission structure is capable of forming between paddle, to adapt to biggish driving moment or higher revolving speed.
It wherein, in order to which propeller to be installed on motor 10, and is dismountable connection type between motor 10, specifically , it include the mounting base 1 being fixed on 10 end face of motor in mounting structure for propeller, and be flexibly connected with mounting base 1 The structures such as locking piece 2 and the elastic component 3 being located in mounting base 1 for driving locking piece 2 to support.Wherein, mounting base 1 is fixed on motor On 10 end faces, thus when the end face rotation of motor 10, mounting base 1 can also be rotated synchronously, to drive propeller to rotate.Mounting base 1 Generally hollow structure, such mounting base 1 can pass through the motor shaft 20 of motor 10 and be fixed on motor 10, make motor shaft 20 The outside of mounting base 1 can be extend out to and propeller is positioned, at the same do not influence motor 10 motor shaft 20 rotation with And power transmission.In addition, in order to fix propeller, it is usually provided with the structures such as protrusion or card slot in mounting base 1, and can be with Engaging is rotated between propeller.In this way by way of rotation engaging, propeller can be from being axially fixed on motor 10.
At work, its own can follow the rotation of mounting base 1 under the drive of motor 10 and synchronize and turned propeller Dynamic, when the revolving speed of propeller is too fast, propeller is possible to be detached from from the position engaged with mounting base 1, to cause to penetrate paddle Phenomena such as, influence the normal flight and safety of unmanned vehicle.And in order to avoid propeller is de- from the position engaged with mounting base 1 From, further include in mounting structure for propeller have locking piece 2 and elastic component 3, and by elastic component 3 elastic force and allow locking piece 2 to support It connects can be on the position of sealed propeller.
Specifically, since mounting base 1 is generally hollow structure, thus locking piece 2 mutually nested with mounting base 1 can be set It sets, e.g. locking piece 2 is arranged in the hollow cavity of mounting base 1 or locking piece 2 is also hollow structure, and is disposed around The outside of mounting base 1.Due to being provided with the structure that can rotate engaging with propeller of protrusion or card slot in mounting base 1, because And relative displacement may be implemented between locking piece 2 and mounting base 1, to be moved to the position with protrusion or the same axial height of card slot It sets, in this way when the snap-in structure of propeller is fixed in mounting base 1 by way of rotation engaging, locking piece 2 can pass through The structure of itself and keep off the outside in protrusion or card slot so that the snap-in structure of propeller is locked part 2 and is stopped, and nothing Method is detached from from the position engaged with protrusion or card slot, so that locking of propeller is completed propeller and installation in clamped position It is relatively fixed between seat 1.
Wherein, locking piece 2 can generally be moved along axial realize of motor shaft 20, so that gear is outside protrusion or card slot Side and the position of locking screw paddle;Either be moved to from protrusion or the different axial position of card slot and release to propeller Limitation locking.When locking piece 2 is located at the different axial positions with protrusion or card slot, at this point, due to convex in mounting base 1 Rise or the outside of card slot do not have locking piece 2 to be blocked, it is thus possible to normally with the snap-in structure revotating card of propeller It closes, or is detached from and engages between the snap-in structure of propeller.Wherein, in order to allow locking piece 2 can freely in motor shaft The movement relative to mounting base 1 is realized in 20 axial direction, and the knot such as groove or evacuation cavity usually can be set in mounting base 1 Structure, to avoid locking piece 2, recurring structure is interfered between mounting base 1 when moving.At this point, locking piece 2 can pass through groove or Person avoids cavity, and along motor shaft 20 radially across in the two sides of mounting base 1, thus mounting base 1 opposite sides simultaneously Realize locking.
Under normal conditions, locking piece 2 should maintain the position for capableing of the snap-in structure of locking screw paddle, so that propeller It is maintained at clamped position, avoids the snap-in structure of propeller from being detached from mounting base and engages.At this point, usually can use elastic component 3 Elastic force by locking piece 2 keep in the position.Specifically, since locking piece 2 is relied on from the movement in 20 axial direction of motor shaft Change the limit state to propeller, thus the elastic force direction of elastic component 3 also can be along the axial direction of motor shaft 20, e.g. court To the direction for deviating from motor side face.Locking piece 2 can be abutted by the elastic force of elastic component 3 or is fixed in mounting base 1 in this way Propeller engagement direction outside, thus allow propeller be locked part 2 be limited in the position being mutually clamped with mounting base 1, And it can not deviate from from the clamped position.
Wherein, due to being rotation engaging between mounting base 1 and propeller, thus the engagement direction of propeller can be along motor The circumferential direction of 10 motor shafts 20, and it is opposite with the direction of rotation of the rotor of motor 10.In this way when elastic component 3 applies elastic force, Elastic component 3 can make locking piece 2 along the axial movement of motor shaft 20 by own resilient, and locking piece 2 is moved along the axial direction of motor shaft 20 It moves to suitable position, the outside along itself direction of rotation of propeller will be blocked in, to allow propeller can not be from the party Engage to the disengaging of mounting base 1.It is connected by way of rotary clamping between propeller and mounting structure for propeller in this way, one Aspect connection is more reliable, is on the other hand also convenient for carrying out the dismounting and replacement operation of propeller.In general, elastic component 3 can be with It is positioned close to the position of 1 central part of mounting base, is e.g. coaxially disposed with motor shaft 20, also can be set close to installation The position of rotation snap-in structure on seat 1.
Optionally, in order to realize rotation engaging with mounting base 1, generally equally have on propeller and mounting base 1 is adapted Clamping structure, and be normally at the propeller hub position of propeller.Propeller can use the clamping structure of itself and realize in this way Rotation between mounting base 1 engages.
In mounting structure for propeller, locking piece 2 positions propeller from the circumferential direction of propeller, thus spiral Paddle can be mounted seat 1 and locking piece 2 is fixed on the position that connection is mutually clamped with mounting base 1 jointly.Thus propeller can be with End face relative to motor 10 is fixed, and when motor 10 rotates, propeller can be rotated with it, while guarantee that inherently safe is reliable Be fixed on motor 10.
Specifically, in order to be connected on motor 10, while rotation engaging completed to propeller, mounting structure for propeller can be with With a variety of different structure types, it is specifically described in detail below.
Optionally, mounting base 1 can be the annular element for being disposed around the outside of motor shaft 20, and mounting base 1 is circumferentially arranged There is at least one first holding part 11, the first holding part 11 is used for and propeller rotation engaging.
Specifically, since mounting base 1 is annular element, thus the motor shaft 20 of motor 10 can be from the sky in 1 center of mounting base Between pass through, and mounting base 1 usually has inner wall or outer wall in a ring, and the clamping structure of such propeller is similarly annular When, the circumferential direction sliding relative to motor shaft 20 can be realized and inner wall with mounting base 1 or outer wall contact, in this way, edge At least one holding part that mounting base 1 is circumferentially arranged can realize that rotation engages between propeller, or under fastening state It rotationally disengages.
Common, since mounting base 1 is annular element, and propeller can be contacted by inner wall with mounting base 1 or outer wall And circumferentially slide, thus as an alternative embodiment, the first holding part 11 can be outwardly protruded in the outer of mounting base 1 Wall.At this point, the clamping structure on propeller can be disposed around the outside of the mounting base 1 of annular, 1 outer wall of mounting base is protruded from this way First holding part 11 can be realized with the clamping structure in outside and is clamped.In the present embodiment, installation is protruded from the first holding part 11 It is illustrated for the outer wall of seat 1.
And as another optional embodiment, the first holding part 11 can the inwardly projecting inner wall in mounting base 1. At this point, mounting base 1 is disposed around the outside of the clamping structure of propeller, and clamping is realized between the clamping structure of inside.Thus Correspondingly, the second holding part can also protrude from the inner wall of mounting base 1, and the clamping knot for being located at 1 inside of mounting base with propeller Structure realizes clamping.
In order to when rotating engaging with propeller, improve the load ability of mounting base 1, the quantity of the first holding part 11 is logical It often can be more than one, at least two first holding parts 11, and at least two first e.g. can be set in mounting base 1 The setting of the interval of holding part 11.For mounting base 1 when realizing rotation engaging, multiple first holding parts 11 can be in mounting base 1 in this way Different parts realize limit engaging to propeller, and 1 stress of mounting base is more dispersed when engaging, it is thus possible to bear biggish power Square.
Optionally, when the first holding part 11 is multiple, multiple first holding parts 11 can be relative to the axis of motor shaft 20 To the setting that is centrosymmetric.In this way connection of the mounting base 1 between realization and propeller when, torque can uniformly be passed to Each first holding part 11 keeps stress of the mounting base 1 in circumferential all directions more balanced, improves the knot of mounting base 1 Structure reliability.
When the first holding part 11 is multiple, since the mode engaged between mounting base 1 and propeller for rotation realizes company It connects, thus for the ease of allowing propeller circumferentially smoothly to rotate relative to mounting base 1, as an alternative embodiment, All first holding parts 11 can be respectively positioned on the sustained height along axial direction of mounting base 1.Due to the equal position of all first holding parts 11 In on the sustained height of mounting base 1, such first holding part 11 can be collectively formed in the circumferential direction of mounting base 1 positioned at sustained height Snap-latch surface.Propeller and mounting base 1 can realize opposite sliding and be rotated by the snap-latch surface, be mutually clamped with turning to Position.
As one of optional snap fit, there can be the snap-in structure along itself radially protruding on propeller, and Correspondingly, can form the first card slot 111 of the circumferentially extending along mounting base 1 on the first holding part 11, the first card slot 111 is used for It rotates and engages with snap-in structure.
Specifically, snap-in structure on propeller can along the radially outward or inwardly projecting of propeller, and correspondingly, The first holding part 11 in mounting base 1 also the inwardly projecting inner wall in mounting base 1 can be outwardly protruded either in mounting base 1 therewith Outer wall.And the first card slot 111 circumferentially extended along mounting base 1 can be formed on the first holding part 11, the first card slot 111 Extending direction and propeller it is axially vertical, thus the snap-in structure of propeller can be moved to transmission shafts upwards with The position that mounting base 1 is overlapped, and rotates snap-in structure, is caught in snap-in structure in the first card slot 111, and with the first card slot 111 Between realize engaging.
In general, the first card slot 111 can circumferentially surround on a certain axial position on the outside of motor shaft 20, and using certainly Snap-in structure on propeller is also limited at the position relative to motor shaft 20 by body cell wall.In addition, on the first card slot 111 Stop configurations are generally also provided with, when being in this way that the snap-in structure of propeller moves rotation along the first card slot 111, can be existed by backstop Relative in a certain circumferential angle of mounting base 1, to realize the positioning to propeller in the axial direction.
It optionally, can on the first different holding parts when the quantity of the first holding part 11 is two or more Various sizes of first card slot is arranged.Illustratively, the size of the first card slot 111 is different, can be the outer of the first card slot 111 Edge or inner edge radius difference etc..In this way when the snap-in structure on propeller is installed on mounting structure for propeller, due to One card slot 111 can engage with snap-in structure, thus various sizes of first card slot can also correspond to the engaging knot for being connected to propeller Various sizes of part on structure.Various sizes of first card slot can be allowed to be located at not according to the rotation direction difference of propeller in this way With direction and position, when the rotation direction mistake of propeller, e.g. positive paddle (CW) and for installing anti-paddle (CCW) propeller peace Assembling structure engage when, just can not with each first card slot, 111 snap-fit, to play foolproof function.
Common, the first card slot 111 can be unidirectional card slot, and the side of extending direction is notch, and extending direction The other side is the slot bottom for backstop snap-in structure.After the snap-in structure of propeller is protruded into from the notch of the first card slot 111 in this way, It can be slided along the extending direction of the first card slot 111, until being abutted with the slot bottom of the first card slot 111.
In addition, when the quantity of the first holding part 11 is only two, the first card slot 111 or two-way card slot, at this point, First holding part 11 and the first card slot 111 are only used for constraining propeller along 20 axial direction of motor shaft, and utilize locking Part 2 constrains propeller in motor shaft 20 in the radial direction.
Wherein, optionally, the first card slot 111 can have diversified forms and structure.For example, the first card slot 111 can have There is bilateral cell wall, alternatively, the first card slot 111 can also only include side cell wall, and other position limiting structures is utilized to limit propeller Axial position relative to mounting base 1.
In a kind of optional structure type, the first card slot 111 includes the first rib on the first holding part 11 1111, the first rib 1111 is circumferentially extended along mounting base 1, when propeller and the rotation of the first card slot 111 engage, the first rib 1111 are located at the side of the separate motor 10 of snap-in structure.
In this way, the first rib 1111 can form the side cell wall of the first card slot 111, when propeller and the first card slot 111 When rotation engaging, the first rib 1111 can be blocked in the side of snap-in structure, to avoid propeller together with snap-in structure from the side It is detached from.Thus the first rib 1111 can with the other structures relative to the snap-in structure other side, e.g. motor 10 or peace Snap-in structure is clipped in wherein by the structure on dress seat 1 jointly, to limit the snap-in structure position upward in transmission shafts.
Optionally, the first card slot 111 further includes the second rib 1112 with the connection of the first rib 1111, the second rib 1112 Positioned at the first rib 1111 one end and along the axially projecting of motor shaft 20, the second rib 1112 is for limiting snap-in structure the Rotation angle in one card slot 111.
At this point, the second rib 1112 can protrude from the first rib 1111, thus be blocked in the rotating path of snap-in structure, When snap-in structure is at rotation to the second rib 1112 in this way, it will abut and stop operating with the second rib 1112, at this point, Snap-in structure can be limited in current rotation angle by the second rib 1112, to complete the engaging between mounting base 1.
Optionally, each second rib 1112 is respectively positioned on the same end of corresponding first rib 1111.Each in this way first The notch of card slot 111 is towards the same side relative to first card slot 111, thus the snap-in structure on propeller is with first Card slot 111 be clamped when, propeller only relative to mounting base 1 circumferentially on same direction, such as towards clockwise or Person could complete engaging towards counter clockwise direction.Since the first card slot 111 has the directionality in circumferential direction, thus can be using the One card slot 111 it is different towards distinguishing the propeller direction being arranged in mounting base 1.For example, when vertical view mounting base 1, first When the notch of card slot 111 is towards clockwise direction, the first card slot 111 can be used for installing positive paddle (CW);And work as and overlook mounting base 1, When the notch of first card slot 111 is towards counter clockwise direction, the first card slot 111 can be used for installing anti-paddle (CCW).And correspondingly, spiral shell Rotation paddle be positive the different directions such as paddle or anti-paddle when, the snap-in structure on propeller also can be different therewith, and can only be with corresponding court To the first card slot 111 rotate engaging, consequently facilitating the direction to propeller distinguishes, realize fool proof operation.
Since the first rib 1111 is only blocked in the side away from motor 10 of propeller snap-in structure, thus it is optional, Mounting base 1 has to the support division 12 protruded far from 10 direction of motor, and support division 12 is for supporting propeller.In this way, propeller The side towards motor 10 of snap-in structure can be supported by support division 12, mobile towards motor 10 to prevent propeller from continuing, And the direction that the first rib 1111 then prevents propeller from facing away from motor 10 is mobile, such support division 12 and the first rib 1111 Jointly wherein by the snap-in structure sandwiched of propeller, to realize the axially position of propeller.
Specifically, support division can be the end face 12 away from 10 side of motor of mounting base 1.The end face is usually annular Face, thus propeller can be supported in the circumferential each different directions of motor shaft 20, and surround jointly with the first rib 1111 To the axially position of propeller.
And locking piece 2 usually can be mobile relative to mounting base 1, to realize to the sealed of the first holding part 11 or unlock, To allow the engaging part of propeller to be caught in or avoid the engaging part of propeller to deviate from from clamped position.Optionally, mounting base 1 On can be set fluted 13, locking piece 2 is located in groove 13 and can be along the axial movement of motor shaft 20.In this way due to the first card Gripping member 11 is usually located on a certain axial position in mounting base 1, thus locking piece 2 along motor shaft 20 move axially when, will Be located relative to the axially different position of the first holding part 11, e.g. be located at and the same axial position of the first holding part 11 on, And outside in the snap-in structure of propeller is kept off, or far from the first holding part 11, so that the snap-in structure of propeller can Smoothly engage with the disengaging of the first holding part 11.
Wherein, optionally, the notch of groove 13 can be opened up towards motor 10, can pass through groove 13 and motor in this way 10 end face realizes that limit is fixed to locking piece 2 jointly, and location structure is relatively simple.
Optionally, since the quantity of the first card slot 111 is one or more, correspondingly, locking piece 2 also can have at least One for backstop in the stopper section 21 of the notch of the first card slot 111.For example, stopper section 21 have it is multiple, and in locking piece 2 Circumferentially-spaced distribution.In this way when locking piece 2 locks propeller, each stopper section 21 can be with backstop in a correspondence The first card slot 111 notch, to avoid propeller by being detached from the first card slot 111.
In order to allow 21 backstop of stopper section at the notch position of the first card slot 111, as an alternative embodiment, backstop Radial distance and the first holding part 11 and the radial distance in the axle center of motor shaft 20 between portion 21 and the axle center of motor shaft 20 is logical It often can be identical.At this point, stopper section 21 and the first holding part 11 are respectively positioned on the same cylindrical surface for being looped around 20 outside of motor shaft. Stopper section 21 is moved axially along motor shaft 20 in this way, and backstop is at the notch position of the first card slot 111, can be just by the The notch of one card slot 111 blocks completely, thus propeller is not easily disconnected from, and engages more reliable.
Since when the first holding part 11 in mounting base 1 is multiple, multiple first holding parts 11 can generally be intervally arranged On the same circumference, thus the notch of each first holding part 11 can be corresponded to towards another holding part adjacent thereto.Correspondingly, As a kind of optional arrangement mode, 21 backstop of stopper section is between two neighboring first holding part 11.At this point, each stopper section 21 can be inserted in the gap between two neighboring first holding part 11, and backstop is in the notch of corresponding first holding part 11 Place.The gap that one side stopper section 21 can use between adjacent first holding part 11 in this way is configured, to effectively save Space;Another aspect stopper section 21 can also be stopped by the first adjacent holding part 11 as support and position limiting structure with improving Reliability when gear.
Optionally, 21 backstop of stopper section is in the notch of the first card slot 111, phase between stopper section 21 and the first holding part 11 Mutually abut.Stopper section 21 can closely be supported by the elastic force and the first holding part 11 of elastic component 3 in this way, to realize to the The backstop and locking of one card slot 111.Wherein, stopper section 21 can only with corresponding first holding part 11 abut, can also with it is right The first holding part 11 answered, and another first holding part 11 adjacent with first holding part 11 realize abutting simultaneously.
Wherein, in order to guarantee stopper section 21 can with the first holding part 11 is reliable mutually abuts, optionally, and form the The first first holding part 11a of one card slot 111 adjacent holding part 11b has the first lozenges 112 diagonally downward, stopper section The second lozenges 211 being mutually matched with the first lozenges 112 is provided on 21, stopper section 21 is acted in the elastic force of elastic component 3 When with this there is the first holding part 11b of the first lozenges 112 to abut, the first lozenges 112 and the second lozenges 211 mutually patch It closes, the position with limit stop portion 21 relative to the notch of the first card slot 111.
Specifically, in general, the elastic force direction that applies to locking piece 2 of elastic component 3 can far from 10 end face of motor, thus The first wedge tilted down can be set in the first holding part 11b adjacent with the first holding part 11a of the first card slot 111 is formed Shape face 112, when such stopper section 21 is moved along axial direction to the first holding part 11, the second lozenges 211 on stopper section 21 will It resists the first lozenges 112 and is bonded wedging therewith.Due to the mutual extrusion of the first lozenges 112 and the second lozenges 211, tool There is the first holding part 11b of the first lozenges 112 that will apply stopper section 21 towards upper first card slot of the first holding part 11a The component of 111 notch completes the snap-in lock to propeller to stopper section 21 is pressed on the notch of the first card slot 111 It is fixed.
Further, since axial direction of the elastic force direction of elastic component 3 generally along motor shaft 20, thus correspondingly, elastic component 3 One end can be relatively fixed with motor, and the other end and locking piece 2 connect, and such locking piece 2 will be under the elastic force of elastic component 3 Along the position for moving axially to be blocked on the outside of 111 notch of the first card slot of motor shaft 20, thus user can pass through movement The position of locking piece 2 come make the first card slot 111 notch close or open.
At this point, optionally, locking piece 2 also has extending radially out along motor shaft 20 for the ease of mobile locking piece 2 Hand-held part 22.User can be by holding hand-held part 22, to apply the effect axial along motor shaft 20 to locking piece 2 is whole Power, and the elastic force of the force direction and elastic component 3 is contrary, such user can be by acting on to 22 application of hand-held part Power makes locking piece 2 along the axial movement of motor shaft 20, completes the lock to the first card slot 111 to offset the elastic force of elastic component 3 Fixed and unlatching.
Common, when user does not apply external force, elastic component 3 can be in nature pressured state, and by the elastic force of itself Locking piece 2 is fixed on to the position being barred from the outside of 111 notch of the first card slot;And when user applies to hand-held part 22 along motor shaft When active force in 20 axial directions, locking piece 2 can overcome the elastic force of elastic component 3 and along the axial movement of motor shaft 20, and from resistance It is blocked in the position on the outside of 111 notch of the first card slot to remove, so that propeller can be loaded into mounting structure for propeller, or by spiral shell It is taken out in rotation paddle mounting structure;After completing the installation or disassembly of propeller, hand-held part 22 can be unclamped, locking piece 2 is made to exist The elastic force effect of elastic component 3 is lower to restore to the position being blocked on the outside of 111 notch of the first card slot.
Wherein, optionally, for convenient for applying active force to locking piece 2, the number of hand-held part 22 can be even number, and phase Motor shaft 20 is symmetrical arranged.User can use finger and push symmetrical hand-held part 22 in this way, to allow the first card slot 111 notch is opened, easily to carry out the quick despatch of propeller.
Optionally, hand-held part 22 is located in groove 13.Hand-held part 22 can directly be stretched out out of groove 13 in this way, locking The structure of part 2 is relatively simple.
Fig. 7 is the structural schematic diagram for another mounting structure for propeller that the utility model embodiment one provides.Such as Fig. 7 institute Show, optionally, is also provided with anti-skid structure on the hand-held part 22 in mounting structure for propeller, it is hand-held to improve user's gripping Frictional force when portion 22 avoids user from rubber sleeve phenomenon occur.Specifically, anti-skid structure can be anti-on 22 surface of hand-held part Sliding line 221 or anti-skidding salient point etc..
And in order to apply elastic force to locking piece 2, it is blocked on the outside of 111 notch of the first card slot so that locking piece 2 is maintained at Position, as a kind of optional structure, the elastic component 3 in mounting structure for propeller can connect for one end and the end face of motor 10 It connects, the mode that the other end and locking piece 2 connect.Elastic component 3 can be support with the end face of motor 10 in this way, apply to locking piece 2 Add the active force far from motor 10.Wherein, the states such as the force direction that elastic component 3 applies locking piece 2 are such as aforementioned reality It applies described in example, details are not described herein again.
Wherein, in order to guarantee that elastic component 3 applies the direction of elastic force, optionally, elastic component 3 and motor shaft 20 can be kept Coaxial arrangement.Specifically, elastic component 3 can be hollow structure, and motor shaft 20 is located among the hollow structure of elastic component 3, or Person's elastic component 3 may be multiple, and multiple elastic components 3 are symmetrical arranged centered on motor shaft 20.
Wherein, elastic component 3 can be there are many possible structure type.In a kind of optional structure type, elastic component 3 can Think spring.Spring usually in the shape of a spiral, thus can be set in 20 outside of motor shaft, and be coaxially disposed with motor shaft 20.
Optionally, elastic component 3 can be larger for one end, and the lesser tower-shaped spring of the other end, such elastic component 3 are compressing When, lesser one end can press to the inside of biggish one end, to effectively reduce the occupied space of elastic component 3.
In addition, elastic component 3 can be Spring capable of diameter varying.Elastic component 3 is made of the spring wire that line footpath gradually changes at this time, impact It, can be by the lesser partial deformation load of line footpath when power is smaller;And impact force it is larger when, can be held by the biggish part of line footpath Power.In this way under smaller pressure, elastic component 3 can have sensitive reaction, and under larger pressure, then there is biggish bullet Power, to realize the reliable deformation of elastic component 3.
In the present embodiment, mounting structure for propeller is used to propeller being detachably arranged in motor.Propeller peace Assembling structure specifically includes mounting base, locking piece and elastic component;Mounting base is fixed on the end face of motor, and mounting base passes through motor Motor shaft, mounting base is used for and propeller rotation engaging, and elastic component connect with locking piece, and elastic component is for along motor shaft It is axial to apply elastic force to locking piece, so that locking piece is at least partly blocked on the outside of the engagement direction of propeller.Such propeller Can be by way of rotation engaging and motor is realized relatively fixed, while connecting more reliable, it is existing can effectively to avoid penetrating paddle As;It dismounts simultaneously relatively simple.
Fig. 8 is a kind of front view for propeller that the utility model embodiment two provides.Fig. 9 is the utility model embodiment The top view of two propellers provided.Figure 10 is the top view for the propeller that the utility model embodiment two provides.Figure 11 is figure The partial schematic diagram of connection component part in 10.Figure 12 is the structural representation for the connection component that the utility model embodiment two provides Figure.Figure 13 is the connection schematic diagram of upper clamping piece and blade in the connection component of the offer of the utility model embodiment two.Figure 14 is The explosive view for the propeller that the utility model embodiment two provides.Figure 15 is the peace for the blade that the utility model embodiment two provides Fill schematic diagram.Figure 16 is structural schematic diagram of the propeller of the offer of the utility model embodiment two when blade folds.Extremely such as Fig. 8 Shown in Figure 16, propeller provided in this embodiment specifically includes at least one blade 4 and the motor shaft for being mounted on motor 10 Connection component 5 on 20, blade 4 are arranged on connection component 5, and connection component 5 includes for pacifying with the propeller on motor 10 The circular connector of assembling structure rotation engaging.
Wherein, propeller includes one or more blades, and blade 4 is usually right centered on the rotary shaft of propeller itself Claim setting.When propeller is in motor 10 when being rotated by, blade 4 can be with movement, and by the own form of blade 4 Air is pushed, to generate lift.And connection component 5 is used to be mounted on the motor shaft 20 of motor 10, to connect 10 He of motor Blade 4.Wherein, connection component 5 includes for the circular connector with the mounting structure for propeller rotation engaging on motor 10 51, circular connector 51 is usually coaxially disposed with the axle center of propeller, and circular connector 51 generally has protrusion or groove 13 equal snap-in structures, to rotate and be fastened togather relative to the mounting structure for propeller on motor 10.
Optionally, the quantity of blade 4 can be two, and two blades are symmetrical arranged, and such propeller can be with less Blade quantity certain lift is provided, structure is relatively simple.The following are convenient for narration, it is including two blades with propeller Example is illustrated.
What is wherein engaged with the rotation of circular connector 51 can be the mounting structure for propeller in previous embodiment one, It can be other connection structures that can be realized rotation engaging function, it is without restriction herein.
Optionally, in order to realize rotation engaging function, circular connector 51 can have annular wall 511 and along annular wall 511 The second holding part of at least one being circumferentially arranged 512, the second holding part 512 is used for and mounting structure for propeller rotation engaging.Its In it is similar with the mounting structure for propeller in previous embodiment one, circular connector 51 equally can have one for realizing The annular wall 511 of rotational slide.When circular connector 51 is moved to the position with mounting structure for propeller overlapping, annular wall 511 inner wall or outer wall will slide against with the main part of mounting structure for propeller, and can allow 51 phase of circular connector Mounting structure for propeller is rotated;And the second holding part 512 can be complete with the corresponding part on mounting structure for propeller It is detached from engaging or from fastening state.
Optionally, same similar with mounting structure for propeller, the second holding part 512, which can be, to be outwardly protruded in annular wall 511 outer wall.At this time correspondingly, corresponding part on mounting structure for propeller, e.g. mounting base 1 can be located at circular connector 51 outside;Alternatively, the second holding part 512 can the inwardly projecting inner wall in annular wall 511, at this point, ring-shaped component can be with Mounting structure for propeller realization positioned inside is connected together.
In order to when rotating engaging with propeller, improve the load ability of mounting base 1, the quantity of the first holding part 11 is logical It often can be more than one, at least two first holding parts 11, and at least two first e.g. can be set in mounting base 1 The setting of the interval of holding part 11.For mounting base 1 when realizing rotation engaging, multiple first holding parts 11 can be in mounting base 1 in this way Different parts realize limit engaging to propeller, and 1 stress of mounting base is more dispersed when engaging, it is thus possible to bear biggish power Square.
It is optionally similar with the first holding part 11 on mounting structure for propeller, it can be set on circular connector 51 At least two second holding parts 512, and the setting of at least two second holding parts 512 interval.In this way circular connector 51 and spiral shell The corresponding portion for revolving paddle mounting structure, when the mounting base 1 e.g. in embodiment one realizes rotation engaging, multiple second holding parts 512 can realize limit engaging, in this way annular connection between the different parts and mounting structure for propeller of circular connector 51 51 stress of part is more dispersed, is able to bear larger torque.
Likewise, second holding part 512 can also be relative to circular connector 51 when the second holding part 512 is multiple Axial centre it is symmetrical, so that torque uniformly to be passed to each second holding part 512, make circular connector 51 circumferential Stress in all directions is more balanced, improves structural reliability.
In addition, all second holding parts 512 can also be respectively positioned on the sustained height along axial direction of circular connector 51.In this way All second holding parts 512, which can be formed, is formed by similar annular surface with the first holding part 11 in previous embodiment one, with Realize propeller and mounting structure for propeller relative to sliding and rotation by the snap-latch surface.The annular surface can be with the first clamping The annular surface fitting that face is formed, the mounting base 1 in circular connector 51 and mounting structure for propeller can be by two patches at this time The annular surface of conjunction realizes relative rotation and supports that structural reliability is higher.
Optionally, the snap-in structure of the radially protruding along motor shaft 20, the second clamping are provided on mounting structure for propeller The second card slot 5121 of the circumferentially extending along circular connector 51 can also be formed on part 512, the second card slot 5121 is used for and blocks Close structure rotation engaging.
Wherein, the second card slot 5121 can circumferentially surround on a certain axial position on the outside of motor shaft 20, and using certainly Snap-in structure on propeller is also limited at the position relative to motor shaft 20 by body cell wall.In addition, the second card slot 5121 On be generally also provided with stop configurations, mounting structure for propeller can be limited in by such first card slot 111 to be connected relative to annular In a certain circumferential angle of part 51, to realize the positioning to propeller in the axial direction.
Wherein, since the snap-in structure on mounting structure for propeller can be various structures, e.g. previous embodiment one First card slot 111 of middle formation or other fasteners etc. that can be mutually matched with the second card slot 5121.Thus correspondingly, For example, the second card slot 5121 or diversified forms, such as the second card slot 5121 can have bilateral cell wall, or only include Side cell wall, then either other common snap-in structures of those skilled in the art etc..
In a kind of wherein optional embodiment, the structure of the second card slot 5121 can be with the card in previous embodiment one Slot mirror-image structure each other.For example, the second card slot 5121 may include the third rib 5122 on the second holding part 512, the Three ribs 5122 along circular connector 51 circumferentially extending, snap-in structure and the second card slot 5121 rotation engaging when, third rib 5122 are located at the side for closing on motor 10 of snap-in structure, and such second card slot 5121 is i.e. using third gear side 5122 by spiral shell Snap-in structure in rotation paddle mounting structure is limited in a certain position in 20 axial direction of motor shaft.
In addition, card slot can also include the fourth gear side 5123 connected with third rib 5122, fourth gear side 5123 is located at One end of third rib 5122 and along the axially projecting of circular connector 51, fourth gear side 5123 exists for limiting snap-in structure Rotation angle in second card slot 5121.
Specifically, it is similar with the relative position of the second rib 1112 with the first rib 1111 in previous embodiment one, the 4th Rib 5123 can also protrude from third rib 5122, to be blocked in the rotating path of mounting structure for propeller, such spiral When paddle mounting structure is rotated relative to circular connector 51 at fourth gear side 5123, will be abutted with fourth gear side 5123 and Stop operating, at this point, mounting structure for propeller can be limited in current rotation angle by fourth gear side 5123, thus complete and Engaging between circular connector 51.
Correspondingly, each fourth gear side 5123 is respectively positioned on the same end of corresponding third rib 5122, at this point, each second The notch of card slot 5121 is towards the same side relative to second card slot 5121, thus mounting structure for propeller blocks with second Slot 5121 be clamped when, propeller only relative to mounting structure for propeller circumferentially on same direction, such as towards clockwise Direction perhaps could complete engaging towards counter clockwise direction and can not then rotate or can not be carried out on other direction when rotated Engaging.Since the second card slot 5121 has the directionality similar with aforementioned first card slot 111, thus the second card slot can be used 5121 it is different towards being distinguished to propeller direction.Circular connector 51 is looked up for example, working as, and the second card slot 5121 Notch towards clockwise direction when, propeller is anti-paddle (CCW) at this time;And works as and look up circular connector 51, and the second card slot When 5121 notch is towards counter clockwise direction, propeller is positive paddle (CW) at this time.Further, the second card slot 5121 can be with One card slot 111 mirror image either complementary structure each other, such as propeller and mounting structure for propeller rotation be when being fastened togather, the The corresponding fitting of the first rib 1111 on third rib 5122 and the first card slot 111 in two draw-in groove 5121, and fourth gear side 5123 together with the second rib 1112 abutting on the first card slot 111.In this way if propeller and mounting structure for propeller Corresponding direction is different, will be unable to complete engaging, thus the design of such directionality carries out convenient for the direction to propeller It distinguishes, realizes fool proof operation.
In addition, similar with previous embodiment one, optionally, when the quantity of the second holding part 512 be two or two with When upper, various sizes of second card slot can be set on the second different holding parts, to play fool proof effect.Its specific structure and Realization principle is similar in previous embodiment one, and details are not described herein again.
In addition, in order to for and motor shaft 20 connect, optionally, be also provided on circular connector 51 be used for and electricity The axle sleeve 513 that the motor shaft 20 of machine 10 connects.513 sets of axle sleeve in 20 outside of motor shaft, so as to the connection of motor shaft 20 simultaneously Fixed motor shaft 20 avoids motor shaft 20 in rotation phenomena such as generation play.
Wherein, the axis hole edge of axle sleeve 513 can have chamfering.Propeller is to mounting structure for propeller and electricity in this way When installing on machine 10, the chamfering at axis hole edge has certain guiding role to motor shaft 20, can be to avoid the rib of motor shaft 20 While causing to cut to axis hole.In general, the chamfering angle size at axis hole edge can be 0.5mm × 45 °.
When the second card slot 5121 only includes third rib 5122 and fourth gear side 5123, in order to further limit spiral The relative position of paddle and mounting structure for propeller in 20 axial direction of motor shaft, optionally, circular connector 51 can also have court The second support division 514 protruded to 10 direction of motor, the second support division 514 are used to support spiral shell from the motor shaft 20 of motor 10 is axial Revolve paddle mounting structure.At this point, the second support division 514 can with 5122 collective effect of third rib, by mounting structure for propeller Corresponding portion is clipped in wherein, realizes that propeller and mounting structure for propeller are relatively fixed in 20 axial direction of motor shaft.
Wherein, since the second holding part 512 on circular connector 51 is usually multiple, and connect in the circumferential around annular Fitting 51, in order to balance each other with the active force of each second holding part 512, optionally, the second support division 514 can be in crosswise It is staggered in the inside of circular connector 51.Central symmetry of such second support division 514 relative to circular connector 51, because And at this time no matter on which direction in the circumferential, circular connector 51 can be realized with mounting structure for propeller and be supported admittedly Fixed, stress is more balanced.
It in addition, the second support division 514 can be other structures and shape, such as can be to protrude from circular connector 51 Supporting structure commonly used by ring edge or other those skilled in the art in annular wall 511 etc., details are not described herein again.
In addition, in order to allow circular connector 51 and blade 4 to be fixed, as an alternative embodiment, annular is even Clamping part 515 can be set on fitting 51, the root of blade 4 is fixed on clamping part 515.At this point, clamping part 515 can be with Fix blade 4 from the side of 4 root of blade, specifically, clamping part 515 can by clamping or threaded fastener with Blade 4 is completed to fix, or utilizes the common fixed blades 4 of other structures part.
Therefore, as one of optional embodiment, connection component 5 can also include upper clamping piece 52, upper clamping Part 52 is used for and clamping part 515 clamps the root of blade 4 jointly.Specifically, upper clamping piece 52 and clamping in connection component 5 Portion 515 can complete to clamp from the two sides up and down of 4 root of blade to blade 4 respectively, so that the structure for being similar to paddle folder is constituted, this Sample blade 4 can be fixed in 20 axial direction of motor shaft, and using between upper clamping piece 52 and clamping part 515 frictional force or Person is position limiting structure, and blade 4 can be allowed to obtain the fixation of connection component 5 in a circumferential direction, makes blade 4 relative to connection component 5 keep certain radial direction, and such blade 4 is positioned using connection component 5.
Wherein, upper clamping piece 52 can use a variety of connection types and the clamping part 515 of lower section completes connection.Such as one In the optional embodiment of kind, it can be attached by threaded fastener 53 between upper clamping piece 52 and circular connector 51. What user can be convenient in this way dismounts blade 4, while guaranteeing that blade 4 can be installed firmly.
Specifically, optionally, may be provided at least one and motor on upper clamping piece 52 in order to which threaded fastener 53 is arranged The parallel boss 521 of axis 20 is provided with threaded hole on boss 521, peace corresponding with threaded hole is provided on circular connector 51 Hole 516 is filled, threaded fastener 53 can be protruded into inside threaded hole by mounting hole 516, to connect upper clamping piece 52 and annular even Fitting 51.Threaded fastener 53 can be installed from bottom to top in this way, and connect the circular connector 51 of upper clamping piece 52 and lower section, The top surface of upper clamping piece 52 does not need to wear threaded fastener, thus more neat and tidy, aesthetics are preferable.
In order to provide enough lift, blade 4 can generally have longer length, at this point, the blade 4 of propeller can have Biggish diameter is not easy to the transport and storage of propeller and unmanned vehicle.It is accounted for reduce the space of propeller blade 4 With can be to be rotatably connected between blade 4 and connection component 5 optionally.In this way when multiple blades on propeller are not having to When can turn to it is close or overlapping position, to make propeller that folded state integrally be presented, to reduce the whole of propeller Body occupied space.In general, blade 4 can usually be rotated relative to connection component 5 in the horizontal plane.
Wherein, in order to realize being rotatably connected between blade 4 and connection component 5, optionally, the root of blade 4 has Pin hole 41, blade 4 can be rotated around pin hole 41, with rotation to folded state or working condition.The root of blade 4 can insert in this way Enter the structures such as pin shaft, and forms turning joint between connection component 5.
Further, in order to allow upper clamping piece 52 and clamping part 515 while clamping blade 4, turning for blade 4 is realized Dynamic connection, as an alternative embodiment, connection component 5 further includes and the matched locating piece of pin hole 41, and upper clamping piece 52 are provided with first positioning hole 522 accordingly, and clamping part 515 is equipped with second location hole 5151, first positioning hole 522 accordingly It is corresponded to each other with the position of second location hole 5151, at this point it is possible to make first positioning hole by adjusting the root position of blade 4 522, the pin hole 41 of 4 root of second location hole 5151 and blade is adjusted to coaxial position, is positioned such that part sequentially passes through first Location hole 522, pin hole 41 and second location hole 5151, so that connection component 5 and blade 4 are fixed together.Due to the first positioning Hole 522, second location hole 5151 and pin hole 41 between locating piece to be rotatably connected, thus locating piece to blade 4 into While row is fixed, also blade 4 can be allowed to be rotated relative to locating piece, to rotate the folding close to each other to different blades The maximized working condition of distance between overlapping state, or different blades.
Wherein, locating piece can for pin shaft, plug screw perhaps at least one of threaded fastener or may be Other common structures of those skilled in the art, it is without restriction herein.
And in order to be matched with different types of locating piece, optionally, second location hole 5151 or unthreaded hole, screw thread Hole or counter sink are at least one.Wherein, when locating piece is that plug screws, second location hole 5151 can be threaded hole, and Directly locking is threadedly engaged with what plug screwed.Alternatively, second location hole 5151 or counter sink, and beaten for fixed plug Screw or threaded fastener etc..At this point, threaded fastener can be packed into counter sink, it can also be packed into and screw matching with plug The nut of conjunction.Wherein, when second location hole 5151 is counter sink, it can also be arranged at the ladder in hole and be used for locking axis Set, axle sleeve is usually plastic cement material etc..In addition, second location hole 5151 can be aperture always one when locating piece is pin shaft The unthreaded hole of cause, and realize by the dimensional fits of pin shaft and connected the matching between second location hole 5151.
For the ease of illustrating, below unless otherwise specified, it is illustrated so that locating piece is pin shaft 54 as an example.
Wherein, in order to which positioning is fixed to pin shaft 54, optionally, can be between first positioning hole 522 and pin shaft 54 Interference fit.At this point, the diameter of pin shaft 54 can be slightly larger than the aperture of first positioning hole 522, thus pin shaft 54 is in first positioning hole Available relatively firm positioning in 522.And the cooperation typically transition on pin shaft 54 and blade 4 between pin hole 41 Cooperation, so that blade 4 can smoothly switch under folded state and working condition, while guaranteeing itself and pin shaft 54 when rotated Between do not relatively rotate.
In order to adapt between interference fit and pin shaft 54 and pin hole 41 between pin shaft 54 and first positioning hole 522 Transition fit can allow the diameter of one end of the insertion first positioning hole 522 of pin shaft 54 to be greater than pin as a kind of optional mode The diameter of the rest part of axis 54 can both guarantee the fixation of pin shaft 54 in this way, can also allow blade 4 freely in rugosity Switching is rotated between state and working condition.
And in another optional embodiment, it, can be directly tight using screw thread when locating piece is threaded fastener Firmware realizes the whole assembly of connection component 5.Figure 17 is another connection component that the utility model embodiment two provides Structural schematic diagram.As shown in figure 17, optionally, locating piece is threaded fastener 53a, upper clamping piece 52 and circular connector 51 it Between by locating piece, that is, threaded fastener 53a connection;At this point, since the position of locating piece is exactly upper clamping piece 52 and ring Tie point position between shape connector 51, thus on locating piece as the thrust of propeller and caused by torsion it is smaller, can Locating piece and corresponding construction is avoided cracking damage phenomenon occur because stress is excessive.In addition, the axis with blade 4 of locating piece The position that hole 41 cooperates has smooth outer wall, so that blade 4 can be freely rotated relative to threaded fastener 53a without by spiral shell The influence of line.
When propeller is in high speed rotational operation, blade 4 can generate high-frequency vibration due to the impact by air-flow, at this point, The vibration of blade 4 may damage connection component 5, or loosen 4 root of blade from connection component 5.In order to subtract The vibration of few blade 4, as a kind of optional mode, upper clamping piece 52, which can specifically include the ontology with cavity and be arranged, to exist Cushion 523 in cavity, first positioning hole 522 are arranged on cushion 523.Blade 4 passes through structures such as pin shaft and upper in this way When clamping piece 52 and clamping part 515 connect, blade 4 can be contacted with cushion 523, and utilize the elastic deformation of cushion 523 The movement and deformation of blade 4 are offset, the damping effect to blade 4 is completed.Wherein, cushion 523 can be set the one of blade Side or upper and lower two sides, depending on specific set-up mode can according to need, with blade towards upper clamping piece in the present embodiment 52 and away from upper clamping piece 52 while be provided with cushion 523 and be illustrated.
Wherein, since blade 4 is generally multiple, thus the quantity of cavity can be identical as the quantity of blade 4.At this point, Each blade can correspond at least one independent cushion 523, thus cushion 523 has preferable effectiveness in vibration suppression.
In order to carry out buffering and vibration damping to blade 4, optionally, cushion 523 can be silicone rubber pad or other tools Flexible material is made.
When being folded to blade 4, due between blade 4 and upper clamping piece 52 or clamping part 515 usually have compared with Big contact area enables blade 4 more smoothly to roll over to reduce the friction between 5 each section of blade 4 and connection component Folded or expansion, optionally, between upper clamping piece 52 and the root of blade 4 and between clamping part 515 and the root of blade 4 At least one can be set gasket 6, gasket 6 and blade 4 are bonded.Gasket 6 is capable of providing more smooth surface, thus has Help reduce the frictional force between connection component 5 and blade 4, so that blade 4 is more smoothly folded or is unfolded, reduce simultaneously Abrasion of 4 surface of blade in rotation.
Optionally, gasket 6 is usually smooth abrasion-proof part, that is, the material system smaller and more wear-resisting by coefficient of friction At.Optionally, gasket 6 is Teflon gasket.Teflon material is also known as polytetrafluoroethylene (PTFE), has lower frictional property and excellent Wearability, thus when 6 surface of gasket and the contact of blade 4, lubricant effect can be played to blade 4, friction is small for generation, makes The rotation of blade 4 is more smooth.
When blade 4 is folded, if two neighboring blade 4 apart from too small, may be caused because contacting with each other Phenomena such as 4 surface damage of blade.In order to avoid adjacent blades 4 collide when the folding of blade 4, as a kind of optional embodiment party Formula, can be arranged at least one limiting section on upper clamping piece 52, and 524 limiting sections are used to limit the rotational angle of blade 4.
By taking Figure 16 as an example, propeller includes that there are two blades, and two blades can be respectively pivoted, directly when folding To going to closer distance.In order to avoid the hypotelorism of two blades, multiple limiting sections are provided on upper clamping piece 52 524, limiting section 524 is arranged in the position between two propeller shanks, when such rotation of blade 4 to predetermined angle, the side of blade 4 Side will collide with limiting section 524 and can not continue to rotate, at this point, two blades 4 will be under the position-limiting action of limiting section 524 Certain spacing is kept, the phenomenon that mutually touching is avoided.Since blade 4 can be rotated to two opposite directions, thus it is corresponding Limiting section 524 there are two can be set in each blade, and two limiting sections 524 are separately positioned on the direction of rotation of blade 4 Two sides.In this way when blade 4 is folded to different directions, two limiting sections 524 can respectively be limited blade 4.
Wherein, limiting section 524 also can have a variety of different structures.Such as in a kind of optional structure, limiting section is set It sets in the bottom surface of upper clamping piece 52, and is protruded towards motor 10.Limiting section 524 has while realizing normal limit in this way Relatively simple structure, and size is smaller.Specifically, limiting section can be the structures such as protrusion or positioning column.
It should be noted that Fig. 8 is to be illustrated in case where propeller includes two blades into Figure 17, and paddle It also can have similar structure when leaf is other quantity, in connection component 5, with the connection and fixation between realization and blade, Details are not described herein again.
In the present embodiment, propeller specifically includes the connection at least one blade and motor shaft for being mounted on motor Component, blade are arranged on connection component, and connection component includes for engaging with the mounting structure for propeller rotation on motor Circular connector.In this way propeller can rotation engaging by way of and motor realize it is relatively fixed, while connection more may be used It leans on, can effectively avoid penetrating paddle phenomenon;The dismounting of propeller is relatively simple simultaneously.
Figure 18 is a kind of structural schematic diagram for power suit that the utility model embodiment three provides.As shown in figure 18, originally The power suit 300 that embodiment provides, includes two institute of mounting structure for propeller 100 described in above-described embodiment one and embodiment At least one of propeller 200 stated, additionally includes motor 10, and propeller 200 is connected by mounting structure for propeller 100 It is connected on motor 10.Wherein, the specific structure of mounting structure for propeller 100 and propeller 200, working principle and function be It is described in detail in the aforementioned embodiment, details are not described herein again.
Specifically, propeller 200 can be allowed by mounting structure for propeller 100 above-mentioned either propeller 200 to revolve The mode for turning engaging is connected in power suit 300, and propeller 200 is fixed, and is not easy in high-speed rotation from propeller Deviate from mounting structure 100, effectively avoids and penetrate paddle phenomenon.
Wherein, Figure 19 is the structural schematic diagram of the motor in the power suit of Figure 18.As shown in figure 19, optionally, motor 10 20 end of motor shaft can have chamfering a, specifically, chamfering a, which can be, first pours out an oblique angle, then pour out the shape of fillet Formula.20 end of motor shaft of motor 10 in this way is not easy to cause to scratch to the structure on propeller 200.
In the present embodiment, power suit includes at least one of mounting structure for propeller and propeller and motor, Propeller is connected on motor by mounting structure for propeller.Propeller in this way can be by way of rotation engaging and motor is real Existing fast assembling-disassembling, while connection is more reliable, can effectively avoid penetrating paddle phenomenon.
The utility model embodiment four also provides a kind of unmanned vehicle, including described in body and at least one embodiment three Power suit, body includes rack and the horn that connect with rack, and power suit setting is on horn.
Specifically, can connect multiple horns on the body of unmanned vehicle, and it is respectively provided with one on each horn and moves Power suit.Propeller in power suit can cut air by rotation, and then generate enough lift to drive nobody Aircraft carries out landing and normal flight.
Specifically, the normal flight in order to guarantee unmanned vehicle, different propellers can have different rotation directions.It is optional , in the power suit that two are disposed adjacent on unmanned vehicle, the steering of motor is usually different.Corresponding, In direction of snap-in structure in power suit on propeller, in mounting structure for propeller the first card slot towards and spiral shell The difference that rotation paddle is loaded into another power set with direction of rotation of the mounting structure for propeller when rotation engages.
In the present embodiment, unmanned vehicle includes body and at least one power suit, and body includes rack and and rack The horn of connection, power suit are arranged on horn;Wherein, power suit includes in mounting structure for propeller and propeller At least one and motor, propeller are connected on motor by mounting structure for propeller.Spiral in this way in unmanned vehicle Paddle can be by way of rotation engaging and motor realizes relatively fixed and fast assembling-disassembling, while connecting more reliable, Neng Gouyou Effect avoids penetrating paddle phenomenon.
Finally, it should be noted that the above various embodiments is only to illustrate the technical solution of the utility model, rather than it is limited System;Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should Understand: it is still possible to modify the technical solutions described in the foregoing embodiments, or to some or all of Technical characteristic is equivalently replaced;And these are modified or replaceed, it does not separate the essence of the corresponding technical solution, and this is practical new The range of each embodiment technical solution of type.

Claims (15)

1. a kind of power suit, which is characterized in that including at least one of mounting structure for propeller and propeller and motor, The propeller is connected on the motor by the mounting structure for propeller;
Wherein, the mounting structure for propeller is used to for propeller being detachably arranged in motor, the propeller installation knot Structure includes mounting base, locking piece and elastic component;The mounting base is fixed on the end face of the motor, and the mounting base passes through The motor shaft of the motor, the mounting base is used for and propeller rotation engaging, the elastic component and the locking piece connect It connects, and the elastic component is used to apply elastic force to the locking piece along the axial of the motor shaft, so that the locking piece is at least Part is blocked on the outside of the engagement direction of the propeller;
The propeller, it is described including the connection component and at least one blade on the motor shaft for being mounted on the motor Blade is arranged on the connection component, and the connection component includes for rotating with the mounting structure for propeller on the motor The circular connector of engaging.
2. power according to claim 1 suit, which is characterized in that the mounting base is be disposed around the motor shaft outer The annular element of side, and the mounting base is circumferentially arranged at least one first holding part, first holding part is used for and institute State propeller rotation engaging.
3. power suit according to claim 2, which is characterized in that the propeller has radially projecting engaging knot Structure forms the first card slot of the circumferentially extending along the mounting base on first holding part, and first card slot is used for and institute State snap-in structure rotation engaging.
4. power suit according to claim 3, which is characterized in that first card slot includes being located at first clamping The first rib on part, the circumferentially extending of mounting base described in the first gear edge, the propeller and first card slot rotation When engaging, first rib is located at the side far from the motor of the snap-in structure of the propeller;
First card slot further includes the second rib connected with first rib, and second rib is located at the first gear The one end on side and along the axially projecting of the motor shaft, second rib is used to limit the snap-in structure of the propeller in institute State the rotation angle in the first card slot.
5. power suit according to claim 3 or 4, which is characterized in that the locking piece has at least one for only Keep off the stopper section in the notch of first card slot.
6. power suit according to claim 5, which is characterized in that slot of the stopper section backstop in first card slot When mouth, mutually abutted between the stopper section and first holding part.
7. power according to claim 6 suit, which is characterized in that the stopper section and form the of first card slot The first adjacent holding part of one holding part mutually abuts;Described first adjacent with the first holding part for forming first card slot Holding part has the first lozenges diagonally downward, and the be mutually matched with first lozenges is provided on the stopper section Two lozenges, the stopper section is in the elastic force effect of the elastic component and with first holding part of first lozenges When abutting, first lozenges and second lozenges are bonded to each other to limit the stopper section relative to first card The position of the notch of slot.
8. power suit according to claim 1-4, which is characterized in that the circular connector has annular wall With at least one second holding part being circumferentially arranged along the annular wall, second holding part is used for and propeller installation Structure rotation engaging.
9. power suit according to claim 8, which is characterized in that be provided on the mounting structure for propeller along described The snap-in structure of the radially protruding of motor shaft forms the of the circumferentially extending along the circular connector on second holding part Two draw-in groove, second card slot is used for and snap-in structure rotation engaging.
10. power suit according to claim 9, which is characterized in that second card slot includes being located at second card Third rib in gripping member, the circumferentially extending of circular connector described in the third gear edge, the mounting structure for propeller When snap-in structure and second card slot rotation engaging, the third rib is located at the motor that closes on of the snap-in structure Side;
The card slot further includes the fourth gear side connected with the third rib, and the fourth gear side is located at the third rib One end and along the axially projecting of the circular connector, the fourth gear side is used to limit the engaging of the mounting structure for propeller Rotation angle of the structure in second card slot.
11. power suit according to claim 8, which is characterized in that be provided with clamping part, institute on the circular connector The root for stating blade is fixed on the clamping part;The connection component further includes upper clamping piece, the upper clamping piece be used for and The clamping part clamps the root of the blade jointly.
12. power suit according to claim 11, which is characterized in that being between the blade and the connection component can Rotation connection.
13. power suit according to claim 12, which is characterized in that the root of the blade has pin hole, the paddle Leaf can be rotated around the pin hole, with rotation to folded state or working condition;The connection component further includes and the pin hole Matched locating piece, the upper clamping piece are provided with first positioning hole, and the clamping part is equipped with second location hole, and described first is fixed Position hole and the position of the second location hole correspond to each other, and the locating piece sequentially passes through the first positioning hole, the pin hole With the second location hole so that the connection component and the blade are fixed together.
14. power suit according to claim 13, which is characterized in that the upper clamping piece includes the ontology with cavity With the cushion being arranged in the cavity, the first positioning hole is arranged on the cushion;And/or
Between the upper clamping piece and the root of the blade and between the clamping part and the root of the blade at least One is provided with gasket, the gasket and blade fitting.
15. power suit according to claim 11, which is characterized in that be provided at least one limit on the upper clamping piece Position portion, the limiting section are used to limit the rotational angle of the blade.
CN201820655756.3U 2018-05-04 2018-05-04 Power suit Expired - Fee Related CN208233359U (en)

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019210501A1 (en) * 2018-05-04 2019-11-07 深圳市大疆创新科技有限公司 Propeller mounting structure, propeller, power set and unmanned aerial vehicle
CN110733624A (en) * 2019-01-23 2020-01-31 杭州零零科技有限公司 Unmanned flight system and control system for unmanned flight system
WO2020107571A1 (en) * 2018-11-30 2020-06-04 深圳市大疆创新科技有限公司 Steering engine and unmanned aerial vehicle
CN111683874A (en) * 2019-04-29 2020-09-18 深圳市大疆创新科技有限公司 Quick detach coupling assembling, screw, power device, power component and unmanned aerial vehicle
CN112119008A (en) * 2019-07-30 2020-12-22 深圳市大疆创新科技有限公司 Power component and unmanned vehicles
WO2021003609A1 (en) * 2019-07-05 2021-01-14 深圳市大疆创新科技有限公司 Power assembly and unmanned aerial vehicle
WO2021081788A1 (en) * 2019-10-30 2021-05-06 深圳市大疆创新科技有限公司 Folding structure, folding structure of unmanned aerial vehicle, and movable platform

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110662695A (en) * 2018-05-04 2020-01-07 深圳市大疆创新科技有限公司 Screw mounting structure, screw, power suit and unmanned vehicles
WO2019210501A1 (en) * 2018-05-04 2019-11-07 深圳市大疆创新科技有限公司 Propeller mounting structure, propeller, power set and unmanned aerial vehicle
WO2020107571A1 (en) * 2018-11-30 2020-06-04 深圳市大疆创新科技有限公司 Steering engine and unmanned aerial vehicle
CN110733624B (en) * 2019-01-23 2021-09-28 杭州零零科技有限公司 Unmanned flight system and control system for unmanned flight system
CN110733624A (en) * 2019-01-23 2020-01-31 杭州零零科技有限公司 Unmanned flight system and control system for unmanned flight system
WO2020151361A1 (en) * 2019-01-23 2020-07-30 杭州零零科技有限公司 Unmanned flight system and control system for use in unmanned flight system
JP7265017B2 (en) 2019-01-23 2023-04-25 ハンチョウ ゼロ ゼロ テクノロジー カンパニー リミテッド Unmanned flight systems and control systems used in unmanned flight systems
JP2022517677A (en) * 2019-01-23 2022-03-09 ハンチョウ ゼロ ゼロ テクノロジー カンパニー リミテッド Control systems used in unmanned flight systems and unmanned flight systems
CN113619767A (en) * 2019-01-23 2021-11-09 杭州零零科技有限公司 Unmanned flight system and control system for unmanned flight system
WO2020220202A1 (en) * 2019-04-29 2020-11-05 深圳市大疆创新科技有限公司 Quick-release connecting assembly, airscrew, power device, power assembly and unmanned aerial vehicle
CN111683874A (en) * 2019-04-29 2020-09-18 深圳市大疆创新科技有限公司 Quick detach coupling assembling, screw, power device, power component and unmanned aerial vehicle
WO2021003609A1 (en) * 2019-07-05 2021-01-14 深圳市大疆创新科技有限公司 Power assembly and unmanned aerial vehicle
CN112119008A (en) * 2019-07-30 2020-12-22 深圳市大疆创新科技有限公司 Power component and unmanned vehicles
WO2021081788A1 (en) * 2019-10-30 2021-05-06 深圳市大疆创新科技有限公司 Folding structure, folding structure of unmanned aerial vehicle, and movable platform

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