CN107112464B - Battery fixing mechanism, the rack of unmanned plane and cell managing device - Google Patents

Battery fixing mechanism, the rack of unmanned plane and cell managing device Download PDF

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Publication number
CN107112464B
CN107112464B CN201680003746.5A CN201680003746A CN107112464B CN 107112464 B CN107112464 B CN 107112464B CN 201680003746 A CN201680003746 A CN 201680003746A CN 107112464 B CN107112464 B CN 107112464B
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CN
China
Prior art keywords
battery
lever
locking
rack
unmanned plane
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
CN201680003746.5A
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Chinese (zh)
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CN107112464A (en
Inventor
彭涛
欧迪
唐尹
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.)
Dji Baiwang Technology Co ltd
Original Assignee
Shenzhen Dajiang Innovations Technology Co Ltd
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Publication of CN107112464A publication Critical patent/CN107112464A/en
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Publication of CN107112464B publication Critical patent/CN107112464B/en
Expired - Fee Related legal-status Critical Current
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Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/20Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
    • H01M50/262Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders with fastening means, e.g. locks
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00Equipment not otherwise provided for
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01MPROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M50/00Constructional details or processes of manufacture of the non-active parts of electrochemical cells other than fuel cells, e.g. hybrid cells
    • H01M50/20Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders
    • H01M50/249Mountings; Secondary casings or frames; Racks, modules or packs; Suspension devices; Shock absorbers; Transport or carrying devices; Holders specially adapted for aircraft or vehicles, e.g. cars or trains
    • 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
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/10Energy storage using batteries

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  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Electrochemistry (AREA)
  • General Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Battery Mounting, Suspending (AREA)

Abstract

The rack and cell managing device of a kind of battery fixing mechanism, unmanned plane, the battery fixing mechanism includes for fixing the locking device of battery (4), and the locking device (4) includes unblock button (41), transmission mechanism (42) and the battery lock (43) for locking the battery (2).The transmission mechanism (42) includes lever (45), and one end of the lever (45) can be connect with the unblock button (41), and other end can latch (43) with the battery and connect.Wherein, when unlocking the locking device, the unblock button is operated, drives the battery lock to be detached from the battery by the transmission mechanism.The unlocking function of locking device uses lever design in the present invention, can use lever when unlocking locking device and reduces operating force, to realize comfortable unlock feel.In addition, the dynamics of locking battery can be increased, reduces the operating force of unlock using the lever, ensure that unlock feel in battery lock firm foundations.

Description

Battery fixing mechanism, the rack of unmanned plane and cell managing device
Technical field
The present invention relates to unmanned plane field, the rack and battery management of especially a kind of battery fixing mechanism, unmanned plane Device.
Background technique
In the prior art, unmanned plane can be used for taking photo by plane, survey and draw, plant protection, detecting, the industries such as the disaster relief, in structure usually by The composition such as centre frame, dynamical system, undercarriage, by carrying winged control, figure passes and other micro computer equipment carry out operation.
Wherein the battery fixing mechanism in the field there are certain requirements the contact engaging and separating force of battery, and need battery with connect Device has certain chucking power.The chucking power is related to the conveyance capacity of connector, needs to make battery and company in the design process It connects device and closely connects and provide the conveyance capacity that biggish chucking power guarantees connector.However the biggish chucking power of offer then can shadow The releasing force that battery pull-off is gone out to battery fixing mechanism is rung, and needs to guarantee that battery is not easy in use from the fixed machine of battery Deviate from structure.Therefore, operation battery is deviate to need biggish active force from battery fixing mechanism, makes inconvenient for operation.
Summary of the invention
The present invention provides the rack and cell managing device of a kind of battery fixing mechanism, unmanned plane.
According to a first aspect of the embodiments of the present invention, a kind of battery fixing mechanism is provided, including the lock for fixing battery Determine device, the locking device includes unblock button, transmission mechanism and the battery lock for locking the battery.The biography Motivation structure includes lever, and one end of the lever can be connect with the unblock button, and other end can be with the battery lock Button connection.
Wherein, when unlocking the locking device, the unblock button is operated, the battery is driven by the transmission mechanism Lock is detached from the battery.
According to a second aspect of the embodiments of the present invention, a kind of rack of unmanned plane, including fuselage are provided, the fuselage is equipped with For the battery compartment of placing battery, and the connector in the battery compartment for being electrically connected with the battery.It is described Fuselage further include for by the battery lock in the locking device in the battery compartment.
The locking device includes unblock button, transmission mechanism and the battery lock for locking the battery.It is described Transmission mechanism includes lever, and one end of the lever can be connect with the unblock button, and other end can be with the battery Lock connection.
Wherein, when unlocking the locking device, the unblock button is operated, the battery is driven by the transmission mechanism Lock is detached from the battery.
According to a third aspect of the embodiments of the present invention, a kind of cell managing device, including shell are provided, the shell is equipped with For the battery compartment of placing battery, and the charging interface in the battery compartment for being electrically connected with the battery.Institute State shell further include for by the battery lock in the locking device in the battery compartment.
The locking device includes unblock button, transmission mechanism and the battery lock for locking the battery.It is described Transmission mechanism includes lever, and one end of the lever can be connect with the unblock button, and other end can be with the battery Lock connection.
Wherein, when unlocking the locking device, the unblock button is operated, the battery is driven by the transmission mechanism Lock is detached from the battery.
The unlocking function of locking device uses lever design in the present invention, can use lever when unlocking locking device Reduce operating force, to realize comfortable unlock feel.In addition, the dynamics of locking battery can be increased, reduced using the lever The operating force of unlock ensure that unlock feel in battery lock firm foundations.
Detailed description of the invention
To describe the technical solutions in the embodiments of the present invention more clearly, make required in being described below to embodiment Attached drawing is briefly described, it should be apparent that, drawings in the following description are only some embodiments of the invention, for For those of ordinary skill in the art, without creative efforts, it can also be obtained according to these attached drawings other Attached drawing.
Fig. 1 is a kind of schematic diagram of unmanned plane shown in the embodiment of the present invention.
Fig. 2 is the structural schematic diagram of battery fixing mechanism in a kind of unmanned plane shown in the embodiment of the present invention.
Fig. 3 is the structural schematic diagram of the battery lock of the locking device shown in the embodiment of the present invention.
Fig. 4 is the structural schematic diagram of the auxiliary device of a-quadrant in locking device shown in Figure 2.
Fig. 5 is the structural schematic diagram before a kind of unmanned plane middle fuselage and battery installation shown in the embodiment of the present invention.
Fig. 6 is that percentage of batteries is mounted on the structural schematic diagram in fuselage in a kind of unmanned plane shown in the embodiment of the present invention.
Fig. 7 is that battery is mounted on the structural schematic diagram in fuselage in a kind of unmanned plane shown in the embodiment of the present invention.
Fig. 8 is a kind of structural schematic diagram of cell managing device shown in the embodiment of the present invention.
Fig. 9 is a kind of part perspective view of the explosion of cell managing device shown in Fig. 8.
Figure 10 is the structural schematic diagram of B area auxiliary device in cell managing device shown in Fig. 9.
Specific embodiment
Example embodiments are described in detail here, and the example is illustrated in the accompanying drawings.Following description is related to When attached drawing, unless otherwise indicated, the same numbers in different drawings indicate the same or similar elements.Following exemplary embodiment Described in embodiment do not represent all embodiments consistented with the present invention.On the contrary, they be only with it is such as appended The example of device and method being described in detail in claims, some aspects of the invention are consistent.
In the absence of conflict, the feature in following embodiment and embodiment can be combined with each other.
It please refers to shown in Fig. 1 to Fig. 7, the embodiment of the present invention provides a kind of rack 100 of unmanned plane, including fuselage 1.Its Described in fuselage 1 be equipped with the battery compartment 3 for placing battery 2, in the battery compartment 3 for electrically connecting with the battery 2 The connector 5 connect and the battery fixing mechanism (not indicating) for battery 2 to be retained in the battery compartment 3.The battery Fixed mechanism includes the locking device 4 for being locked in the battery 2 in the battery compartment 3.
The setting position of the locking device 4 can be designed according to different demands, for example, in one embodiment, institute Stating locking device 4 can be set in the outside of the fuselage 1.Really, in another embodiment, the locking device 4 can also It is set to inside the fuselage 1.
The specific structure of the locking device 4 can be designed according to different demands, for example, in the illustrated embodiment, The locking device 4 includes unblock button 41, transmission mechanism 42 and the battery lock 43 for locking the battery 2.Wherein, The battery lock 43 can be held on the battery 2, be fixed on the battery 2 in the battery compartment 3.
The transmission mechanism 42 is equipped with shaft 44 and the lever 45 around the shaft 44 rotation.Wherein, the shaft 44 It fixes on the fuselage 1, the lever 45 can be rotated around the shaft 44.
The lever 45 latches 43 direct or indirect connections with the unblock button 41 and the battery respectively.For example, In the illustrated embodiment, one end of the lever 45 is separably abutted with the unblock button 41, the lever 45 The other end is separably abutted with battery lock 43.When unlocking the locking device 4, the unblock button can be operated 41, drive the battery lock 43 to be detached from the battery by the transmission mechanism 42.Institute is pressed by the unblock button 41 One end of lever 45 is stated, the lever 45 is rotated around the shaft 44, and the other end of the lever 45 drives the battery lock 43 is mobile.So that the battery lock 43 is detached from the battery 2, realizes and unlock the locking device 4.It follows that institute It states battery lock 43 battery 2 is fixed in the battery compartment 3, unlocks institute using the lever construction of the transmission mechanism 42 State battery lock 43.
Certainly, the lever 45 is not limited to separably abut with the unblock button 41 and battery lock 43, The connection that other modes can be used direct or indirect, for example, in other embodiments, the lever can also be pressed with unlock respectively Button and battery lock articulated connection.
It is well known that lever construction have the characteristics that it is laborsaving.Therefore, in an embodiment of the present invention, the solution can be based on It locks button 41 and battery lock 43 is of different sizes relative to the torque of the lever 45, realize that the battery lock 43 uses The fixed battery 2 of biggish active force, and easily unlock institute is realized in the unblock button 41 using lesser active force State locking device 4.To guarantee to lock to the battery 2, battery 2 is set not latch 43 abjections from battery, and tune can be passed through The length adjustment of section lever 45 unlocks the unlock feel of the tripper 4.
The regulative mode of the lever 45 can be adjusted according to different demands, for example, in the illustrated embodiment, it is described Lever 45 is divided into first connecting portion and the second connecting portion with rotation center, and the first connecting portion and the unblock button 41 connect It connects, the second connecting portion is connect with battery lock 43.Wherein, the length of the first connecting portion is greater than described second and connects The length of socket part.Since the length of the first connecting portion is greater than the length of the second connecting portion, the pressing solution is alleviated The unlock dynamics for locking button 41, to obtain preferably unlocking feel.
The quantity of the battery lock 43 can be designed according to the quantity of the battery compartment 3, for example, in an embodiment In, when the fuselage 1 includes a battery compartment 3, the tripper 4 includes 41, transmission mechanisms of a unblock button 42 and battery lock 43.One unblock button 41 of operation can drive two levers 45 around two shafts 44 Rotation drives the battery lock 43 to be detached from the battery 2.It is corresponding to increase above-mentioned tripper if two battery compartments 3 are arranged The quantity of 4 each structure.
In another embodiment, when the fuselage 1 includes two battery compartments 3, the tripper 4 includes a solution Lock button, a transmission mechanism and the unblock button and two electricity that transmission mechanism cooperates, being located on two battery compartments Pond lock.Two battery lock buttons are separately connected one end of a lever, and the other end of lever is connect with unblock button, described in pressing When unblock button, the lever rotates around the axis, so that two battery locks of driving are detached from battery.
The specific structure of the battery lock 43 can be designed according to different demands, for example, in the fig. 3 embodiment, The battery lock 43 includes locking piece 46 and the elastic component 47 connecting with the locking piece 46.The elastic component 47 is for providing One elastic-restoring force gives the locking piece 46, makes battery described in effect force locking of the locking piece 46 based on the elastic component 47 2。
Wherein, described 47 one end of elastic component is connect with fuselage 1, and the other end supports on the locking piece 46, makes the lock Determine the crimping of part 46 to be held on the battery 2 to lock battery 2.Operate one end that the unblock button 41 drives the lever 45 It moves down, the other end of the lever 45 drives the locking piece 46 to move up, and compresses the elastic component 47, until the locking piece 46 are detached from the battery 2.When no longer operating the unblock button 41, the elastic component 47 supports the locking piece 46 and moves down, and The one end for driving the lever 45 to connect with the locking piece 46 moves down reset, and the other end of the lever 46 moves up reset.
The specific structure of the elastic component 47 can be designed according to different demands.For example, the elastic component can for Connect boss, lantern ring, limiting slot or limited post etc..In the embodiment shown in fig. 3, elastic component 47 be compressed spring, one end with The locking piece 46 abuts, and other end is connected with the inside of fuselage 1.
The bottom of the locking piece 46 may be configured as wedge shape, be provided with fixing groove 21 on the corresponding battery 2.The lock The bottom for determining part 46 is held in the fixing groove 21, and the side wall of the fixing groove 21 hinders the battery 2 mobile.Certainly described The bottom of locking piece 46 may be arranged as other shapes, meets the locking piece 46 and locks the electricity at least two directions Pond 2.Described two directions include:Battery 2 described in 46 clamping of locking piece, is fixed on the battery 2 in the battery compartment 3 Direction, and be detached from the battery 2 the contrary direction of the battery compartment 3, battery 2 applied in the opposite direction Add active force, prevents the battery 2 from deviating from the battery compartment 3.
The locking piece 46 further includes the interconnecting piece 48 connecting with the transmission mechanism 42.Specifically, interconnecting piece 48 can It is abutted with the lever 45, to be cooperated and 46 phase separation of locking piece by lever 45 and the interconnecting piece 48.
The specific structure of the interconnecting piece 48 can be designed according to different demands, for example, the interconnecting piece 48 can be Abut boss, lantern ring, limiting slot or limited post etc..In the embodiment shown in fig. 3, the interconnecting piece 48 is to abut boss, It is integrally formed with the locking piece 46.Really, in other embodiment, the interconnecting piece 48 or limited post, It can be installed together with locking piece 46.
Referring to Fig. 4, for the ease of the battery 2 to be conveniently located in the battery compartment 3, the locking device 4 It further include auxiliary device 6.
In conjunction with shown in Fig. 2 to Fig. 5, the auxiliary device 6 is set on the fuselage 1 for supporting the battery 2.And And to abut the direction of the 43 locking batteries 2 of direction and battery lock of the battery 2 different for the auxiliary device 6.It is logical It crosses and the auxiliary device 6 is set, so that battery 2 is preferably connect with connector 5, and battery 2 is made to be easy the abjection battery Storehouse 3 is more firmly fixed in the battery compartment 3.The auxiliary device 6 is after unlocking the locking device 4, by the electricity The all or part in pond 2 pops up the battery compartment 3.
The setting position of the auxiliary device 6 can be designed according to different demands, for example, in the illustrated embodiment, The auxiliary device 6 supports the position on the one side of the battery 2, close to the middle part or end of 2 side of battery.When When unlocking the locking device 4, the auxiliary device 6 is supported in the upper end of the one side of the battery 2, and close to the lock Determine device 4, the battery 2 can be released the battery compartment 3.There are other devices in the battery compartment 3, hinders the battery 2 The battery compartment 3 (being detailed later) is all popped up, the battery compartment 3 is popped up in the part of the battery 2 by the auxiliary device 6.
In another embodiment, the auxiliary device 6 can also support the battery to the interior direction of the battery compartment 3 2, make the battery 2 is stronger to be fixed in the battery compartment 3, with prevent the battery 2 deviate from the battery compartment 3 or because The battery compartment 3 is deviate from the vibration of fuselage 1.The auxiliary device 6 is supported in the medium position of 2 one side of battery, can be used It is fixed in the battery compartment 3 in by the battery 2.It should illustrate, the outside of the battery compartment 3 is the battery 2 abjection The direction position of the fuselage 1 is the battery 2 close to the direction position of fuselage 1 on the inside of corresponding battery compartment.
Fig. 5 to Fig. 7 is please referred to, for the ease of positioning the battery 2, the auxiliary device 6 can be total with the connector 5 The battery 2 is positioned with cooperation.For example, the connector 5 is set to the bottom of battery compartment 3, it is connect with the bottom of battery 2. The locking device 4 abut the battery 2 make on one side the battery 2 and the connector 5 in a first direction (in such as Fig. 7 to Under arrow it is signified) on hold, the another side that the auxiliary device 6 abuts the battery 2 makes the battery 2 and the connector 5 hold on second direction (arrow in such as Fig. 7 to the right is signified).
Specifically, the auxiliary device 6 is connected to the position on the side of the battery 2, far from the battery 2 and institute State one end of the electric connection of connector 5.The top surface that the locking device 4 abuts the battery 2 makes the battery 2 described first It is held on direction with the connector 5.The auxiliary device 6 abuts the one side of the battery 2, and the bottom of the battery 2 becomes To in the connector 5, and the battery 2 is held in a second direction with the connector 5.The auxiliary device 6 supports The battery 2 is held, and the auxiliary device 6 abuts the 43 locking battery 2 of direction and battery lock of the battery 2 Direction is different, for reach make the battery 2 in two directions with the close-connected effect of connector 5, so as to solve Because the battery 2 caused by reasons such as vibration contacts bad problem with the connector 5.
It should be noted that in the above-described embodiment, the first direction can be vertical with second direction.When So, there can also be certain angle between the first direction and second direction.For example, the locking device 4 locks the battery 2 Direction is vertical with the direction that 2 pull-off of battery goes out the battery compartment 3, or forms an angle.
The specific structure of the auxiliary device 6 can be designed according to different demands, for example, in Fig. 2 to reality shown in Fig. 4 It applies in example, the auxiliary device 6 includes elastic supporting member for supporting optical member 61 and the sliding part 62 connecting with the elastic supporting member for supporting optical member 61, the bullet Property supporting element 61 for driving the sliding part 62 to slide abut the battery 2, make the battery 2 from battery to provide one The auxiliary force being detached from storehouse 3.
Wherein, when the locking device 4 locks the battery 2, the elastic supporting member for supporting optical member 61 drives the sliding part 62 The side wall for supporting the battery 2, when unlocking the locking device 4, the elastic supporting member for supporting optical member 61 drives the sliding part 62 to push away The side wall for moving the battery 2 makes battery 2 be detached from battery compartment.
Further, the elastic supporting member for supporting optical member 61 further includes the locating part 22 on the battery, the locating part 22 It is abutted with the sliding part 62, for pushing the sliding part 62.The elastic supporting member for supporting optical member 61 drives the sliding part 62, described Sliding part 62, which can be supported, releases battery compartment 3 for battery 2 on the locating part 22.When installing battery 2, the locating part 22 is pushed away It moves the sliding part 62 to slide, to compress the elastic supporting member for supporting optical member 61, until 2 locking means 4 of battery are locked in battery compartment 3 It is interior.
The quantity of the auxiliary device 6 can design according to actual needs, for example, the auxiliary device 6 can be more It is a, and it is respectively arranged on opposite two inner wall of the battery compartment 3.At this point, the locating part 22 is also multiple, and respectively Set on the opposite sides of the battery 3.
For example, the identical auxiliary of two position heights is arranged on two corresponding side walls of a battery compartment 3 Device 6.Cylindrical body of the locating part 22 using 2 side wall of protrusion or the battery being set on the battery 2, the battery Two locating parts 22 are set on 2 each side walls.The sliding part 62 is connected on the locating part 22.
The specific structure of the elastic supporting member for supporting optical member 61 can be designed according to different demands, for example, the elastic supporting member for supporting optical member 61 can be compressed spring, extension spring, torsional spring, rubber item, rubber column or metal clips etc..Embodiment shown in Fig. 4 In, the elastic supporting member for supporting optical member 61 uses compressed spring, and one end of the compressed spring is connected on the fuselage 1, and the other end connects It connects on the sliding part 62.The elastic supporting member for supporting optical member can drive the sliding part 62 to support the battery 2, can also be electric Pond 2 pushes sliding part 62 and compresses.
Please continue to refer to Fig. 4, for the ease of installing and repairing the auxiliary device 6, the fuselage 1 further includes far from described The holding tank 11 that connector 5 is arranged is equipped at least one described auxiliary device 6 in the holding tank 11.The battery compartment 3 to It is equipped with one less, the sliding block 62 of at least one auxiliary device 6 extends at least one described battery compartment 3 to support State battery 2.
The auxiliary device 6 is set on two opposite side walls of the battery compartment 3, is arranged two on a battery compartment 3 A auxiliary device 6.If two battery compartments 3 are arranged, a partition 12 is arranged for branch in the ipsilateral holding tank 11 of battery compartment 3 The elastic supporting member for supporting optical member 61 is supportted, two auxiliary devices 6 are oppositely arranged.The elastic supporting member for supporting optical member 61 is described to drive using spring Sliding block 62.
It please refers to shown in Fig. 2 to Fig. 5, the battery fixing mechanism further includes guide frame 7, and the battery can be described The battery compartment 3 is slid under the guiding role of guide frame 7, and the guide frame 7 and the locking device 4 cooperation are held The battery 2.
For example, the guide frame 7 is gradually open from bottom to top, it is conducive to fixed and installation battery.The locking Device 4 holds the battery 2 on the direction that Fig. 7 downward arrow is directed toward with the connector 5.The guiding can be tied The bottom end of structure 7 is flushed with the bottom of the connector 5, and the 4 clamping battery 2 of locking device is fixed on the bottom of guide frame 7 In space, so that the bottom of the battery 2 and the connector 5 are held.
The specific structure of the guide frame 7 can be designed according to different demands, for example, as shown in figure 5, the guiding The guide part 71 and the auxiliary section 23 on the battery that structure 7 includes the inner wall set on the battery compartment 3, the cooperation Portion 23 is matched with the guide part 71, to guide the battery 2 to be inserted into the battery compartment 3.The auxiliary section 23 is placed in In the guide part 71, the bottom of battery 2 is set to be divided into the bottom of battery compartment 3, while the bottom of battery 2 is connect with connector 5.Institute It states when guide frame 7 is oriented to the battery 2 with more battery anti-off effect, prevents the battery 2 from taking off from the battery compartment 3 Out.
Further, the guide part 71 may be configured as multiple, and be respectively arranged on opposite two of the battery compartment 3 On inner wall.The auxiliary section 23 may be configured as opposite facing two sides that are multiple, and being respectively arranged on the battery 2.For example, The guide part 71 is respectively set on the two sidewalls of one battery compartment 3.The auxiliary section 23 on each side wall is settable Two, and it is spaced setting, it is conducive to that battery 2 is connect and fixed with guide part 71.
As shown in Figures 5 to 7, in order to make the battery 2 be electrically connected stabilization, the guide frame 7 with the connector 5 It can be used in combination with the auxiliary device 6, so as to the battery 2 and make battery 2 and the connector 5 closely fixing.The lock Determine device 4 and provide active force downwards for the battery 2, holds the battery 2 with the connector 5.While the battery 2 Bottom is fixed on 71 bottom of guide part, and holds with the connector 5.And the auxiliary device 6 is supported in the battery 2 Side on, and far from the connector 5 one end, push up battery 2 in the side that pull-off goes out battery compartment 3.The thus electricity The bottom in pond 2 is intended to the connector 5 in the bottom of the guide part 71 and holds with the connector 5.
As shown in Fig. 2, the auxiliary device 6 is set to 7 top of guide frame when being equipped with the guide frame 7. The locking device 4 is unlocked, the part of the battery 2 can be popped up the battery compartment 3 by the auxiliary device 6.Certainly, described auxiliary Device 6 is helped to may also set up in the top close to the guide frame 7.
For convenience of installing and using, the connector 5 is equipped with construction opening, and the battery 2 is along the construction opening energy It is enough to be rotated relative to the connector 5.Such as on the connector 5 be arranged 90 ° construction opening, it can be achieved that the battery 2 with The rotation connection of the connector 5.It is appreciated that the battery 2 can be relative to after connecting or connect with the connector 5 The connector 5 rotates.
The specific structure of the guide part 71 can be designed according to different demands, and the guide part 71, which is specifically as follows, leads To slot, guide rail, guide post or guide rod etc..The auxiliary section 23 can be slide post, sliding slot, guide groove or sleeve etc..In Fig. 5 Shown in embodiment, the guide part is guide groove, and the auxiliary section 23 is slide post.
Fig. 5 to Fig. 7 is please referred to, when the battery 2 is installed to the battery compartment 3, firstly, the auxiliary section 23 is put Entering the guide part 71 makes battery 2 slide into the guide frame 7.When the battery 2 slides into the bottom of the guiding mechanism 7 and institute State the connection of connector 5.Then, it pushes the battery 2 to connect the top of the battery 2 with the locking device 4, makes the electricity Pond 2 is fixed in the battery compartment 3, while the locating part 22 drives the sliding part 62 of the auxiliary device 6 mobile.Complete electricity The installation in pond 2, the battery 2 are fixed in the battery compartment 3, final as shown in Figure 7.
It please refers to shown in Fig. 8 to Figure 10, the embodiment of the present invention also provides a kind of cell managing device 200, including shell 10, the shell 10 is equipped with the battery compartment 3 for placing battery 2, and is set in the battery compartment 3 and is used for and the battery 2 The charging interface 8 of electric connection.The shell 10 further includes the locking for being locked in the battery 2 in the battery compartment 3 Device 4.The cell managing device is battery charger or battery check device.
The locking device 4 includes unblock button 41, transmission mechanism 42 and the battery lock for locking the battery 43;The transmission mechanism 42 includes lever 45, and one end of the lever 45 can be connect with the unblock button 41, other end 43 can be latched with the battery to connect.
Wherein, when unlocking the locking device 4, the unblock button 41 is operated, institute is driven by the transmission mechanism 42 It states battery lock 43 and is detached from the battery.
The cell managing device 200 further include be set to it is on the shell 10, for showing charge capacity state Charge reminder device 14.The charge reminder device 14, which can be warning light or other, can show the structure of charge capacity state Or device.
The cell managing device 200 can make battery 2 and connector 5 preferably connect, using 45 He of lever Auxiliary device 6 facilitates the dismounting of battery 2.
In the absence of conflict, the description about the locking device 4 of the cell managing device 200 can refer to institute as above State the description as described in locking device 4 in each embodiment.Embodiment description about the cell managing device 200 can refer to Embodiment in the respective embodiments described above about the rack of unmanned plane 100.Wherein, the shell of the cell managing device 200 10 structure can be considered same or similar with 1 structure of fuselage of the rack 100 of the unmanned plane;It the connector 5 and described fills Electrical interface 8 can be considered that structure is same or similar.Further, the auxiliary device that the a-quadrant in the B area and Fig. 4 in Fig. 9 indicates It is same or like.Accordingly, with respect to the specific structure of the cell managing device 200, details are not described herein again.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all in essence of the invention Within mind and principle, any modification, equivalent substitution, improvement and etc. done be should be included within the scope of the present invention.
This patent document disclosure includes material protected by copyright.The copyright is all for copyright holder.Copyright Owner does not oppose the patent document in the presence of anyone replicates the proce's-verbal of Patent&Trademark Office and archives or should Patent discloses.

Claims (72)

1. a kind of battery fixing mechanism, which is characterized in that including the locking device for fixing battery, the locking device includes Unblock button, transmission mechanism and the battery lock for locking the battery;The transmission mechanism includes lever and shaft, institute The one end for stating lever can be separably attached with the unblock button, and other end can latch separably with the battery Connection;
Wherein, when unlocking the locking device, the unblock button is operated, presses the one of the lever by the unblock button End, the lever are rotated around the shaft, and the other end of the lever drives the battery lock to be detached from the battery.
2. battery fixing mechanism according to claim 1, which is characterized in that one end of the lever and the unblock button It separably abuts, the other end of the lever is separably abutted with battery lock.
3. battery fixing mechanism according to claim 1, which is characterized in that the lever is divided into the first company with rotation center Socket part and second connecting portion, the first connecting portion are connect with the unblock button, the second connecting portion and the battery Lock connection, the length of the first connecting portion are greater than the length of the second connecting portion.
4. battery fixing mechanism according to claim 1, which is characterized in that battery lock include locking piece and with institute State the elastic component of locking piece connection;The elastic component makes the locking piece for providing an elastic-restoring force to the locking piece Battery described in effect force locking based on the elastic component.
5. battery fixing mechanism according to claim 4, which is characterized in that the elastic component includes following at least one:
Compressed spring, extension spring, torsional spring, rubber item, rubber column, metal clips.
6. battery fixing mechanism according to claim 4, which is characterized in that the locking piece includes and the transmission mechanism The interconnecting piece of connection.
7. battery fixing mechanism according to claim 6, which is characterized in that the interconnecting piece includes following at least one:
Abut boss, lantern ring, limiting slot, limited post.
8. battery fixing mechanism according to claim 1, which is characterized in that the battery fixing mechanism further includes auxiliary dress Set, the auxiliary device for supporting the battery, and the auxiliary device abut the battery direction and the battery lock The direction that padlock determines the battery is different.
9. battery fixing mechanism according to claim 8, which is characterized in that the auxiliary device include elastic supporting member for supporting optical member and The sliding part connecting with the elastic supporting member for supporting optical member, the elastic supporting member for supporting optical member abut the electricity for driving the sliding part to slide Pond, to provide an auxiliary force for being detached from the battery out of battery compartment.
10. battery fixing mechanism according to claim 9, which is characterized in that the elastic supporting member for supporting optical member include it is following at least It is a kind of:
Compressed spring, extension spring, torsional spring, rubber item, rubber column, metal clips.
11. battery fixing mechanism according to claim 9, which is characterized in that the elastic supporting member for supporting optical member further includes being set to institute The locating part on battery is stated, the locating part is abutted with the sliding part, for pushing the sliding part.
12. battery fixing mechanism according to claim 11, which is characterized in that the auxiliary device is multiple, and point Not She Yu the battery compartment opposite two inner walls;The locating part is multiple, and is respectively arranged on opposite the two of the battery Side.
13. battery fixing mechanism according to claim 1, which is characterized in that further include guide frame, the battery can Battery compartment, and the guide frame and locking device cooperation fixing institute are slid under the guiding role of the guide frame State battery.
14. battery fixing mechanism according to claim 13, which is characterized in that the guide frame includes being set to the electricity The guide part of the inner wall of Chi Cang and the auxiliary section on the battery, the auxiliary section are matched with the guide part, with The battery is guided to be inserted into the battery compartment.
15. battery fixing mechanism according to claim 14, which is characterized in that the guide part includes following at least one Kind:Guide groove, guide rail, guide post, guide rod;
And/or the auxiliary section includes following at least one:Slide post, sliding slot, guide groove, sleeve.
16. battery fixing mechanism according to claim 14, which is characterized in that the guide part is multiple, and respectively On opposite two inner wall of the battery compartment;
The auxiliary section is multiple, and is respectively arranged on opposite facing two sides of the battery.
17. a kind of rack of unmanned plane, including fuselage, the fuselage is equipped with the battery compartment for placing battery, and is set to institute State the connector in battery compartment for being electrically connected with the battery;It is characterized in that, the fuselage further includes for will be described Battery lock is in the locking device in the battery compartment;
The locking device includes unblock button, transmission mechanism and the battery lock for locking the battery;The transmission Mechanism includes lever and shaft, and one end of the lever can be separably attached with the unblock button, and other end can It is latched with the battery separably attached;
Wherein, when unlocking the locking device, the unblock button is operated, presses the one of the lever by the unblock button End, the lever are rotated around the shaft, and the other end of the lever drives the battery lock to be detached from the battery.
18. the rack of unmanned plane according to claim 17, which is characterized in that pressed with the unlock one end of the lever Button separably abuts, and the other end of the lever is separably abutted with battery lock.
19. the rack of unmanned plane according to claim 17, which is characterized in that the lever is divided into first with rotation center Interconnecting piece and second connecting portion, the first connecting portion are connect with the unblock button, the second connecting portion and the electricity Pond lock connection, the length of the first connecting portion are greater than the length of the second connecting portion.
20. the rack of unmanned plane according to claim 17, which is characterized in that the transmission mechanism includes being placed in the solution At least one described lever below button is locked, the fuselage includes at least one battery compartment, and the locking device includes at least One battery lock;Lever described in wherein at least one is placed in the side of a battery compartment for driving at least one described battery Lock is detached from the battery.
21. the rack of unmanned plane according to claim 17, which is characterized in that battery lock include locking piece and with The elastic component of the locking piece connection;The elastic component makes the locking for providing an elastic-restoring force to the locking piece Battery described in effect force locking of the part based on the elastic component.
22. the rack of unmanned plane according to claim 21, which is characterized in that the elastic component includes following at least one Kind:
Compressed spring, extension spring, torsional spring, rubber item, rubber column, metal clips.
23. the rack of unmanned plane according to claim 21, which is characterized in that the locking piece includes and the driver The interconnecting piece of structure connection.
24. the rack of unmanned plane according to claim 23, which is characterized in that the interconnecting piece includes following at least one Kind:
Abut boss, lantern ring, limiting slot, limited post.
25. the rack of unmanned plane according to claim 17, which is characterized in that the locking device further includes auxiliary dress It sets, the auxiliary device is set on the fuselage for supporting the battery;And the auxiliary device abuts the battery It is different that the direction of the battery from the battery lock padlock is determined in direction.
26. the rack of unmanned plane according to claim 25, which is characterized in that the auxiliary device is used for described in the unlock The all or part of the battery is popped up into the battery compartment after locking device.
27. the rack of unmanned plane according to claim 26, which is characterized in that the auxiliary device is supported in the battery One side on position, close to the battery side middle part or end.
28. the rack of unmanned plane according to claim 25, which is characterized in that the locking device abuts the battery Hold the battery in a first direction with the connector, the another side that the auxiliary device abuts the battery makes The battery is held in a second direction with the connector.
29. the rack of unmanned plane according to claim 28, which is characterized in that the locking device abuts the battery Top surface holds the battery with the connector in said first direction;The auxiliary device abuts the side of the battery Face holds the battery with the connector in this second direction.
30. the rack of unmanned plane according to claim 29, which is characterized in that the auxiliary device is connected to the battery Side on position, the one end being electrically connected far from the battery and the connector.
31. the rack of unmanned plane according to claim 28, which is characterized in that the first direction and the second direction Vertically.
32. the rack of unmanned plane according to claim 25, which is characterized in that the auxiliary device includes elastic supporting member for supporting optical member The sliding part connecting with the elastic supporting member for supporting optical member, the elastic supporting member for supporting optical member is for driving the sliding part to slide and described in abutting Battery, to provide an auxiliary force for being detached from the battery out of battery compartment.
33. the rack of unmanned plane according to claim 32, which is characterized in that the elastic supporting member for supporting optical member include it is following at least It is a kind of:
Compressed spring, extension spring, torsional spring, rubber item, rubber column, metal clips.
34. the rack of unmanned plane according to claim 32, which is characterized in that the elastic supporting member for supporting optical member further includes being set to institute The locating part on battery is stated, the locating part is abutted with the sliding part, for pushing the sliding part.
35. the rack of unmanned plane according to claim 34, which is characterized in that the auxiliary device is multiple, and point Not She Yu the battery compartment opposite two inner walls;The locating part is multiple, and is respectively arranged on opposite the two of the battery Side.
36. the rack of unmanned plane according to claim 32, which is characterized in that the fuselage includes far from the connector The holding tank of setting is equipped at least one described auxiliary device in the holding tank;The battery compartment at least provided with one, until The sliding part of a few auxiliary device extends at least one described battery compartment to support the battery.
37. the rack of unmanned plane described in 7 or 25 according to claim 1, which is characterized in that it further include guide frame, the electricity Pond can slide into battery compartment under the guiding role of the guide frame, and the guide frame and the locking device cooperate Hold the battery.
38. the rack of the unmanned plane according to claim 37, which is characterized in that the guide frame includes being set to the electricity The guide part of the inner wall of Chi Cang and the auxiliary section on the battery, the auxiliary section are matched with the guide part, with The battery is guided to be inserted into the battery compartment.
39. the rack of the unmanned plane according to claim 38, which is characterized in that the guide part includes following at least one Kind:Guide groove, guide rail, guide post, guide rod;
And/or the auxiliary section includes following at least one:Slide post, sliding slot, guide groove, sleeve.
40. the rack of the unmanned plane according to claim 38, which is characterized in that the guide part is multiple, and respectively On opposite two inner wall of the battery compartment;
The auxiliary section is multiple, and is respectively arranged on opposite facing two sides of the battery.
41. the rack of the unmanned plane according to claim 37, which is characterized in that the guide frame is set to the battery compartment Opposite two inner wall on, and the bottom end of the guide frame is flushed with the bottom of the connector so that the battery with The connector fixing.
42. the rack of unmanned plane according to claim 17, which is characterized in that the connector is equipped with construction opening, The battery can be rotated along the construction opening relative to the connector.
43. the rack of unmanned plane according to claim 17, which is characterized in that the locking device locks the battery Direction is vertical with the direction that the battery pull-off goes out the battery compartment.
44. a kind of cell managing device, which is characterized in that including shell, the shell is equipped with the battery compartment for placing battery, And the charging interface in the battery compartment for being electrically connected with the battery;It is characterized in that, the shell also wraps Include for by the battery lock in the locking device in the battery compartment;
The locking device includes unblock button, transmission mechanism and the battery lock for locking the battery;The transmission Mechanism includes lever and shaft, and one end of the lever can be separably attached with the unblock button, and other end can It is latched with the battery separably attached;
Wherein, when unlocking the locking device, the unblock button is operated, presses the one of the lever by the unblock button End, the lever are rotated around the shaft, and the other end of the lever drives the battery lock to be detached from the battery.
45. cell managing device according to claim 44, which is characterized in that pressed with the unlock one end of the lever Button separably abuts, and the other end of the lever is separably abutted with battery lock.
46. cell managing device according to claim 44, which is characterized in that the lever is divided into first with rotation center Interconnecting piece and second connecting portion, the first connecting portion are connect with the unblock button, the second connecting portion and the electricity Pond lock connection, the length of the first connecting portion are greater than the length of the second connecting portion.
47. cell managing device according to claim 44, which is characterized in that the transmission mechanism includes being placed in the solution At least one described lever below button is locked, the shell includes at least one battery compartment, and the locking device includes at least One battery lock;Lever described in wherein at least one is placed in the side of a battery compartment for driving at least one described battery Lock is detached from the battery.
48. cell managing device according to claim 44, which is characterized in that battery lock include locking piece and with The elastic component of the locking piece connection;The elastic component makes the locking for providing an elastic-restoring force to the locking piece Battery described in effect force locking of the part based on the elastic component.
49. cell managing device according to claim 48, which is characterized in that the elastic component includes following at least one Kind:
Compressed spring, extension spring, torsional spring, rubber item, rubber column, metal clips.
50. cell managing device according to claim 48, which is characterized in that the locking piece includes and the driver The interconnecting piece of structure connection.
51. cell managing device according to claim 50, which is characterized in that the interconnecting piece includes following at least one Kind:
Abut boss, lantern ring, limiting slot, limited post.
52. cell managing device according to claim 44, which is characterized in that the cell managing device further includes auxiliary Device, the auxiliary device are set on the shell for supporting the battery;And the auxiliary device abuts the battery From the battery lock padlock to determine the direction of the battery different in direction.
53. cell managing device according to claim 52, which is characterized in that the auxiliary device is used for described in the unlock The all or part of the battery is popped up into the battery compartment after locking device.
54. cell managing device according to claim 53, which is characterized in that the auxiliary device is supported in the battery One side on position, close to the battery side middle part or end.
55. cell managing device according to claim 52, which is characterized in that the locking device abuts the battery Hold the battery in a first direction with the charging interface, the auxiliary device abuts the another side of the battery Hold the battery in a second direction with the charging interface.
56. cell managing device according to claim 55, which is characterized in that the locking device abuts the battery Top surface holds the battery with the charging interface in said first direction;The auxiliary device abuts the one of the battery Side holds the battery with the charging interface in a second direction.
57. cell managing device according to claim 56, which is characterized in that the auxiliary device is connected to the battery Side on position, the one end being electrically connected far from the battery and the charging interface.
58. cell managing device according to claim 55, which is characterized in that the first direction and the second direction Vertically.
59. cell managing device according to claim 52, which is characterized in that the auxiliary device includes elastic supporting member for supporting optical member The sliding part connecting with the elastic supporting member for supporting optical member, the elastic supporting member for supporting optical member is for driving the sliding part to slide and described in abutting Battery, to provide an auxiliary force for being detached from the battery out of battery compartment.
60. cell managing device according to claim 59, which is characterized in that the elastic supporting member for supporting optical member include it is following at least It is a kind of:
Compressed spring, extension spring, torsional spring, rubber item, rubber column, metal clips.
61. cell managing device according to claim 59, which is characterized in that the elastic supporting member for supporting optical member further includes being set to institute The locating part on battery is stated, the locating part is abutted with the sliding part, for pushing the sliding part.
62. cell managing device according to claim 61, which is characterized in that the auxiliary device is multiple, and point Not She Yu the battery compartment opposite two inner walls;The locating part is multiple, and is respectively arranged on opposite the two of the battery Side.
63. cell managing device according to claim 59, which is characterized in that the shell includes far from the charging The holding tank of mouthful setting, is equipped at least one described auxiliary device in the holding tank;The battery compartment at least provided with one, The sliding part of at least one auxiliary device extends at least one described battery compartment to support the battery.
64. the cell managing device according to claim 44 or 52, which is characterized in that it further include guide frame, the electricity Pond can slide into battery compartment under the guiding role of the guide frame, and the guide frame and the locking device cooperate Hold the battery.
65. cell managing device according to claim 64, which is characterized in that the guide frame includes being set to the electricity The guide part of the inner wall of Chi Cang and the auxiliary section on the battery, the auxiliary section are matched with the guide part, with The battery is guided to be inserted into the battery compartment.
66. cell managing device according to claim 65, which is characterized in that the guide part includes following at least one Kind:Guide groove, guide rail, guide post, guide rod;
And/or the auxiliary section includes following at least one:Slide post, sliding slot, guide groove, sleeve.
67. cell managing device according to claim 65, which is characterized in that the guide part is multiple, and respectively On opposite two inner wall of the battery compartment;
The auxiliary section is multiple, and is respectively arranged on opposite facing two sides of the battery.
68. cell managing device according to claim 64, which is characterized in that the guide frame is set to the battery compartment Opposite two inner wall on, and the bottom end of the guide frame is flushed with the bottom of the connector so that the battery with The connector fixing.
69. cell managing device according to claim 44, which is characterized in that the charging interface is equipped with installation and opens Mouthful, the battery can be rotated along the construction opening relative to the charging interface.
70. cell managing device according to claim 44, which is characterized in that the locking device locks the battery Direction is vertical with the direction that the battery pull-off goes out the battery compartment.
71. cell managing device according to claim 44, which is characterized in that the cell managing device further includes setting In charge reminder device on the shell, for showing charge capacity state.
72. cell managing device according to claim 44, which is characterized in that the cell managing device is battery charging Device or battery check device.
CN201680003746.5A 2016-12-28 2016-12-28 Battery fixing mechanism, the rack of unmanned plane and cell managing device Expired - Fee Related CN107112464B (en)

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