CN208593501U - Device for quickly disassembling and unmanned plane - Google Patents
Device for quickly disassembling and unmanned plane Download PDFInfo
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- CN208593501U CN208593501U CN201821151317.5U CN201821151317U CN208593501U CN 208593501 U CN208593501 U CN 208593501U CN 201821151317 U CN201821151317 U CN 201821151317U CN 208593501 U CN208593501 U CN 208593501U
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- support
- limit assembly
- quickly disassembling
- interconnecting piece
- hole
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Abstract
A kind of device for quickly disassembling and unmanned plane.Device for quickly disassembling includes the first support;Second support is rotatably dispose in the first support, can rotate around first direction relative to the first support, equipped with the interconnecting piece connecting with outer structural parts;First limit assembly is flexibly connected with the first support, can be moved along first direction relative to the first support;Set on the second limit assembly of the first support, for limiting the second support around the position that first direction rotates;When the first limit assembly is in first state along first direction, the second support is abutted with the first limit assembly, and so that interconnecting piece and the first support is formed enclosure space in first position by the limit of the second limit assembly, outer structural parts are locked in interconnecting piece;When the first limit assembly is in the second state along first direction, the second support can be rotated around first direction and be limited by the second limit assembly in the second position, and interconnecting piece be made to be in open state, by outer structural parts and coupling part from.
Description
Technical field
The utility model relates to air vehicle technique field, in particular to a kind of device for quickly disassembling and unmanned plane.
Background technique
Unmanned plane of taking photo by plane in the industry requires to carry holder at present, when needing to dismount holder, be usually all from
Lower part is dismounted, if unmanned machine head is the setting shield of closure, need to be dismounted together with shield, could be incited somebody to action
Holder is dismantled, complicated for operation, also adds the risk in structure.
Therefore, how quickly and easily holder to be dismounted, is this field urgent problem to be solved.
Utility model content
The utility model provides a kind of device for quickly disassembling and unmanned plane, and fast assembling-disassembling between holder and unmanned plane may be implemented.
According to the utility model embodiment in a first aspect, providing a kind of device for quickly disassembling, comprising:
First support;
Second support is rotatably dispose in the side surface of first support, and second support can be opposite around first direction
The first support rotation;Second support is equipped with the interconnecting piece for being cooperatively connected with outer structural parts;
First limit assembly is flexibly connected with first support, and first limit assembly can be along the first direction
It is mobile relative to first support;
Set on the second limit assembly of first support, rotated for limiting second support around the first direction
Position;
When first limit assembly is in first state along the first direction, second support and described first
Limit assembly abuts;Second support is limited in first position, so that the interconnecting piece by second limit assembly
Enclosure space is formed with first support, the outer structural parts are locked in the interconnecting piece;
When first limit assembly is in the second state along the first direction, second support can be around described
One direction rotates and passes through second limit assembly and limits second support in the second position, so that at the interconnecting piece
In open state, by the outer structural parts and the coupling part from.
Further, the side surface of first support is formed with concave part, and the concave part is by first support
Side wall surrounds, and second support and first limit assembly are housed in the concave part, and the first direction is institute
State the depth direction of concave part.
Further, the interconnecting piece is slot, and the slot includes interface;The device for quickly disassembling locks the outside
When structural member, the interface and the side wall form enclosure space.
Further, the side wall of the concave part is formed with notch section, and the outer structural parts are torn open from the device for quickly disassembling
Except when, the interconnecting piece is connected to the notch section.
Further, second limit assembly includes the elastic component that rotation connection is kept with second support, described
Elastic component provides second support pretightning force rotated around the first direction.
Further, the elastic component is torsional spring, and the side surface of first support is formed with receiving portion, the elastic component
Be sheathed on outside the receiving portion, second support is sheathed on outside the receiving portion and the elastic component, and with the elastic component
Keep rotation connection.
Further, the side surface of second support is equipped with first through hole, is equipped with bearing, the axis in the receiving portion
It holds and is equipped with connection through-hole corresponding with the first through hole position, be equipped with jointly in the first through hole and the connection through-hole
The fastener being connect with the receiving portion.
Further, second limit assembly include be formed in the side surface of first support the first stopper section and
Second stopper section;
When the device for quickly disassembling locks the outer structural parts, the side of second support and first limit assembly
It abuts, the other side of second support is abutted with first stopper section;
When the outer structural parts are removed from the device for quickly disassembling, second support is abutted with second stopper section.
Further, the side surface of first support is formed with concave part, and the concave part is by first support
Side wall surrounds;The side wall of first stopper section and second stopper section along the concave part extends inwardly to form.
Further, the side wall of the concave part is formed with notch section, and the outer structural parts are torn open from the device for quickly disassembling
Except when, the interconnecting piece is connected to the notch section;First stopper section and second stopper section are located at described lack
The two sides of oral area.
Further, first limit assembly include: be set to the side surface of first support mandril and with institute
State the stop block of mandril connection;
The mandril can be moved along the first direction, to drive the stop block to move along the first direction, so that
Second support is abutted or is separated with the stop block.
Further, the side surface of first support is equipped with the second through-hole, and the mandril and the stop block are set respectively
It is placed in the two sides of first support;The mandril is arranged in second through-hole and part protrudes from first support, institute
It states stop block and is connect with the part that the mandril protrudes from first support.
Further, second through-hole is stepped hole, is equipped with pressure spring in the stepped hole in the biggish hole in aperture, described
Compression spring sleeve is set to the mandril.
Further, second support is formed with limiting section close to the side of first limit assembly;
It is located at described the when first limit assembly is in first state and second support along the first direction
When one position, the limiting section is abutted along the rotation direction of second support with the stop block;
It is located at described the when first limit assembly is in the second state and second support along the first direction
When two positions, the limiting section is abutted along the first direction with the stop block.
According to the second aspect of the utility model embodiment, a kind of unmanned plane is provided, including fuselage, be installed in the fuselage
Mounting bracket and the cradle head structure that is detachably connected with the mounting bracket;Wherein, the mounting bracket includes such as taking up an official post
Device for quickly disassembling described in one embodiment, the cradle head structure are equipped with the knot being cooperatively connected with the interconnecting piece of the device for quickly disassembling
Component.
Further, the mounting bracket includes being installed in the annular frame of the fuselage and being symmetrically disposed on the annular
Two device for quickly disassembling of frame body, the two sides of the cradle head structure are equipped with the structural member.
The device for quickly disassembling of the utility model, by the cooperation of the first limit assembly and the second limit assembly, to the second support
Position limited so that interconnecting piece switches between closed state and open state, outer structural parts are locked with realizing
In interconnecting piece, or by outer structural parts and coupling part from.The simple structure, high reliability, and it is easy to operate, it is easy to tear open
Dress.
Detailed description of the invention
Fig. 1 is a kind of stereoscopic schematic diagram of device for quickly disassembling shown in the utility model embodiment.
Fig. 2 is a kind of perspective view of the explosion of device for quickly disassembling shown in the utility model embodiment.
Fig. 3 is the schematic diagram that a kind of device for quickly disassembling shown in the utility model embodiment is in a kind of state.
Fig. 4 is the side view of Fig. 3.
Fig. 5 is the schematic diagram that a kind of device for quickly disassembling shown in the utility model embodiment is in another state.
Fig. 6 is the side view of Fig. 5.
Fig. 7 is a kind of mandril of device for quickly disassembling shown in the utility model embodiment and the connection schematic diagram of the first support.
Fig. 8 is a kind of stereoscopic schematic diagram of unmanned plane shown in the utility model embodiment.
Stereoscopic schematic diagram when Fig. 9 is a kind of unmanned machine head locking shown in the utility model embodiment.
Figure 10 is the partial enlargement diagram of device for quickly disassembling and annular frame in Fig. 9.
Figure 11 is stereoscopic schematic diagram when a kind of unmanned machine head shown in the utility model embodiment is removed.
Figure 12 is the partial enlargement diagram of device for quickly disassembling and annular frame in Figure 11.
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 consistent with the utility model.On the contrary, they be only with such as
The example of the consistent device and method of some aspects be described in detail in the appended claims, the utility model.
It is only to be not intended to be limiting this reality merely for for the purpose of describing particular embodiments in the term that the utility model uses
With novel.In the "an" of the utility model and singular used in the attached claims, " described " and "the"
Most forms are intended to include, unless the context clearly indicates other meaning.It is also understood that term used herein " and/
Or " refer to and include that one or more associated any or all of project listed may combine.
It should be appreciated that " first " " second " and similar word used in present specification and claims
It is not offered as any sequence, quantity or importance, and is used only to distinguish different component parts.Equally, "one" or
The similar word such as " one " does not indicate that quantity limits yet, but indicates that there are at least one.Unless otherwise noted, " front ", " after
The similar word such as portion ", " lower part " and/or " top " is not limited to a position or a kind of sky only to facilitate explanation
Between orient.The similar word such as " comprising " or "comprising" means to appear in element or object before " comprising " or "comprising"
Cover the element for appearing in " comprising " or "comprising" presented hereinafter or object and its equivalent, it is not excluded that other elements or
Object." connection " either the similar word such as " connected " is not limited to physics or mechanical connection, and may include
Electrical connection, it is either direct or indirect.
The utility model provides a kind of device for quickly disassembling and unmanned plane.With reference to the accompanying drawing, to the fast dismounting of the utility model
It sets and unmanned plane is described in detail.In the absence of conflict, the feature in following embodiment and embodiment can phase
Mutually combination.
Referring to Figure 1 and shown in Fig. 2, the embodiment of the present application provides a kind of device for quickly disassembling 100, can conveniently and efficiently and outside
Portion's structural member is dismounted.The device for quickly disassembling 100 includes: the first support 10, the second support 20 and is used for the second support 20
The first limit assembly 30 limited and the second limit assembly.
Wherein, second support 20 is equipped with the interconnecting piece 21 for being cooperatively connected with outer structural parts.Second support 20
It is rotatably dispose in the side surface of first support 10, the second support 20 can be 10 turns of first support relatively described around first direction X
It is dynamic.
First limit assembly 30 is flexibly connected with first support 10, and first limit assembly 30 can be along described first
Direction X is mobile relative to first support 10, to limit or allow the second support 20 to rotate around first direction X.
Second limit assembly is set to first support 10, rotates for limiting second support 20 around first direction X
Position.
In conjunction with shown in Fig. 3 and Fig. 4, when first limit assembly 30 is moved to along the first direction X in the first shape
When state, second support 20 is abutted with first limit assembly 30, is rotated with limiting the second support 20 around first direction X,
Specifically, second support 20 includes side 29, and the side 29 is abutted with first limit assembly 30.Pass through described
Two limit assemblies limit second support 20 in first position, so that the interconnecting piece 21 and first support 10 formation
The outer structural parts 81 are locked in the interconnecting piece 21 by enclosure space.
In conjunction with shown in Fig. 5 and Fig. 6, when first limit assembly 30 is moved to along the first direction X in the second shape
When state, the side 29 is separated with first limit assembly 30, to allow the second support 20 to rotate around first direction X.At this point,
Second support 20 can turn left around the first direction X and pass through second limit assembly for second support 20
Limit is in the second position, so that the interconnecting piece 21 is in open state, by the outer structural parts 81 and the interconnecting piece
21 separation.Realize the fast assembling-disassembling of outer structural parts 81.
By above-described embodiment, it can be concluded that, the device for quickly disassembling 100 of the utility model passes through the first limit assembly 30 and second
The cooperation of limit assembly can limit the position of the second support 20, so that interconnecting piece 21 is in closed state and open shape
Switch between state, outer structural parts 81 is locked in interconnecting piece 21 to realize, or outer structural parts 81 and interconnecting piece 21 are divided
From the fast assembling-disassembling of realization outer structural parts 81.100 simple structure, high reliability of device for quickly disassembling, and it is easy to operate, it is easy to
Dismounting.
In an optional embodiment, the side surface of first support 10 is formed with concave part 12, the first party
It is the depth direction of the concave part 12 to X.The concave part 12 is surrounded by the side wall 121 of first support 10, and described
Two supports 20, first limit assembly 30 and second limit assembly are housed in the concave part 12.Optionally,
The side wall 121 of first support 10 is arcuate structure compatible with the rotary motion trace of second support 20, it is ensured that
The aesthetics of 100 overall appearance of device for quickly disassembling.
Certainly, in other embodiments, second support 20, first limit assembly 30 and second limit
Component also can be arranged directly on the side surface of the first support 10 without concave part 12 is arranged, and can achieve identical effect.
Why in the side surface of the first support 10 concave part 12 is set, and by the second support 20, the first limit assembly 30 and second
Limit assembly is housed in the concave part 12, can achieve the effect for saving space and material.
In an optional embodiment, the interconnecting piece 21 is slot, and the slot includes interface 22.When described fast
When dismantling device 100 locks the outer structural parts 81, the side wall 121 of the interface 22 and first support 10, which is formed, to be closed
Space.
When first limit assembly 30 is moved to along the first direction X in first state, second support
20 side 29 is abutted with first limit assembly 30, is rotated with limiting the second support 20 around first direction X.Pass through described
Two limit assemblies limit second support 20 in first position, so that the interface 22 of the interconnecting piece 21 and described first
The side wall 121 of support 10 forms enclosure space, to guarantee that outer structural parts 81 are locked in the interface 22 of interconnecting piece 21.
Further, the side wall 121 of the concave part 12 is formed with notch section 13, and the outer structural parts 81 are from described fast
When dismantling device 100 is removed, the interface 22 of the interconnecting piece 21 is connected to the notch section 13.
When first limit assembly 30 is moved to along the first direction X in the second state, second support
20 side 29 is separated with first limit assembly 30, to allow the second support 20 to rotate around first direction X.At this point, described
Second support 20 can turn left around the first direction X and pass through second limit assembly and limit second support 20
In the second position, it is connected to the interface 22 of the interconnecting piece 21 with the notch section 13, i.e., the described interconnecting piece 21, which is in, to be opened
State carries out realization outer structural parts to allow to separate the outer structural parts 81 with the interface 22 of the interconnecting piece 21
81 fast assembling-disassembling.
In an optional embodiment, second limit assembly includes keeping being rotatablely connected with second support 20
Elastic component 17, the elastic component 17 provides the pretightning force that rotates around the first direction X to second support 20.
In one example, (interconnecting piece 21 and first support 10 formation when the second support 20 is located at first position
When enclosure space), the elastic component 17 is in original state.Under usual state, the second support 20 is located at first position, the first limit
Hyte part 30 is in first state along first direction X.
When needing for outer structural parts 81 to be locked in interconnecting piece 21, first by the first limit assembly 30 along first direction X
It is moved in the second state, then the second support 20 is turned left around first direction X to the second position, so that the interconnecting piece
21 are in open state, and outer structural parts 81 are assembled in interconnecting piece 21.The elastic component 17 is to described second at this time
Seat 20 provides the pretightning force to turn right around first direction X.
Outer structural parts 81 unclamp the second support 20, preload of the elastic component 17 to the second support 20 after being packed into interconnecting piece 21
Power is changed into the reset force of driving the second support 20 rebound, so that the second support 20 turns right around first direction X to returning to the
Then first limit assembly 30 is moved to along first direction X in first state, makes interconnecting piece 21 and described first by one position
Support 10 forms enclosure space, and the second support 20 is made to return back to first state, the side 29 and first limit assembly 30
It abuts, outer structural parts 81 is locked in interconnecting piece 21.
When needing to separate outer structural parts 81 with interconnecting piece 21, first by first limit assembly 30 along described first
Direction X, which is moved to, separates the side 29 of the second support 20 with the first limit assembly 30.Again by the second support
20 turn left around first direction X to the second position, so that the interconnecting piece 21 is in open state, by outer structural parts 81
It is separated with interconnecting piece 21.
In another example, when the second support 20 is located at the second position (when interconnecting piece 21 is in open state), institute
It states elastic component 17 and is in original state.Under usual state, the second support 20 is located at first position, and the first limit assembly 30 is along first
Direction X is in first state.The elastic component 17 turns left to second support 20 offer around first direction X pre- at this time
Clamp force.
When needing for outer structural parts 81 to be locked in interconnecting piece 21, first by the first limit assembly 30 along first direction X
It is moved in the second state, separates the side 29 of the second support 20 with the first limit assembly 30.Elastic component 17 is at this time
The pretightning force of two supports 20 be changed into driving the second support 20 rebound reset force so that the second support 20 around first direction X to
A left side, which turns to, returns to the second position, and the interconnecting piece 21 is made to be in open state, and outer structural parts 81 are assembled to interconnecting piece
In 21.
Outer structural parts 81 again turn right the second support 20 to returning to the around first direction X after being packed into interconnecting piece 21
Then first limit assembly 30 is moved to the side 29 for making the second support 20 in first state by one position along first direction X
It is abutted with first limit assembly 30, and then interconnecting piece 21 and first support 10 is made to form enclosure space, it will be external
Structural member 81 is locked in interconnecting piece 21.The elastic component 17 provides around first direction X to the left second support 20 at this time
The pretightning force of rotation.
When needing to separate outer structural parts 81 with interconnecting piece 21, first by first limit assembly 30 along described first
Direction X, which is moved to, separates the side 29 of the second support 20 with the first limit assembly 30.Second support at this time
20 turn left around first direction X to the second position is returned to, so that the interconnecting piece 21 again under the pretightning force of elastic component 17
In open state, outer structural parts 81 are separated with interconnecting piece 21.
It should be noted that can also then be wanted with no restrictions to the state of elastic component 17 in the embodiment described above
The second support 20 is kept to need in the second position by manpower.In an optional embodiment, the elastic component 17 is torsional spring,
The side surface of first support 10 is formed with receiving portion 16, and the torsion spring set is set to outside the receiving portion 16, and described second
Seat 20 is sheathed on outside the receiving portion 16 and the torsional spring, and keeps being rotatablely connected with the torsional spring.Wherein, the torsional spring includes
Main part 171 and by main part 171 extends two twist joint portion 172, twist joint portion 172 for two and be equipped with towards being reversed
Twist joint 173.Interconnecting piece 21, which is equipped with, twists joint hole 211 with described two compatible two first of portions 172 of twisting joint.First support
It is again provided on 10 and twists joint hole 101 with stating two and twist joint compatible two second of portion 172.
What one of twist joint 173 of the torsional spring was installed in interconnecting piece 21 twists joint hole 211, institute positioned at the first of left side
State another of torsional spring twist joint 173 be installed in the first support 10 be located at right side second twist joint hole 101.In this way, when second
When support 20 rotates, the corresponding portion 172 of twisting joint of the torsional spring can be driven to rotate together, so that torsional spring generates deformation, in turn
The pretightning force rotated around first direction X is provided the second support 20.
Further, the side surface of second support 20 is equipped with first through hole 23, is equipped with bearing in the receiving portion 16
24, the bearing 24 is equipped with connection through-hole 241 corresponding with 23 position of first through hole, the first through hole 23 and the company
It connects in hole 241 and is equipped with the fastener 25 connecting with the receiving portion 16 jointly.Wherein, the bearing 24 is housed in the receipts
In appearance portion 16, and height is slightly above the receiving portion 16, can open up threaded hole in receiving portion 16, fastener 25 can use
With the screw of threaded hole cooperation.The torsion spring set is set to outside the receiving portion 16, and second support 20 is sheathed on the receiving
It keeps being rotatablely connected with the torsional spring outside portion 16 and the torsional spring, and is abutted with the bearing 24.It is worn by the fastener 25
Cross after first through hole 23 and connection through-hole 241 with the screw hole in the receiving portion 16, and then by the second support 20 and the
The position of one support 10 is fixed, and the second support 20 can be rotated by the torsional spring relative to the first support 10.
In an optional embodiment, second limit assembly can also include being formed in first support 10
The first stopper section 14 and the second stopper section 15 of side surface.Optionally, first stopper section 14 and second stopper section 15
Side wall 121 along the concave part 12 extends inwardly to form.First stopper section 14 and second stopper section 15 difference
Positioned at the two sides of the notch section 13, the distance between first stopper section 14 and second stopper section 15 are greater than described lack
Oral area 13.
When first limit assembly 30 is moved to along the first direction X in first state, second support
20 side 29 is abutted with first limit assembly 30, and (as shown in the figure is second for the other side of second support 20
The right side 291 of seat 20) it is abutted with first stopper section 14, to limiting the second support 20 in first position, so that institute
The side wall 121 of the interface 22 and first support 10 of stating interconnecting piece 21 forms enclosure space, to guarantee outer structural parts 81
It is locked in the interface 22 of interconnecting piece 21.
When first limit assembly 30 is moved to along the first direction X in the second state, second support
20 side 29 is separated with first limit assembly 30, to allow the second support 20 to turn left around first direction X.At this point,
Second support 20 can turn left to second stopper section 15 around the first direction X and abut, thus by described
Two supports 20 are limited in the second position, are connected to the interface 22 of the interconnecting piece 21 with the notch section 13, i.e., the described connection
Portion 21 is in open state, to allow to separate the outer structural parts 81 with the interface 22 of the interconnecting piece 21, carries out real
The fast assembling-disassembling of existing outer structural parts 81.
It should be noted that the second limit assembly of the device for quickly disassembling 100 of the application can be by elastic component 17, the first backstop
Portion 14 and the second stopper section 15 are used in combination, to reach better limit effect.Of course for structure is simplified, can also only have
Any limit assembly in elastic component 17 or the first stopper section 14 or the second stopper section 15.
When elastic component 17, the first stopper section 14 and the second stopper section 15 are used in combination the second limit assembly.Work as institute
When stating the first limit assembly 30 and being moved to along the first direction X in first state, the side 29 of second support 20
It is abutted with first limit assembly 30, (as shown in the figure is the right side of the second support 20 for the other side of second support 20
291) it is abutted with first stopper section 14, and pretightning force can be provided to the second support 20 by elastic component 17, thus by second
The limit of support 20 is in first position, so that the formation of the side wall 121 of the interface 22 of the interconnecting piece 21 and first support 10
Enclosure space, to guarantee that outer structural parts 81 are locked in the interface 22 of interconnecting piece 21.
When first limit assembly 30 is moved to along the first direction X in the second state, second support
20 separate with first limit assembly 30, to allow the second support 20 to turn left around first direction X.At this point, described second
Support 20 can turn left to second stopper section 15 around the first direction X and abut, and can be by elastic component 17 to
Two supports 20 provide pretightning force, to limiting second support 20 in the second position, make the interface of the interconnecting piece 21
22 are connected to the notch section 13, i.e., the described interconnecting piece 21 is in open state, to allow the outer structural parts 81 and institute
The interface 22 for stating interconnecting piece 21 separates, and carries out the fast assembling-disassembling for realizing outer structural parts 81.When elastic component 17, the first stopper section
14 and second stopper section 15 be used in combination when, the state of elastic component 17 does not need when being at different location to the second support 20
Carry out any restrictions.
In an optional embodiment, first limit assembly 30 includes: the side for being set to first support 10
The mandril 31 on surface and the stop block 32 being connect with the mandril 31.The mandril 31 can be moved along the first direction X, with band
It moves the stop block 32 to move along the first direction, so that the side 29 of second support 20 is abutted with the stop block 32
Or separation.
It is described when the mandril 31 drives the stop block 32 to be moved to along the first direction X in first state
The side 29 of second support 20 is abutted with the stop block 32.When first limit assembly 30 is moved along the first direction X
To when being in the second state, the side 29 of second support 20 is separated with the stop block 32.
In an optional embodiment, the side surface of first support 10 is equipped with the second through-hole 102, the mandril 31
The two sides of first support 10 are respectively arranged at the stop block 32.The mandril 31 is arranged in second through-hole 102
And part protrudes from first support 10, the stop block 32 protrudes from the part of first support 10 with the mandril 31
Connection.Optionally, the mandril 31 protrude from first support 10 part be equipped with threaded portion, the stopper section 32 be equipped with
The threaded hole that the threaded portion matches.
Shown in Figure 7, further, the mandril 31 includes the body of rod 311 and the press section for being connected to 311 end of the body of rod
312, the body of rod 311 is arranged in second through-hole 102 and part protrudes from first support 10, and the body of rod 311 is convex
Part for first support 10 is equipped with threaded portion 313.Second through-hole 102 is stepped hole, including aperture is biggish
Lesser second hole 1022 in first hole 1021 and aperture, wherein the second hole 1022 is located at the same of the first support 10 with the second support 20
Side.The other side of the body of rod 311 from the first support 10 is arranged in second through-hole 102, so that press section 312 and the second support
20 are located at the two sides of the first support 10.
Optionally, pressure spring 33 is equipped in first hole 1021, the pressure spring 33 is sheathed on the body of rod 311, and institute
The both ends for stating pressure spring 33 are abutted with the side wall of press section 312 and the second hole 1022 respectively.In this way, when by the mandril 31 along described
First direction X is moved to after the second state, and the pressure spring 33 is in compressive state.After unclamping mandril 31, mandril 31 can be with
First state is automatically returned to by the elastic acting force of the pressure spring 33.
Referring to shown in Fig. 3 and Fig. 5, in an optional embodiment, second support 20 is close to first limit
The side of component 30 is formed with limiting section 27.When first limit assembly 30 is in first state and institute along the first direction
When stating the second support 20 and being located at the first position, the side 29 of the limiting section 27 is (that is, the side of the second support 20
29) it is abutted along the rotation direction of second support 20 with the stop block 32, as shown in figure 3, can be risen to the second support 20
To position-limiting action.When first limit assembly 30 is moved to the second state and second support 20 shifting along the first direction
When moving to the second position, the second support 20 drives limiting section 27 to turn left along first direction X, and the mandril 31 is in pressure spring
It abuts the stop block 32 along the end face of the first direction 28 with the limiting section 27, passes through limit
Abutting contact of the block 32 between first direction and limiting section 27, mutually abutting the frictional force generated between the two can both prevent
The rebound of second support 20, and can prevent stop block 32 from springing back, limit can be played to the second support 20 and stop block 32 simultaneously
Effect.After rotating to the right the second support 20 is detached from the end face 28 of limiting section 27 and stop block 32, the stop block 32 is being pressed
It can be moved to along first direction under the active force of spring 33 and be restored to first state, so that the side of the limiting section 27 of the second support 20
Face 29 can be abutted along the rotation direction of second support 20 with the stop block 32, and then the second support 20 is maintained at
One position.
In the preferred embodiment, the device for quickly disassembling 100 of the application, when first limit assembly 30 is along the first direction
When X is in first state, the side 29 of second support 20 is limited along the rotation direction of second support 20 and described first
The stop block 32 of hyte part 30 abuts, and (as shown in the figure is the right side of the second support 20 for the other side of second support 20
291) it is abutted along the rotation direction of second support 20 with first stopper section 14, and can be by elastic component 17 to second
Seat 20 provides pretightning force, to limiting the second support 20 in first position, so that the interface 22 of the interconnecting piece 21 and institute
The side wall 121 for stating the first support 10 forms enclosure space, to guarantee that outer structural parts 81 are locked in the interface of interconnecting piece 21
In 22, as shown in Figure 3.
When needing to separate outer structural parts 81 with the interconnecting piece 21 of the second support 20, by first limit assembly 30
Be moved to along the first direction X in the second state so that the side 29 of the second support 20 and the first limit assembly 30 only
Block 32 separates.Second support 20 turns left to the second position and abuts with second stopper section 15, by described
Two supports 20 are limited in the second position, are connected to the interface 22 of the interconnecting piece 21 with the notch section 13, i.e., the described connection
Portion 21 is in open state, to allow to separate the outer structural parts 81 with the interface 22 of the interconnecting piece 21, carries out real
The fast assembling-disassembling of existing outer structural parts 81, as shown in Figure 5.The mandril 31 makes the stop block under the active force of pressure spring 33
32 abut with the limiting section 27 along the end face of the first direction 28, by limited block 32 along first direction and limiting section 27 it
Between abutting contact, mutually abutting the frictional force generated between the two can not only prevent the second support 20 from springing back, but also can prevent
Stop block 32 is sprung back, and can play position-limiting action to the second support 20 and stop block 32 simultaneously.
Accordingly, it is desirable to when outer structural parts 81 are packed into the interface 22 of interconnecting piece 21, by first limit assembly
30 are in the second state along the first direction X and turn to the second support 20 positioned at the second position, by outer structural parts 81
Rotating to the right the second support 20 after the interface 22 of loading interconnecting piece 21 again is detached from the end face 28 of limiting section 27 and stop block 32,
The stop block 32 can be moved under the active force of pressure spring 33 along first direction is restored to first state, so that the second support
The side 29 of 20 limiting section 27 can be abutted along the rotation direction of second support 20 with the stop block 32, and then by
Two supports 20 are maintained at first position again, so that the side wall of the interface 22 of the interconnecting piece 21 and first support 10
121 form enclosure space, to guarantee that outer structural parts 81 are locked in the interface 22 of interconnecting piece 21.
Shown in Figure 8, the embodiment of the present application also provides a kind of unmanned plane 200, including fuselage 90, is installed in the fuselage
90 mounting bracket and the cradle head structure 80 being detachably connected with the mounting bracket.Wherein, the mounting bracket includes fast
Dismantling device 100, the cradle head structure 80 are equipped with the structural member being cooperatively connected with the interconnecting piece 21 of the device for quickly disassembling 100
81.It should be noted that the description as described in the device for quickly disassembling 100 in above-described embodiment and embodiment, is equally applicable to this
The unmanned plane 200 of application.
Shown in Figure 9, in an optional embodiment, the mounting bracket includes the ring for being installed in the fuselage 90
Shape frame body 91 and two device for quickly disassembling 100 for being symmetrically disposed on the annular frame 91, the two sides of the cradle head structure 80
It is equipped with the structural member 81.It can guarantee that the connection between cradle head structure 80 and the fuselage 90 of unmanned plane 200 is more firm.
Referring to shown in Fig. 9 and Figure 10, when cradle head structure 80 needs to assemble with the mounting bracket, pass through the fast dismounting of rotation
100 the second support 20 is set, the structural member 81 of cradle head structure 80 can be locked in the connection of the device for quickly disassembling 100 of mounting bracket
In portion 21, and then realize that cradle head structure 80 is installed to the fuselage 90 of unmanned plane 200.
Referring to shown in Figure 11 and Figure 12, when needing to remove cradle head structure 80, pass through the second of rotation device for quickly disassembling 100
Support 20 can separate the structural member 81 of cradle head structure 80 with the interconnecting piece 21 of the device for quickly disassembling 100 of mounting bracket, Jin Ershi
Existing cradle head structure 80 is removed from the fuselage 90 of unmanned plane 200.To replace the equipment of taking photo by plane of unmanned plane 200.
The above is only the preferred embodiment of the utility model, not does in any form to the utility model
Limitation, although the utility model has been disclosed with preferred embodiment as above, is not intended to limit the utility model, any to be familiar with
Professional and technical personnel, in the range of not departing from technical solutions of the utility model, when in the technology using the disclosure above
Hold the equivalent embodiment for being modified or being modified to equivalent variations, but all without departing from technical solutions of the utility model
Hold, any simple modification, equivalent change and modification made by the above technical examples according to the technical essence of the present invention, still
It is within the scope of the technical solutions 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 (16)
1. a kind of device for quickly disassembling characterized by comprising
First support;
Second support, is rotatably dispose in the side surface of first support, and second support can be relatively described around first direction
The rotation of first support;Second support is equipped with the interconnecting piece for being cooperatively connected with outer structural parts;
First limit assembly is flexibly connected with first support, and first limit assembly can be opposite along the first direction
First support is mobile;
Set on the second limit assembly of first support, for limiting second support around the position that the first direction rotates
It sets;
When first limit assembly is in first state along the first direction, second support and first limit
Component abuts;Second support is limited in first position, so that the interconnecting piece and institute by second limit assembly
It states the first support and forms enclosure space, the outer structural parts are locked in the interconnecting piece;
When first limit assembly is in the second state along the first direction, second support can be around the first party
To rotating and being limited second support in the second position by second limit assembly, opened so that the interconnecting piece is in
Put state, by the outer structural parts and the coupling part from.
2. device for quickly disassembling according to claim 1, which is characterized in that the side surface of first support forms fluted
Portion, the concave part are surrounded by the side wall of first support, and second support and first limit assembly are housed in
In the concave part, the first direction is the depth direction of the concave part.
3. device for quickly disassembling according to claim 2, which is characterized in that the interconnecting piece is slot, and the slot includes inserting
Interface;When the device for quickly disassembling locks the outer structural parts, the interface and the side wall form enclosure space.
4. device for quickly disassembling according to claim 2, which is characterized in that the side wall of the concave part is formed with notch section, institute
When stating outer structural parts and removing from the device for quickly disassembling, the interconnecting piece is connected to the notch section.
5. device for quickly disassembling according to claim 1, which is characterized in that second limit assembly includes and described second
Seat keeps the elastic component of rotation connection, and the elastic component provides second support preload rotated around the first direction
Power.
6. device for quickly disassembling according to claim 5, which is characterized in that the elastic component is torsional spring, first support
Side surface is formed with receiving portion, and the elastic component is sheathed on outside the receiving portion, and second support is sheathed on the receiving portion
And outside the elastic component, and keep being rotatablely connected with the elastic component.
7. device for quickly disassembling according to claim 6, which is characterized in that it is logical that the side surface of second support is equipped with first
Hole, is equipped with bearing in the receiving portion, and the bearing is equipped with connection through-hole corresponding with the first through hole position, and described first
It is equipped with the fastener connecting with the receiving portion jointly in through-hole and the connection through-hole.
8. device for quickly disassembling according to claim 1 or claim 7, which is characterized in that second limit assembly includes being formed in institute
State the first stopper section and the second stopper section of the side surface of the first support;
When the device for quickly disassembling locks the outer structural parts, the side of second support is supported with first limit assembly
It connects, the other side of second support is abutted with first stopper section;
When the outer structural parts are removed from the device for quickly disassembling, second support is abutted with second stopper section.
9. device for quickly disassembling according to claim 8, which is characterized in that the side surface of first support forms fluted
Portion, the concave part are surrounded by the side wall of first support;First stopper section and second stopper section are along described
The side wall of concave part extends inwardly to form.
10. device for quickly disassembling according to claim 9, which is characterized in that the side wall of the concave part is formed with notch section, institute
When stating outer structural parts and removing from the device for quickly disassembling, the interconnecting piece is connected to the notch section;First stopper section and
Second stopper section is located at the two sides of the notch section.
11. device for quickly disassembling according to claim 1, which is characterized in that first limit assembly include: be set to it is described
The mandril of the side surface of first support and the stop block being connect with the mandril;
The mandril can be moved along the first direction, to drive the stop block to move along the first direction, so that described
Second support is abutted or is separated with the stop block.
12. device for quickly disassembling according to claim 11, which is characterized in that it is logical that the side surface of first support is equipped with second
Hole, the mandril and the stop block are respectively arranged at the two sides of first support;It is logical that the mandril is arranged in described second
Hole simultaneously partially protrudes from first support, and the stop block is connect with the part that the mandril protrudes from first support.
13. device for quickly disassembling according to claim 12, which is characterized in that second through-hole is stepped hole, the ladder
Pressure spring is equipped in hole in the biggish hole in aperture, the compression spring sleeve is set to the mandril.
14. device for quickly disassembling according to claim 11, which is characterized in that second support is close to the first limit group
The side of part is formed with limiting section;
It is located at described first when first limit assembly is in first state and second support along the first direction
When setting, the limiting section is abutted along the rotation direction of second support with the stop block;
When first limit assembly is in the second state along the first direction and second support is located at the second
When setting, the limiting section is abutted along the first direction with the stop block.
15. a kind of unmanned plane, which is characterized in that including fuselage, be installed in the fuselage mounting bracket and with the installation
The cradle head structure that bracket is detachably connected;Wherein, the mounting bracket includes fast as described in any one of claim 1~14
Dismantling device, the cradle head structure are equipped with the structural member being cooperatively connected with the interconnecting piece of the device for quickly disassembling.
16. unmanned plane according to claim 15, which is characterized in that the mounting bracket includes being installed in the fuselage
Annular frame and two device for quickly disassembling for being symmetrically disposed on the annular frame, the two sides of the cradle head structure are all provided with
State structural member.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201821151317.5U CN208593501U (en) | 2018-07-19 | 2018-07-19 | Device for quickly disassembling and unmanned plane |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201821151317.5U CN208593501U (en) | 2018-07-19 | 2018-07-19 | Device for quickly disassembling and unmanned plane |
Publications (1)
Publication Number | Publication Date |
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CN208593501U true CN208593501U (en) | 2019-03-12 |
Family
ID=65603455
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Application Number | Title | Priority Date | Filing Date |
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CN201821151317.5U Expired - Fee Related CN208593501U (en) | 2018-07-19 | 2018-07-19 | Device for quickly disassembling and unmanned plane |
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Country | Link |
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CN (1) | CN208593501U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112003081A (en) * | 2020-08-25 | 2020-11-27 | 北京安达维尔航空设备有限公司 | Novel equipment helps plug fixed establishment |
-
2018
- 2018-07-19 CN CN201821151317.5U patent/CN208593501U/en not_active Expired - Fee Related
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112003081A (en) * | 2020-08-25 | 2020-11-27 | 北京安达维尔航空设备有限公司 | Novel equipment helps plug fixed establishment |
CN112003081B (en) * | 2020-08-25 | 2021-08-24 | 北京安达维尔航空设备有限公司 | Equipment plug-in and plug-out assisting fixing mechanism |
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CF01 | Termination of patent right due to non-payment of annual fee | ||
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Granted publication date: 20190312 |