CN106672238A - Air throwing device with double bodies - Google Patents
Air throwing device with double bodies Download PDFInfo
- Publication number
- CN106672238A CN106672238A CN201610790275.9A CN201610790275A CN106672238A CN 106672238 A CN106672238 A CN 106672238A CN 201610790275 A CN201610790275 A CN 201610790275A CN 106672238 A CN106672238 A CN 106672238A
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- Prior art keywords
- housing
- terminal pad
- cover body
- fixed
- bodies
- Prior art date
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- 230000001360 synchronised effect Effects 0.000 claims description 30
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 9
- 238000010276 construction Methods 0.000 claims description 3
- 238000010030 laminating Methods 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 3
- 238000000034 method Methods 0.000 description 5
- 230000002411 adverse Effects 0.000 description 4
- 238000010009 beating Methods 0.000 description 2
- 230000006870 function Effects 0.000 description 2
- 238000001727 in vivo Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 230000003068 static effect Effects 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 241000521257 Hydrops Species 0.000 description 1
- 206010030113 Oedema Diseases 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000002955 isolation Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
- B64D1/10—Stowage arrangements for the devices in aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Actuator (AREA)
Abstract
The invention discloses an air throwing device with double bodies, which comprises the two bodies, two driving parts and a connecting seat, wherein each of the bodies comprises a storage area, a first shell and a second shell, the first shell is movably connected with the second shell, and the second shell rotates relative to the first shell, so that the second shell is opened or closed relative to the first shell so as to throw or store to-be-thrown objects stored in the storage area; each driving part is movably connected with the second shell in the corresponding body; and the two bodies are fixed on the connecting seat. The air throwing device achieves the effect that the to-be-thrown objects can be prevented from being damaged due to being influenced by severe environment or air obstructions, and has the advantages that the structure is simple, the safety performance is high and applicable performance is wide.
Description
Technical field
The invention belongs to technical field of aerospace, the aerial delivery device of more particularly to a kind of pair body.
Background technology
In prior art, generally needs are thrown in certain ad-hoc location (such as marine site, mountain area, forest) by unmanned plane
The goods and materials put are thrown in, and then play emergencing action.
However, being all often directly thing to be thrown to be fixed on into nothing loading when thing is thrown due to the characteristic of unmanned plane itself
Man-machine bottom, is directly thrown in thing to be thrown when running aerial.But this kind of mode causes thing to be thrown completely exposed
In the air, cause to damage so that easily treating throwing thing when running into barrier in the presence of a harsh environment or in the air.
The content of the invention
The technical problem to be solved be how to guarantee thing to be thrown during transport by adverse circumstances or
Aerial barrage thing affects and causes to damage.
To solve above-mentioned technical problem, the invention provides the aerial delivery device of a kind of pair of body, the described pair of body
Aerial delivery device includes：Two bodies, each described body includes：Memory area, for storing thing to be thrown；First shell
Body；Second housing, first housing and second housing are flexibly connected, and the two can be relatively rotated, first housing
And the clearance space between second housing constitutes the memory area；In two actuators, and each described actuator
Be accordingly flexibly connected with second housing in a body；Two actuators obtain independently control respectively
Signal processed, accordingly controls the second shell body phase in a body for accordingly first housing is carried out
Rotation；Connecting seat, two bodies are fixed on the connecting seat, and two bodies are parallel to each other.
Optionally, also include：Positioning element, the positioning element is fixed on the connecting seat, with to the thing to be thrown
Placement position positioned.
Optionally, also include：Camera head, the camera head is fixed on the connecting seat, with to the thing to be thrown
Placement position carry out real-time photography.
Optionally, the positioning element is laser designator；And/or, the camera head is video camera.
Optionally, second housing includes：Drive end and synchronous end, the drive end and the synchronous end are symmetrically divided
It is distributed in the two ends of second housing；The body also includes：Bearing assembly；First cover body, first cover body is fixed on institute
State on drive end, and the actuator is fixed in first cover body；Second cover body, second cover body is fixed on described same
On step end, and the bearing assembly is fixed in second cover body；Wherein, the actuator is in first cover body and institute
Drive end flexible connection is stated, the bearing assembly is flexibly connected in second cover body with the synchronous end, and the bearing
Component is in second cover body and the synchronous end synchronous axial system.
Optionally, first cover body is in hemispherical configuration, and first cover body includes one first circular open ends, and leads to
Cross first circular open ends to be fixed on the drive end；First circular open ends are straight in the hemispherical configuration
A maximum circular port of footpath；It is in hemispherical configuration with second cover body, second cover body is opened including one second circle
Mouth end, and be fixed on the synchronous end by second circular open ends；Second circular open ends are the hemisphere
A maximum circular port of diameter in shape structure.
Optionally, first housing is in semi-circular cylindrical, one end of first housing and first circular open ends
It is fixedly connected, the other end is fixedly connected with second circular open ends；Second housing is in semi-circular cylindrical, the first shell
The inside radius of body more than the inside radius of second housing, and fit the interior of first housing by the lateral surface of second housing
Side is rotated.
Optionally, the actuator includes：Steering wheel, the steering wheel is fixed in first cover body；Steering wheel disk, the rudder
Machine disk is fixed on the drive end, and is flexibly connected with the steering wheel, to be driven by steering wheel disk described in the servo driving
The drive end is rotated.
Optionally, the actuator also includes：First terminal pad, first terminal pad and first circular open ends
Phase clamping, and the drive end is fixed in first terminal pad, one end of first housing and first terminal pad
Phase clamping；Wherein, first terminal pad is located between the steering wheel disk and the drive end, the steering wheel disk and described first
Terminal pad is fixedly connected, to drive the steering wheel disk, first terminal pad to drive the drive end successively by the steering wheel
Rotated；Second terminal pad, second terminal pad is fixed with the second circular open ends phase clamping, and the synchronous end
In second terminal pad, the other end of second housing and the second terminal pad phase clamping；The bearing assembly exists
It is flexibly connected with the synchronous end by second terminal pad in second cover body.
Optionally, the connecting seat includes：Pedestal, the pedestal includes：First side, second side, the 3rd side and
4th side；And the first side, the second side, the 3rd side and the 4th side are surrounded to be formed inside one
The pedestal in hollow-core construction；The first side and the second side are two opposites, the 3rd side and institute
The 4th side is stated for two opposites；Two bodies are symmetrically fixed on the 3rd side and the 4th side；
First lid, first lid is covered in the first side, and the connecting seat by first lid with it is described
The bottom of unmanned plane is fixedly connected；Second lid, second lid is covered in the second side, and second lid
On offer the first projection window and second projection window, the positioning element be fixed on it is described first projection window at, it is described
Camera head is fixed at the second projection window.
Beneficial effect：
The invention provides a kind of Aerial Delivery Equipment of many bodies, by the way that 2 bodies are fixed on connecting seat, and
Each arranges in vivo the first housing and the second housing that can be rotated against, between the first housing and the second housing
A memory area is constituted every space, for storing thing to be thrown.Simultaneously by each in 2 actuator 2 bodies of corresponding driving
Individual intrinsic second shell body phase rotates for the first housing so that second shell body phase may be at beating for the first housing
On or off closes two states, i.e., when open, thing to be thrown is launched, and upon closing, then thing to be thrown is stored in the memory block
In domain.So allow for during thing to be thrown transported in the air by unmanned plane, because thing to be thrown is disposed between memory block
In domain, it is isolated with free surrounding space in the first housing and acting on for the second housing, ensure that thing to be thrown in transport process with this
In do not affected by extraneous adverse circumstances (such as thunderstorm weather) or aerial barrage thing and cause to damage, with simple structure, pacify
The characteristics of full performance is high.
Description of the drawings
In order to be illustrated more clearly that the embodiment of the present invention or technical scheme of the prior art, below will be to institute in embodiment
The accompanying drawing that needs are used is briefly described, it should be apparent that, drawings in the following description are only some enforcements of the present invention
Example, for those of ordinary skill in the art, on the premise of not paying creative work, can be being obtained according to these accompanying drawings
Obtain other accompanying drawings.
Fig. 1 is the overall structure diagram of the aerial delivery device of provided in an embodiment of the present invention pair of body；
Fig. 2 is the upward view of the aerial delivery device of provided in an embodiment of the present invention pair of body；
Fig. 3 is the top view of the aerial delivery device of provided in an embodiment of the present invention pair of body；
Fig. 4 is the side view of the aerial delivery device of provided in an embodiment of the present invention pair of body；
Fig. 5 is the overall structure exploded perspective view one of the aerial delivery device of provided in an embodiment of the present invention pair of body；
Fig. 6 is the overall structure exploded perspective view two of the aerial delivery device of provided in an embodiment of the present invention pair of body.
Specific embodiment
The invention provides a kind of Aerial Delivery Equipment of many bodies, by the way that 2 bodies are fixed on connecting seat, and
Each arranges in vivo the first housing and the second housing that can be rotated against, between the first housing and the second housing
A memory area is constituted every space, for storing thing to be thrown.Simultaneously by each in 2 actuator 2 bodies of corresponding driving
Individual intrinsic second shell body phase rotates for the first housing so that second shell body phase may be at beating for the first housing
On or off closes two states, i.e., when open, thing to be thrown is launched, and upon closing, then thing to be thrown is stored in the memory block
In domain.So allow for during thing to be thrown transported in the air by unmanned plane, because thing to be thrown is disposed between memory block
In domain, it is isolated with free surrounding space in the first housing and acting on for the second housing, ensure that thing to be thrown in transport process with this
In do not affected by extraneous adverse circumstances (such as thunderstorm weather) or aerial barrage thing and cause to damage, with simple structure, pacify
The characteristics of full performance is high.
Below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is carried out clear, complete
Site preparation is described, it is clear that described embodiment is only a part of embodiment of the invention, rather than the embodiment of whole.It is based on
Embodiment in the present invention, the every other embodiment that those of ordinary skill in the art are obtained belongs to present invention protection
Scope；Wherein involved in this enforcement "and/or" key word, represent and or two kinds of situations, in other words, the present invention implement
A and/or B mentioned by example, illustrates A and B, two kinds of situations of A or B, describes three kinds of states existing for A and B, such as A and/or
B, represents：Only including A does not include B；Only including B does not include A；Including A and B.
Meanwhile, in the embodiment of the present invention, when component is referred to as " being fixed on " another component, it can be directly at another
On component or can also there is component placed in the middle.When a component is considered as " connection " another component, it can be direct
It is connected to another component or may be simultaneously present component placed in the middle.When a component is considered as " being arranged at " another group
Part, it can be set directly on another component or may be simultaneously present component placed in the middle.Made in the embodiment of the present invention
Term " vertical ", " level ", "left", "right" and similar statement are merely for purposes of illustration, and are not intended to
Limit the present invention.
Fig. 1-4 are referred to, the aerial delivery device of a kind of pair of body provided in an embodiment of the present invention is applied to unmanned plane,
The aerial delivery device of described pair of body at least can include：Body 1, actuator 14, positioning element 3 and camera head 4.
Wherein, the body 1 includes：For storing memory area 13, the first housing 11, second housing 12 of thing to be thrown.
First housing 11 is fixed on the bottom of the unmanned plane, and first housing 11 and the activity of second housing 12 are even
Connect, and the two can be relatively rotated, the clearance space between first housing 11 and second housing 12 constitutes the storage
Region 13.The actuator 14 is flexibly connected with second housing 12, and to obtain control signal second housing 12 is driven
Rotated relative to first housing 11.
It will be understood by those skilled in the art that the body 1 is the loading body of thing to be thrown, the machine of unmanned plane is installed in
Body bottom.Certainly, for how body 1 is arranged on the fuselage of unmanned plane, the present invention does not limit to, and can be by a fixation
Device is fixed on the fuselage of unmanned plane, or by the detachable fuselage for being fixed on unmanned plane of a Quick-dismantle component
On, directly it can also be fixed on threadably on the fuselage of unmanned plane by screw or bolt, then fit
For the present invention.Likewise, the installation position for body 1 on the fuselage of unmanned plane, of the invention also not limit to, can be with root
According to the spatial distribution position of practical function demand unmanned aerial vehicle body bottom, the fuselage bottom pars intermedia of unmanned plane is fixed on
Position, the latter's sidepiece, or it is anterior, or rear portion etc., may also apply to the present invention.
Further, second housing 12 in the embodiment of the present invention relative to first housing 11 by being revolved
Turn, second housing 12 is opened or is closed relative to first housing 11, will be stored in the memory area 13
Thing described to be thrown throw in or storage.
Specifically, the first housing 12 in the body 1, can be a shell structure in semi-circular cylindrical, can be with
It is not understood as a hollow cylindrical tube Yan Qi centers vertical pivot being switched to two halves, wherein half is the first described housing 11, another
Half is second housing 12.Certainly, unlike the embodiment of the present invention, the inside radius of first housing 11 is more than described
The inside radius of the second housing 12, the lateral surface that can thus enable second housing 12 is closely fitted in described
The medial surface of one housing 11 is rotated.Realized with this second housing 12 open relative to first housing 11 or
Close.That is, when second housing 12 is opened relative to first housing 11, then the now outside of second housing 12
The medial surface of face and first housing 11 is (can be understood as what is overlapped) bonded to each other, and memory area 13 is beaten
Open, thing to be thrown is launched.When second housing 12 is closed relative to first housing 11, then now second housing
The medial surface of 12 lateral surface and first housing 11 is (can be understood as misaligned) being separated from each other, now by institute
The clearance space stated between the second housing 12 and first housing 11 constitutes the memory area 13, that is, thing to be thrown is stored
In the memory area 13.
Thus it is effectively guaranteed, when unmanned plane flight in the air, by second housing 12 and the first shell
Body 11 constitutes a protective cover, memory area 13 is stored in by thing to be thrown is temporary, so that the thing to be thrown and free surrounding space phase
Isolation, so prevent the external world adverse circumstances such as thunderstorm weather either aerial barrage thing treat throwing thing because contact or collision and
Cause to damage.
It should be noted that the first above-mentioned housing 11, the definition of the second housing 12, are not to the first housing 11, second
The essence restriction of the number order of housing 12, in embodiments of the present invention the first housing 11, the second housing 12 are only that housing is entered
Row is distinguished used.In other words, when the second housing 12 is fixed on unmanned plane, and the inside radius of the second housing 12 is more than first shell
The inside radius of body 11, causes the second housing 12 to be rotated relative to the first housing 11, to realize first housing 11 then
Open or close relative to second housing 12, be also applied for the present invention.
Below, continuation is by the embodiment of the present invention more than the inside radius of the second housing 12 with the inside radius of the first housing 11
Example, is expanded on further the present invention.
In embodiments of the present invention, in order in launch process, carrying out accurately in default position to missile
Throw in, the aerial delivery device of double bodies that the embodiment of the present invention is provided also includes a positioning element 2, the positioning element 2
Can be fixed on first housing 11, be positioned with the placement position to the thing to be thrown.And positioning element 2 has finger
Show the laser designator of positioning function.Certainly, in order to observe impression information to be put in real time, and ground is thrown in collection
Geographical location information, the embodiment of the present invention is additionally provided with camera head 3, and the camera head 3 is fixed on first housing
On 11, real-time photography is carried out with the placement position to the thing to be thrown.
It is noted that actuator 14 involved in the embodiment of the present invention, positioning element 2 and camera head 3, can be equal
Either earth station or remote terminal are connected and carry out information transmission with the flight control system inside unmanned plane, with by control of flying
Either earth station or remote terminal send driving instruction to system processed to the actuator 14, are driven by the actuator 14 then
Move second housing 12 to be rotated relative to first housing 11.
Further, Fig. 5-6 are referred to, for second housing 12, second housing 12 can include：
Drive end 121 and synchronous end 122.The drive end 121 and the synchronous end 122 are symmetrically distributed in second housing 12
Two ends.It is also understood that the drive end 121 and the synchronous end 122 are the two ends of second housing 12.While institute
Stating body 1 also includes：Bearing assembly 15, the first cover body 16 and the second cover body 17.Wherein, first cover body 16 is fixed on described
On drive end 121, and the actuator 14 is fixed in first cover body 16.Second cover body 17 is fixed on the synchronization
On end 122, and the bearing assembly 15 is fixed in second cover body 17.
Specifically, the actuator 14 is flexibly connected in first cover body 16 with the drive end 121, to receive
Drive signal drives the drive end 122 to be rotated, while drive end 121 causes second shell as one end of the second housing 12
Body 12 is overall to synchronize therewith rotation.The bearing assembly 15 is movable with the synchronous end 122 in second cover body 17
Connection, and the bearing assembly 15 is in second cover body 17 and the synchronous axial system of synchronous end 122.
Further, first cover body 16 is in hemispherical configuration so that the circular open and first of the first cover body 16
The semicircle opening of the housing 12 of housing 11 and second matches.First cover body 16 includes one first circular open ends 161, and
It is fixed on the drive end 121 by first circular open ends 161.Here, the first cover body 16 is in hemispherical configuration, can
To be interpreted as the first cover body 16 by, to its tail end, internal diameter is gradually reduced with the connecting portion of drive end 121, i.e., described first is circular
Opening 161 is a maximum circular port of diameter in the hemispherical configuration.Likewise, second cover body 17 is in hemisphere
Shape structure so that the circular open of the second cover body 17 also matches with the semicircle opening of the first housing 11 and the second housing 12.
Second cover body 17 includes one second circular open ends 171, and is fixed on by second circular open ends 171 described same
On step end 122.Here, the second cover body 17 is in hemispherical configuration, it can be understood as the second cover body 17 by with the connecting portion of synchronous end 122
It is gradually reduced to its tail end, internal diameter at position, i.e., described second circular open ends 171 are that diameter is maximum in the hemispherical configuration
One circular port.
Need exist for especially, it is emphasized that why first cover body 16 and second cover body 17 are designed to into hemisphere
Shape structure, so that the lateral surface of first cover body 16 and second cover body 17 (can be understood as unmanned plane during flying process
In double bodies aerial delivery device windward side) as windward side when, the resistance of wind is along first cover body 16 and/or institute
The spherical surface for stating the second cover body 17 is slowed down, and then maximized reduces the aerial of the provided in an embodiment of the present invention pair of body
The resistance that delivery device is received in running in the air.It is also possible to run into bad weather circumstances such as thunderstorm so that working as
During weather, the rainwater landed on first cover body 16 and/or second cover body 17 can be along first cover body 16
And/or the spherical surface of second cover body 17 is dirty, it is to avoid hydrops.
For actuator 15, in embodiments of the present invention the actuator 15 can include：Steering wheel 141 and steering wheel disk
142.Wherein, the steering wheel 141 is fixed in first cover body 16.The steering wheel disk 142 is fixed on the drive end 121
On, and be flexibly connected with the steering wheel 141, to obtain control instruction by the steering wheel 141, drive the band of steering wheel disk 142
The dynamic drive end 121 is rotated.The entirety of the second housing 12 that rotarily drives that drive end 121 is realized with this is revolved therewith
Turn, realize that second housing 12 is opened or closed relative to first housing 11.That is, refer to when steering wheel 141 obtains control
Order, when driving the steering wheel disk 142 to drive the drive end 121 (the second housing 12) to open relative to first housing 11,
Then now the medial surface of the lateral surface of second housing 12 and first housing 11 is bonded to each other (can be understood as
Overlap), memory area 13 is opened, and thing to be thrown is launched.When steering wheel 141 obtains control instruction, the steering wheel is driven
When disk 142 drives the drive end 121 (the second housing 12) to close relative to first housing 11, then the now second shell
The medial surface of the lateral surface of body 12 and first housing 11 is (can be understood as misaligned) being separated from each other, now by
Clearance space between second housing 12 and first housing 11 constitutes the memory area 13, that is, thing to be thrown is deposited
Storage is in the memory area 13.
In addition, in embodiments of the present invention, further referring to Fig. 5-6, the actuator 14 can also include：First connects
The terminal pad 18 of flange 143 and second.Wherein, first terminal pad 143 and the phase clamping of first circular open ends 161, and
The drive end 121 is fixed in first terminal pad 143, one end of first housing 11 and first terminal pad
143 phase clampings.
Specifically, by first terminal pad 143 and the phase clamping of first circular open ends 161, and the drive
Moved end 121 is fixed in first terminal pad 143, and this is allowed for when steering wheel 141 drives steering wheel disk 142 to be rotated, rotation
Steering wheel disk 142 in turning drives the drive end 121 to synchronize rotation, and due to drive end 121 and first terminal pad
It is fixedly connected between 143, and then causes first terminal pad 143 also synchronous axial system.Due to first terminal pad 143 and institute
One end phase clamping of the first circular open ends 161, first housing 11 is stated, therefore first terminal pad 143 was being rotated
Cheng Zhong, you can realize first circular open ends 161 (the first cover body 16) and first housing 11 relative in rotation
First terminal pad remains static.
For the snap fit between first terminal pad 143 and first circular open ends 161, described first connect
Snap fit between one end of flange 143 and first housing 11, can be in first circular open ends 161
Side opens up the annulus chute of a depression, and in the edge of first terminal pad 143 boss of a projection is opened up, and by this
Boss is connected in the annulus chute of the inner side of the first circular open ends 161, with this be implemented in first terminal pad 143 with it is described
Clamping between first circular open ends 161, and so that first terminal pad 143 can be relative to first circular open ends
161 are rotated.Likewise, for the snap fit between one end of first terminal pad 143 and first housing 11,
Can also be that an annulus chute is opened up at the edge side surface of the first terminal pad 143, now can be by first terminal pad 143
On the boss that opens up be interpreted as in the diametric(al) of the first terminal pad 143, the annulus opened up in first terminal pad 143
In the card of first terminal pad 143, the two plane being located is mutually perpendicular to chute.While the one of first housing 11
End offers the boss of a projection, and is connected at the edge side surface of first terminal pad 143 by the boss and is opened up
In annulus chute, the clamping between first terminal pad 143 and first housing 11, and so that described first are realized with this
Terminal pad 143 can be rotated relative to first housing.
Certainly, for first terminal pad 143 can relative to first housing 11, first cover body 16 can be relative
Rotate, i.e., during the rotation of the first terminal pad 143, first housing 11, the transfixion of the first cover body 16.Also deposit
In other designs, above-mentioned first terminal pad 143 of the embodiment of the present invention and first circular open ends 161 it
Between phase clamping, first terminal pad 143 and one end phase clamping of first housing 11 be only a kind of mode wherein realized,
Not limit to.
For example, it is also possible to be respectively with described first by one end of first terminal pad 143 and first housing 11
The phase clamping of first circular open ends 161 of cover body 16, i.e., in the edge of first circular open ends 161, and near side
The medial surface of edge position, opens up respectively the annulus chute of depression, while starting a matching in the edge of the first terminal pad 143
Boss, also open up the boss of a matching in the edge of one end of the first housing 11, and then respectively by the first terminal pad 143
Edge boss be connected to the first circular open ends 161 in the annulus chute of edge medial surface, and by
The boss of one end of one housing 11 is connected in the annulus chute of the edge of the first circular open ends 161, is also capable of achieving with this
First terminal pad 143 be able to can be relatively rotated relative to first housing 11, first cover body 16, i.e., in the first connection
During disk 143 rotates, first housing 11, the transfixion of the first cover body 16 may also apply to the present invention.
You need to add is that, first terminal pad 143 is located between the steering wheel disk 142 and the drive end 121, institute
State steering wheel disk 142 to be fixedly connected with first terminal pad 143, to drive the steering wheel disk successively by the steering wheel 141
142nd, first terminal pad 143 drives the drive end 121 to be rotated.The steering wheel disk 142 and first terminal pad
Being fixedly connected between 143 can be mode connects for screw, or bolt connection, and the present invention is not limited, as long as enabling to
Being fixedly connected for synchronous axial system can occur therebetween, then within protection scope of the present invention.
Corresponding with the first terminal pad 143, the aerial delivery device of provided in an embodiment of the present invention pair of body also includes：The
Two terminal pads 18, second terminal pad 18 is fixed with the phase clamping of second circular open ends 171, and the synchronous end 122
In second terminal pad 18, the other end of second housing 12 and the phase clamping of second terminal pad 18；The bearing
Component 15 is flexibly connected by second terminal pad 18 in second cover body 17 with the synchronous end 122.
Identical, second terminal pad 18 and the phase clamping of second circular open ends 171, and the synchronous end 121
It is fixed in second terminal pad 18, this is allowed for when steering wheel 141 drives steering wheel disk 142 to be rotated, the rudder in rotation
Machine disk 142 drives the drive end 121 (the second housing 12) to synchronize rotation, and because synchronous end 122 connects with described second
It is fixedly connected between flange 18, and then causes second terminal pad 18 also synchronous axial system.Due to second terminal pad 18 with
The other end phase clamping of second circular open ends 171, first housing 11, therefore second terminal pad 18 is in rotation
During, you can realize second circular open ends 171 (the second cover body 17) and first housing 11 relative in rotation
The second terminal pad 18 remain static.
For the snap fit between second terminal pad 18 and second circular open ends 171, described second connect
Snap fit between the other end of flange 18 and first housing 11, can be in second circular open ends 171
Inner side opens up the annulus chute of a depression, and in the edge of second terminal pad 18 boss of a projection is opened up, and passes through
The boss is connected in the annulus chute of the inner side of the second circular open ends 171, and with this second terminal pad 18 and institute are implemented in
The clamping between the second circular open ends 171 is stated, and so that second terminal pad 18 can be relative to second circular open
End 171 is rotated.Likewise, for the clamping side between the other end of second terminal pad 18 and first housing 11
Formula, or an annulus chute is opened up at the edge side surface of the second terminal pad 18, now can be by second terminal pad
The boss opened up on 18 is interpreted as in the diametric(al) of the second terminal pad 18, the annulus opened up in second terminal pad 18
In the card of second terminal pad 18, the two plane being located is mutually perpendicular to chute.Simultaneously first housing 11 is another
One end also offers the boss of a projection, and is connected at the edge side surface of second terminal pad 18 by the boss and is opened
If in annulus chute, with this clamping between second terminal pad 18 and first housing 11 is realized, and cause described the
Two terminal pads 18 can be rotated relative to first housing 11.
Certainly, for second terminal pad 18 can relative to first housing 11, second cover body 17 can be relative
Rotate, i.e., during the rotation of the second terminal pad 18, first housing 11, the transfixion of the first cover body 17.Also deposit
In other designs, above-mentioned second terminal pad 18 of the embodiment of the present invention and second circular open ends 171 it
Between phase clamping, second terminal pad 18 and the other end phase clamping of first housing 11 be only one kind side for wherein realizing
Formula, not limits to.
For example, it is also possible to be respectively with described second by the other end of second terminal pad 18 and first housing 11
The phase clamping of second circular open ends 171 of cover body 17, i.e., in the edge of second circular open ends 171, and near side
The medial surface of edge position, opens up respectively the annulus chute of depression, while starting a matching in the edge of the second terminal pad 18
Boss, also open up the boss of a matching in the edge of the other end of the first housing 11, and then respectively by the second terminal pad
18 edge boss is connected to the second circular open ends 171 in the annulus chute of edge medial surface, and will
The boss of the other end of the first housing 11 is connected in the annulus chute of the edge of the second circular open ends 171, also may be used with this
Realize that second terminal pad 18 be able to can be relatively rotated relative to first housing 11, second cover body 17, i.e., second
During terminal pad 18 rotates, first housing 11, the transfixion of the second cover body 17 may also apply to the present invention.
By the terminal pad 18 of above-mentioned first terminal pad 143 and second, second housing 12 and the first shell are realized
The connected mode for rotating against between body 11, that is, realize second housing 12 and can be at relative to first housing 11
The state opened or close.Certainly, in order to mitigate main screw lift, because the first terminal pad 143 will be with the card of steering wheel disk 142
It is flexibly connected, therefore for the first terminal pad 143 uses solid structure, and for the second terminal pad 18, due to
It need not be connected with the card of steering wheel disk 142, therefore for the second terminal pad 18 can be set using the structure of " hollow body " as far as possible
Meter, to mitigate automatically, for example：Second terminal pad includes：Cross type frame 181, support disk 182 are framework 183.Cross type frame
181 are used to connect the support disk 182 and the framework 183 as support frame so that the support disk 182 is fixed
In the framework 183, with the solid structure that this replaces the first terminal pad 143 by the structure of cross type frame 181, reach
Mitigate the technique effect of deadweight.Bearing assembly 15 is fixed on the support disk 182, and as one kind of the embodiment of the present invention
Embodiment, the bearing assembly 15 can include a bearing 151 and a ring flange 152.Wherein, the bearing 151 and described
The bearing connection at the support disk 182 of ring flange 152.For the bearing 151, the ring flange 152 and the support
The bearing connection of disk 182, to realize the relative rotation of the second terminal pad 18 to be prior art, here is omitted.It is worth
One is mentioned that, the bearing assembly 15 is arranged in the embodiment of the present invention, is in order that the bearing assembly 15 and the driving
Part 14 second housing 12 two ends constitute a pair of rotation balance fulcrum, with avoid when only exist actuator 14 this
During pivot point, the second housing 12 is caused to rotate jiggly technological deficiency.
Finally it is emphasized that a kind of embodiment of the embodiment of the present invention described above, the unmanned plane for each meaning
Fuselage bottom secure a body 1, but for the quantity present invention of body 1 is not limited.Namely in the present invention, institute
The quantity for stating body 1 can be n, and the bottom for being fixed on the unmanned plane that the individual bodies 1 of n can be parallel.Meanwhile, institute
The quantity for stating actuator 14 is corresponding with the quantity of the body 1, and each described actuator 14 accordingly with described in one
Second housing 12 in body 1 is flexibly connected；Wherein, the n is more than or equal to 2, and each described actuator 14 is distinguished
Independently controlled signal is obtained, second housing 12 in a body 1 is accordingly controlled relative to accordingly one
First housing 11 is rotated.
For example, with continued reference to one embodiment of the present invention during Fig. 1-4, as n=2, now for the ease of connection 2
Individual or multiple bodies 1 (being illustrated by taking n=2 as an example below), the present invention can also include a connecting seat 4.And described in 2
Body 1 is parallel to be fixed on the connecting seat 4.
Specifically, the connecting seat can include：Pedestal 41, the first lid 42 and the second lid 43.
Wherein, the pedestal 41 includes：First side, second side, the 3rd side and the 4th side；And first side
Face, the second side, the 3rd side and the 4th side are surrounded to form the pedestal of the inside in hollow-core construction
41；The first side and the second side are two opposites, and the 3rd side and the 4th side are two right
Facade；2 bodies 1 are symmetrically fixed on the 3rd side and the 4th side.First lid 42 is covered
In the first side, and the connecting seat 4 is fixedly connected by first lid 42 with the bottom of the unmanned plane；Institute
State the second lid 43 to cover in the second side, and the first projection window 431 and are offered on second lid 43
Two projection windows 432.The positioning element 2 is fixed at the first projection window 431, and the camera head 3 is fixed on institute
State at the second projection window 432.Identical, the positioning element 2 can be laser designator；The camera head 3 can be
Video camera.
It should be noted last that, above specific embodiment only to illustrate technical scheme and unrestricted,
Although being described in detail to the present invention with reference to example, it will be understood by those within the art that, can be to the present invention
Technical scheme modify or equivalent, without deviating from the spirit and scope of technical solution of the present invention, it all should cover
In the middle of scope of the presently claimed invention.
Claims (10)
1. the aerial delivery device of a kind of pair of body, it is characterised in that the aerial delivery device of described pair of body includes：
Two bodies, each described body includes：
Memory area, for storing thing to be thrown；
First housing；
Second housing, first housing and second housing are flexibly connected, and the two can be relatively rotated, first housing
And the clearance space between second housing constitutes the memory area；
It is accordingly movable with second housing in a body in two actuators, and each described actuator
Connection；Two actuators obtain respectively independently controlled signal, accordingly control described second in a body
Housing is rotated relative to accordingly one first housing；
Connecting seat, two bodies are fixed on the connecting seat, and two bodies are parallel to each other.
2. the aerial delivery device of bodies as claimed in claim 1 double, it is characterised in that also include：
Positioning element, the positioning element is fixed on the connecting seat, is positioned with the placement position to the thing to be thrown.
3. the aerial delivery device of bodies as claimed in claim 2 double, it is characterised in that also include：
Camera head, the camera head is fixed on the connecting seat, is carried out in real time with the placement position to the thing to be thrown
Shooting.
4. the aerial delivery device of bodies as claimed in claim 3 double, it is characterised in that：
The positioning element is laser designator；
And/or,
The camera head is video camera.
5. the aerial delivery device of the double bodies as described in any one of claim 2-4, it is characterised in that：
Second housing includes：Drive end and synchronous end, the drive end and the synchronous end are symmetrically distributed in described the
The two ends of two housings；
The body also includes：
Bearing assembly；
First cover body, first cover body is fixed on the drive end, and the actuator is fixed in first cover body；
Second cover body, second cover body is fixed on the synchronous end, and the bearing assembly is fixed on second cover body
It is interior；
Wherein, the actuator is flexibly connected in first cover body with the drive end, and the bearing assembly is described
It is flexibly connected with the synchronous end in two cover bodies, and the bearing assembly synchronously turns in second cover body with the synchronous end
It is dynamic.
6. the aerial delivery device of bodies as claimed in claim 5 double, it is characterised in that：
First cover body is in hemispherical configuration, and first cover body includes one first circular open ends, and by described first
Circular open ends are fixed on the drive end；First circular open ends are diameter is maximum in the hemispherical configuration one
Individual circular port；
With,
Second cover body is in hemispherical configuration, and second cover body includes one second circular open ends, and by described second
Circular open ends are fixed on the synchronous end；Second circular open ends are diameter is maximum in the hemispherical configuration one
Individual circular port.
7. the aerial delivery device of bodies as claimed in claim 6 double, it is characterised in that：
First housing is in semi-circular cylindrical, and one end of first housing is fixedly connected with first circular open ends, separately
One end is fixedly connected with second circular open ends；
Second housing is in semi-circular cylindrical, and the inside radius of first housing is more than the inside radius of second housing, and institute
The medial surface for stating lateral surface laminating first housing of the second housing is rotated.
8. the aerial delivery device of bodies as claimed in claim 7 double, it is characterised in that the actuator includes：
Steering wheel, the steering wheel is fixed in first cover body；
Steering wheel disk, the steering wheel disk is fixed on the drive end, and is flexibly connected with the steering wheel, to be driven by the steering wheel
The dynamic steering wheel disk drives the drive end to be rotated.
9. the aerial delivery device of bodies as claimed in claim 8 double, it is characterised in that the actuator also includes：
First terminal pad, first terminal pad and the first circular open ends phase clamping, and the drive end is fixed on institute
State in the first terminal pad, one end of first housing and the first terminal pad phase clamping；Wherein, the first terminal pad position
Between the steering wheel disk and the drive end, the steering wheel disk is fixedly connected with first terminal pad, with by the rudder
Machine drives successively the steering wheel disk, first terminal pad to drive the drive end to be rotated；
Second terminal pad, second terminal pad and the second circular open ends phase clamping, and institute is fixed at the synchronous end
State in the second terminal pad, the other end of second housing and the second terminal pad phase clamping；The bearing assembly is described
It is flexibly connected with the synchronous end by second terminal pad in second cover body.
10. the aerial delivery device of bodies as claimed in claim 9 double, it is characterised in that the connecting seat includes：
Pedestal, the pedestal includes：First side, second side, the 3rd side and the 4th side；And the first side, institute
State second side, the 3rd side and the 4th side to surround to form the pedestal of the inside in hollow-core construction；It is described
First side and the second side are two opposites, and the 3rd side and the 4th side are two opposites；Two
The individual body is symmetrically fixed on the 3rd side and the 4th side；
First lid, first lid is covered in the first side, and the connecting seat by first lid with
The bottom of unmanned plane is fixedly connected；
Second lid, second lid is covered in the second side, and offers the first projection on second lid
Window and the second projection window.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610790275.9A CN106672238B (en) | 2016-08-31 | 2016-08-31 | The aerial delivery device of double ontologies |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610790275.9A CN106672238B (en) | 2016-08-31 | 2016-08-31 | The aerial delivery device of double ontologies |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106672238A true CN106672238A (en) | 2017-05-17 |
| CN106672238B CN106672238B (en) | 2019-11-19 |
Family
ID=58840274
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610790275.9A Expired - Fee Related CN106672238B (en) | 2016-08-31 | 2016-08-31 | The aerial delivery device of double ontologies |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106672238B (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2072255A (en) * | 1980-03-19 | 1981-09-30 | Rolls Royce | Door operating mechanisms |
| JPS60193899U (en) * | 1984-06-05 | 1985-12-24 | 日本飛行機株式会社 | Aircraft payload launcher |
| GB2169067A (en) * | 1982-06-16 | 1986-07-02 | Hunting Eng Ltd | Ejection equipment |
| US6679454B2 (en) * | 2002-04-15 | 2004-01-20 | The Boeing Company | Radial sonobuoy launcher |
| CN104590562A (en) * | 2015-02-12 | 2015-05-06 | 马鞍山市赛迪智能科技有限公司 | Anti-collision fixed-point unmanned aerial vehicle for fire control |
| CN205998130U (en) * | 2016-08-31 | 2017-03-08 | 易瓦特科技股份公司 | The aerial delivery device of double bodies |
-
2016
- 2016-08-31 CN CN201610790275.9A patent/CN106672238B/en not_active Expired - Fee Related
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2072255A (en) * | 1980-03-19 | 1981-09-30 | Rolls Royce | Door operating mechanisms |
| GB2169067A (en) * | 1982-06-16 | 1986-07-02 | Hunting Eng Ltd | Ejection equipment |
| JPS60193899U (en) * | 1984-06-05 | 1985-12-24 | 日本飛行機株式会社 | Aircraft payload launcher |
| US6679454B2 (en) * | 2002-04-15 | 2004-01-20 | The Boeing Company | Radial sonobuoy launcher |
| CN104590562A (en) * | 2015-02-12 | 2015-05-06 | 马鞍山市赛迪智能科技有限公司 | Anti-collision fixed-point unmanned aerial vehicle for fire control |
| CN205998130U (en) * | 2016-08-31 | 2017-03-08 | 易瓦特科技股份公司 | The aerial delivery device of double bodies |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106672238B (en) | 2019-11-19 |
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Granted publication date: 20191119 Termination date: 20210831 |