CN106275437B - More ontology delivery devices applied to unmanned plane - Google Patents
More ontology delivery devices applied to unmanned plane Download PDFInfo
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- CN106275437B CN106275437B CN201610789848.6A CN201610789848A CN106275437B CN 106275437 B CN106275437 B CN 106275437B CN 201610789848 A CN201610789848 A CN 201610789848A CN 106275437 B CN106275437 B CN 106275437B
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
Abstract
The invention discloses a kind of more ontology delivery devices applied to unmanned plane, including：N ontology, each ontology include：Storage region；First shell；Second shell, the first shell and second shell flexible connection；N actuator, and being accordingly flexibly connected with the second shell in an ontology in each described actuator；Connecting seat, the n ontologies are fixed on the connecting seat.Wherein, the second shell makes the second shell be opened relative to the first shell and either closes will be stored in object dispensing or storage to be thrown described in the storage region by being rotated relative to the first shell.The present invention, which realizes, can not be influenced by adverse circumstances or aerial barrage object and be damaged, and have the characteristics that simple in structure, security performance is high and applicable performance is wide.
Description
Technical field
The invention belongs to technical field of aerospace, more particularly to a kind of more ontology delivery devices applied to unmanned plane.
Background technology
In the prior art, usually by unmanned plane to needing to throw in certain specific position (such as marine site, mountain area, forest)
The goods and materials put are launched, and then play emergencing action.
All it is often that object to be thrown directly is fixed on nothing loading when throwing object however, due to the characteristic of unmanned plane itself
Object to be thrown directly is launched when running aerial in man-machine bottom.However such mode makes object to be thrown completely exposed
In the air, it is damaged so that easily being treated when encountering barrier in the presence of a harsh environment or in the air and throwing object.
Invention content
The technical problem to be solved by the present invention is to, how to ensure object to be thrown during transport not by adverse circumstances or
Aerial barrage object is influenced and is damaged.
In order to solve the above technical problems, the present invention provides a kind of more ontology delivery devices applied to unmanned plane, it is described
More ontology delivery devices applied to unmanned plane include：N ontology, each described ontology include：Storage region, for storing
Object to be thrown；First shell；Second shell, the first shell and second shell flexible connection, and the two can relatively rotate,
Clearance space between the first shell and the second shell constitutes the storage region, and the storage region is in cylinder
Shape；N actuator, and accordingly connecting with the second shell activity in an ontology in each described actuator
It connects；The n actuators obtain independently control signal respectively, accordingly control the second shell in an ontology
It is rotated relative to an accordingly first shell；Connecting seat, the n ontologies are fixed on the connecting seat, and n
A ontology is mutually parallel two-by-two；And the connecting seat is fixed on the unmanned plane wherein, n is 2 or 3 or 4.
Optionally, further include：Positioning element, the positioning element are fixed on the connecting seat, with to the object to be thrown
Placement position positioned.
Optionally, further include：Photographic device, the photographic device are fixed on the connecting seat, with to the object to be thrown
Placement position carry out real-time photography.
Optionally, the positioning element is laser designator；And/or the photographic device is video camera.
Optionally, the second shell includes：Driving end and synchronous end, the driving end are symmetrically divided with the synchronous end
It is distributed in the both ends of the second shell；The ontology further includes：Bearing assembly；First cover body, first cover body are fixed on institute
It states on driving end, and the actuator is fixed in first cover body；Second cover body, second cover body are fixed on described same
It walks on end, and the bearing assembly is fixed in second cover body；Wherein, the actuator is in first cover body and institute
The flexible connection of driving end is stated, the bearing assembly is flexibly connected in second cover body with the synchronous end, and the bearing
Component rotates synchronously in second cover body with the synchronous end.
Optionally, first cover body is in hemispherical configuration, and first cover body includes one first circular open ends, and is led to
First circular open ends are crossed to be fixed on the driving end；First circular open ends are straight in the hemispherical configuration
The maximum circular port of diameter；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
The maximum circular port of diameter in shape structure.
Optionally, the first shell is in semi-circular cylindrical, one end of the first shell and first circular open ends
It is fixedly connected, the other end is fixedly connected with second circular open ends；The second shell is in semi-circular cylindrical, the first shell
The inside radius of body is more than the inside radius of the second shell, and the lateral surface of the second shell is bonded the interior of the first shell
Side is rotated.
Optionally, the actuator includes：Steering engine, the steering engine are fixed in first cover body；Steering engine disk, the rudder
Machine disk is fixed on the driving end, and is flexibly connected with the steering engine, to be driven by steering engine disk described in the servo driving
The driving end is rotated.
Optionally, the actuator further includes：First terminal pad, first terminal pad and first circular open ends
It is mutually clamped, and the driving end is fixed in first terminal pad, one end of the first shell and first terminal pad
Mutually it is clamped；Wherein, first terminal pad is between the steering engine disk and the driving end, the steering engine disk and described first
Terminal pad is fixedly connected, to drive the steering engine disk, first terminal pad to drive the driving end successively by the steering engine
It is rotated；Second terminal pad, second terminal pad are mutually clamped with second circular open ends, and the synchronous end is fixed
In in second terminal pad, the other end of the second shell is mutually clamped with second terminal pad；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 include：First side, second side, third side and
4th side；And the first side, the second side, the third side and the 4th side are surrounded to be formed inside one
In the pedestal of hollow-core construction；The first side and the second side are two opposites, the third side and institute
It is two opposites to state the 4th side；Two ontologies are symmetrically fixed on the third side and the 4th side；
First lid, first cover cap closes in the first side, and the connecting seat passes through first lid and nobody
The bottom of machine is fixedly connected；Second lid, second cover cap closes in the second side, and is opened on second lid
Equipped with the first projection window and the second projection window.
Advantageous effect：
The present invention provides a kind of Aerial Delivery Equipments of more ontologies, by the way that n ontology is fixed on connecting seat, and
In each ontology setting can relative rotation first shell and second shell, between first shell and second shell
A storage region is constituted every space, for storing object to be thrown.Simultaneously by each in the corresponding n ontology of driving of n actuator
A intrinsic second shell is rotated relative to first shell so that second shell may be at beating relative to first shell
On or off closes two states, i.e., when open, object to be thrown is launched, and upon closing, then object to be thrown is stored in the memory block
In domain.It allows in this way during object to be thrown transported in the air by unmanned plane, since object to be thrown is disposed between memory block
It in domain, is isolated with free surrounding space in first shell and acting on for second shell, ensures object to be thrown in transport process with this
In do not influenced and damaged by extraneous adverse circumstances (such as thunderstorm weather) or aerial barrage object, there is simple in structure, peace
The high feature of full performance.
Description of the drawings
It in order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, below will be to institute in embodiment
Attached drawing to be used is needed to be briefly described, it should be apparent that, the accompanying drawings in the following description is only some implementations of the present invention
Example, for those of ordinary skill in the art, without creative efforts, can also obtain according to these attached drawings
Obtain other attached drawings.
Fig. 1 is the overall structure diagram of more ontology delivery devices provided in an embodiment of the present invention applied to unmanned plane；
Fig. 2 is the upward view of more ontology delivery devices provided in an embodiment of the present invention applied to unmanned plane；
Fig. 3 is the vertical view of more ontology delivery devices provided in an embodiment of the present invention applied to unmanned plane；
Fig. 4 is the side view of more ontology delivery devices provided in an embodiment of the present invention applied to unmanned plane；
Fig. 5 is the overall structure explosion signal of more ontology delivery devices provided in an embodiment of the present invention applied to unmanned plane
Figure one；
Fig. 6 is the overall structure explosion signal of more ontology delivery devices provided in an embodiment of the present invention applied to unmanned plane
Figure two.
Specific implementation mode
The present invention provides a kind of Aerial Delivery Equipments of more ontologies, by the way that n ontology is fixed on connecting seat, and
In each ontology setting can relative rotation first shell and second shell, between first shell and second shell
A storage region is constituted every space, for storing object to be thrown.Simultaneously by each in the corresponding n ontology of driving of n actuator
A intrinsic second shell is rotated relative to first shell so that second shell may be at beating relative to first shell
On or off closes two states, i.e., when open, object to be thrown is launched, and upon closing, then object to be thrown is stored in the memory block
In domain.It allows in this way during object to be thrown transported in the air by unmanned plane, since object to be thrown is disposed between memory block
It in domain, is isolated with free surrounding space in first shell and acting on for second shell, ensures object to be thrown in transport process with this
In do not influenced and damaged by extraneous adverse circumstances (such as thunderstorm weather) or aerial barrage object, there is simple in structure, peace
The high feature of full performance.
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation describes, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, the every other embodiment that those of ordinary skill in the art are obtained belong to what the present invention protected
Range；Involved "and/or" keyword wherein in this implementation, indicate and or two kinds of situations, in other words, the present invention is implemented
A and/or B mentioned by example, illustrate two kinds of A and B, A or B situations, describe three kinds of states present in A and B, such as A and/or
B is indicated：It includes B to only include A not；It includes A to only include B not；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 there may also be components 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 set to " another group
Part, it can be set up directly on another component or may be simultaneously present component placed in the middle.Made in the embodiment of the present invention
Term " vertically ", " horizontal ", "left", "right" and similar statement are merely for purposes of illustration, and are not intended to
The limitation present invention.
- 4 are please referred to Fig.1, a kind of more ontology delivery devices applied to unmanned plane provided in an embodiment of the present invention are applied to
Unmanned plane, more ontology delivery devices applied to unmanned plane at least may include：Ontology 1, actuator 14, positioning element 3
With photographic device 4.
Wherein, the ontology 1 includes：Storage region 13, first shell 11, second shell 12 for storing object to be thrown.
The first shell 11 is fixed on the bottom of the unmanned plane, and the first shell 11 and 12 activity of the second shell are even
It connects, and the two can relatively rotate, the clearance space between the first shell 11 and the second shell 12 constitutes the storage
Region 13.The actuator 14 is flexibly connected with the second shell 12, and the second shell 12 is driven to obtain control signal
It is rotated relative to the first shell 11.
It will be understood by those skilled in the art that the ontology 1 is the loading body of object to be thrown, it is installed in the machine of unmanned plane
Body bottom.Certainly, how ontology 1 is mounted on the fuselage of unmanned plane, the present invention does not limit to, and can be fixed by one
Device is fixed on the fuselage of unmanned plane, can also be by the detachable fuselage for being fixed on unmanned plane of a Quick-dismantle component
On, directly it can also be fixed on the fuselage of unmanned plane threadably by screw or bolt, then it is suitable
For the present invention.Likewise, the installation position for ontology 1 on the fuselage of unmanned plane, the present invention does not also limit to, Ke Yigen
According to the spatial distribution position of practical function demand unmanned aerial vehicle body bottom, it is fixed on the fuselage bottom middle part of unmanned plane
Position, the latter side either front or rear portion etc., may also apply to the present invention.
Further, the second shell 12 in the embodiment of the present invention relative to the first shell 11 by being revolved
Turn, so that the second shell 12 is opened or is closed relative to the first shell 11, the storage region 13 will be stored in
The object to be thrown launch or store.
Specifically, the first shell 12 in the ontology 1, can be one be in semi-circular cylindrical shell structure, can be with
It is not understood as a hollow cylindrical tube prolonging its center vertical pivot and is switched to two halves, wherein half is the first shell 11, another
Half is the second shell 12.Certainly, unlike the embodiment of the present invention, the inside radius of the first shell 11 is more than described
The inside radius of second shell 12 can thus enable the lateral surface of the second shell 12 to be closely fitted in described
The medial surface of one shell 11 is rotated.With this come realize the second shell 12 relative to the first shell 11 open or
It closes.That is, when the second shell 12 is opened relative to the first shell 11, then the outside of the second shell 12 at this time
The medial surface of face and the first shell 11 is (can be understood as overlapping) being bonded to each other, and storage region 13 is beaten
It opens, object to be thrown is launched.When the second shell 12 is closed relative to the first shell 11, then the second shell at this time
12 lateral surface and the medial surface of the first shell 11 are (can be understood as misaligned) being separated from each other, at this time by institute
It states the clearance space between second shell 12 and the first shell 11 and constitutes the storage region 13, that is, object to be thrown is stored
In the storage region 13.
It is thus effectively guaranteed, when unmanned plane flight in the air, by the second shell 12 and the first shell
Body 11 constitutes a protective cover, storage region 13 is stored in by object to be thrown is temporary, so that the object to be thrown and free surrounding space phase
Isolation, and then prevent extraneous adverse circumstances such as thunderstorm weather either aerial barrage object is treated and throws object due to contacting or collide
It damages.
It should be noted that the definition of above-mentioned first shell 11, second shell 12, is not to first shell 11, second
The number order of shell 12 essence limit, in embodiments of the present invention first shell 11, second shell 12 be only to shell into
Used in row is distinguished.In other words, when second shell 12 is fixed on unmanned plane, and the inside radius of second shell 12 is more than first shell
The inside radius of body 11, then so that second shell 12 is rotated relative to first shell 11, to realize the first shell 11
It opens or closes relative to the second shell 12, be also applied for the present invention.
In the following, the inside radius for continuing to be more than with the inside radius of first shell 11 second shell 12 is by the embodiment of the present invention
Example, the present invention is further explained.
In embodiments of the present invention, in order in launch process, missile is carried out in preset position accurate
It launches, more ontology delivery devices applied to unmanned plane that the embodiment of the present invention is provided further include a positioning element 2, described fixed
Position component 2 can be fixed in the first shell 11, be positioned with the placement position to the object to be thrown.And positioning element
2 have the laser designator of instruction positioning function.Certainly, in order to observe impression information to be put in real time, and acquisition
The geographical location information on ground is launched, the embodiment of the present invention is additionally provided with photographic device 3, and the photographic device 3 is fixed on described
In first shell 11, to carry out real-time photography to the placement position of the object to be thrown.
It is noted that actuator 14, positioning element 2 and photographic device 3 involved in the embodiment of the present invention, it can be equal
Either earth station or remote terminal are connect into row information transmission with the flight control system inside unmanned plane, are controlled with passing through to fly
Either earth station or remote terminal send driving instruction to system processed to the actuator 14, are then driven by the actuator 14
The second shell 12 is moved to be rotated relative to the first shell 11.
Further, Fig. 5-6 is please referred to, for the second shell 12, the second shell 12 may include：
Drive end 121 and synchronous end 122.The driving end 121 is symmetrically distributed with the synchronous end 122 in the second shell 12
Both ends.It is also understood that the driving end 121 and the both ends that the synchronous end 122 is the second shell 12.Institute simultaneously
Stating ontology 1 further includes：Bearing assembly 15, the first cover body 16 and the second cover body 17.Wherein, first cover body 16 is fixed on described
It drives on 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 driving end 121, to receive
Drive signal drives the driving end 122 to be rotated, while end 121 being driven to make second shell as one end of second shell 12
Body 12 is whole to synchronize rotation therewith.The bearing assembly 15 is movable with the synchronous end 122 in second cover body 17
Connection, and the bearing assembly 15 rotates synchronously in second cover body 17 with the 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 shell 11 and second shell 12 matches.First cover body 16 includes one first circular open ends 161, and
It is fixed on the driving 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 driving 121 connecting portion of end, i.e., described first is round
Open end 161 is the maximum circular port of diameter in the hemispherical configuration.Likewise, second cover body 17 is in hemisphere
Shape structure so that semicircle opening of the circular open of the second cover body 17 also with first shell 11 and second shell 12 matches.
Second cover body 17 includes one second circular open ends 171, and is fixed on by second circular open ends 171 described same
It walks on end 122.Here, the second cover body 17 be in hemispherical configuration, it can be understood as the second cover body 17 by with 122 interconnecting piece of synchronous end
It is gradually reduced to its tail end, internal diameter at position, i.e., second circular open ends 171 are that diameter is maximum in the hemispherical configuration
One circular port.
Needing exist for special emphasis is, why first cover body 16 and second cover body 17 is designed to 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 be applied to unmanned plane more ontology delivery devices windward side) be used as windward side when, the resistance of wind is along first cover body
16 and/or the spherical surface of second cover body 17 slowed down, and then maximumlly reduce provided in an embodiment of the present invention answer
The resistance that more ontology delivery devices for unmanned plane are received in operational process in the air.It is also possible to so that when encountering
When bad weather circumstances such as thunderstorm weather, landing, can be in the rainwater on first cover body 16 and/or second cover body 17
It flows down along the spherical surface of first cover body 16 and/or second cover body 17, avoids ponding.
For actuator 15, the actuator 15 may include in embodiments of the present invention：Steering engine 141 and steering engine disk
142.Wherein, the steering engine 141 is fixed in first cover body 16.The steering engine disk 142 is fixed on the driving end 121
On, and be flexibly connected with the steering engine 141, to obtain control instruction by the steering engine 141, drive 142 band of steering engine disk
The driving end 121 is moved to be rotated.It is revolved therewith with this to realize that the rotation drive second shell 12 at driving end 121 is whole
Turn, realizes that the second shell 12 is opened or closed relative to the first shell 11.That is, referring to when steering engine 141 obtains control
It enables, when driving the steering engine disk 142 that the driving end 121 (second shell 12) is driven to be opened relative to the first shell 11,
Then the lateral surface of the second shell 12 and the medial surface of the first shell 11 are (can be understood as of being bonded to each other at this time
Overlap), storage region 13 is opened, and object to be thrown is launched.When the acquisition control instruction of steering engine 141, the steering engine is driven
When disk 142 drives the driving end 121 (second shell 12) to be closed relative to the first shell 11, then the second shell at this time
The lateral surface of body 12 and the medial surface of the first shell 11 are (can be understood as misaligned) being separated from each other, at this time by
Clearance space between the second shell 12 and the first shell 11 constitutes the storage region 13, that is, object to be thrown is deposited
Storage is in the storage region 13.
In addition, in embodiments of the present invention, further referring to Fig. 5-6, the actuator 14 can also include：First connects
Connect disk 143 and the second terminal pad 18.Wherein, first terminal pad 143 is clamped with 161 phase of the first circular open ends, and
The driving end 121 is fixed in first terminal pad 143, one end of the first shell 11 and first terminal pad
143 phases are clamped.
Specifically, be clamped by first terminal pad 143 and 161 phase of the first circular open ends, and the drive
Moved end 121 is fixed in first terminal pad 143, this is allowed for when steering engine 141 drives steering engine disk 142 to be rotated, rotation
Steering engine disk 142 in turning drives the driving end 121 to synchronize rotation, and due to driving end 121 and first terminal pad
It is fixedly connected between 143, so that first terminal pad 143 also rotates synchronously.By first terminal pad 143 and institute
State the first circular open ends 161, one end of the first shell 11 is mutually clamped, therefore first terminal pad 143 was rotating
Cheng Zhong, you can realize first circular open ends 161 (the first cover body 16) and the first shell 11 relative in rotation
First terminal pad remains static.
For the snap fit between first terminal pad 143 and first circular open ends 161, first company
The snap fit between disk 143 and one end of the first shell 11 is connect, can be in first circular open ends 161
Side opens up the annulus sliding slot of a recess, opens up the boss of a protrusion in the edge of first terminal pad 143, and pass through this
Boss is connected in the annulus sliding slot of the inside 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 first terminal pad 143 and one end of the first shell 11,
Can also be that an annulus sliding slot is opened up at the edge side surface of the first terminal pad 143, it at this time can be by first terminal pad 143
On the boss that opens up be interpreted as in 143 diametric(al) of the first terminal pad, the annulus opened up in first terminal pad 143
In the disk of first terminal pad 143, the plane where the two is mutually perpendicular to sliding slot.The one of the first shell 11 simultaneously
End offers the boss of a protrusion, and is connected at the edge side surface of first terminal pad 143 and is opened up by the boss
In annulus sliding slot, the clamping between first terminal pad 143 and the first shell 11 is realized with this, and make described first
Terminal pad 143 can be rotated relative to the first shell.
It certainly, can be opposite relative to the first shell 11, first cover body 16 for first terminal pad 143
Rotation, i.e., during the first terminal pad 143 rotates, the first shell 11, first cover body 16 are stationary.Also deposit
In other design methods, above-mentioned first terminal pad 143 of the embodiment of the present invention and first circular open ends 161 it
Between mutually clamping, first terminal pad 143 and the first shell 11 to be mutually clamped only be a kind of mode wherein realized for one end,
Not limit to.
For example, it is also possible to be by one end of first terminal pad 143 and the first shell 11 respectively with described first
161 phase of the first circular open ends of cover body 16 is clamped, i.e., in the edge of first circular open ends 161, and leans near side (ns)
The medial surface of edge position, opens up the annulus sliding slot of recess, while starting a matching in the edge of the first terminal pad 143 respectively
Boss, also open up a matched boss in the edge of one end of first shell 11, and then respectively by the first terminal pad 143
Edge boss be connected to the first circular open ends 161 in the annulus sliding slot of edge medial surface, and by
The boss of one end of one shell 11 is connected in the annulus sliding slot of 161 edge of the first circular open ends, can also be realized with this
First terminal pad 143 can be relatively rotated relative to the first shell 11, first cover body 16, i.e., in the first connection
During disk 143 rotates, the first shell 11, first cover body 16 are stationary, may also apply to the present invention.
You need to add is that first terminal pad 143 is between the steering engine disk 142 and the driving end 121, institute
It states steering engine disk 142 to be fixedly connected with first terminal pad 143, to drive the steering engine disk successively by the steering engine 141
142, first terminal pad 143 drives the driving end 121 to be rotated.The steering engine disk 142 and first terminal pad
Being fixedly connected between 143 can be screw connection, can also be to be bolted, the present invention does not limit, as long as enabling to
Therebetween what can be rotated synchronously is fixedly connected, then within protection scope of the present invention.
It is corresponding with the first terminal pad 143, more ontology delivery devices provided in an embodiment of the present invention applied to unmanned plane
Further include：Second terminal pad 18, second terminal pad 18 is clamped with 171 phase of the second circular open ends, and the synchronization
End 122 is fixed in second terminal pad 18, and the other end of the second shell 12 is clamped with 18 phase of the second terminal pad；
The bearing assembly 15 is flexibly connected by second terminal pad 18 with the synchronous end 122 in second cover body 17.
Identical, second terminal pad 18 is clamped with 171 phase of the second circular open ends, and the synchronous end 121
It is fixed in second terminal pad 18, this is allowed for when steering engine 141 drives steering engine disk 142 to be rotated, the rudder in rotation
Machine disk 142 drives the driving end 121 (second shell 12) to synchronize rotation, and due to synchronous end 122 and second company
It connects and is fixedly connected between disk 18, so that second terminal pad 18 also rotates synchronously.Due to second terminal pad 18 with
Second circular open ends 171, the first shell 11 the other end be mutually clamped, therefore second terminal pad 18 is rotating
In the process, you can realize second circular open ends 171 (the second cover body 17) and the first shell 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, second company
The snap fit between disk 18 and the other end of the first shell 11 is connect, can be in second circular open ends 171
Inside opens up the annulus sliding slot of a recess, opens up the boss of a protrusion in the edge of second terminal pad 18, and pass through
The boss is connected in the annulus sliding slot of 171 inside of the second circular open ends, and second terminal pad 18 and institute are implemented in this
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 second terminal pad 18 and the other end of the first shell 11
Formula can also be that an annulus sliding slot is opened up at the edge side surface of the second terminal pad 18, at this time can be by second terminal pad
The boss opened up on 18 is interpreted as in 18 diametric(al) of the second terminal pad, the annulus opened up in second terminal pad 18
In the disk of second terminal pad 18, the plane where the two is mutually perpendicular to sliding slot.The first shell 11 is another simultaneously
One end also offers the boss of a protrusion, and is connected at the edge side surface of second terminal pad 18 and is opened by the boss
If in annulus sliding slot, the clamping between second terminal pad 18 and the first shell 11 is realized with this, and make described the
Two terminal pads 18 can be rotated relative to the first shell 11.
It certainly, can be opposite relative to the first shell 11, second cover body 17 for second terminal pad 18
Rotation, i.e., during the second terminal pad 18 rotates, the first shell 11, first cover body 17 are stationary.Also deposit
In other design methods, above-mentioned second terminal pad 18 of the embodiment of the present invention and second circular open ends 171 it
Between mutually clamping, second terminal pad 18 and the first shell 11 the other end to be mutually clamped only be a kind of side wherein realized
Formula is not limited to.
For example, it is also possible to be by the other end of second terminal pad 18 and the first shell 11 respectively with described second
171 phase of the second circular open ends of cover body 17 is clamped, i.e., in the edge of second circular open ends 171, and leans near side (ns)
The medial surface of edge position, opens up the annulus sliding slot of recess, while starting a matching in the edge of the second terminal pad 18 respectively
Boss, also open up a matched boss in the edge of the other end of first shell 11, and then respectively by the second terminal pad
18 edge boss is connected to the second circular open ends 171 in the annulus sliding slot of edge medial surface, and will
The boss of the other end of first shell 11 is connected in the annulus sliding slot of 171 edge of the second circular open ends, also may be used with this
Realize that second terminal pad 18 can be relatively rotated relative to the first shell 11, second cover body 17, i.e., second
During terminal pad 18 rotates, the first shell 11, second cover body 17 are stationary, may also apply to the present invention.
By 143 and second terminal pad 18 of above-mentioned first terminal pad, the second shell 12 and the first shell are realized
The connection type of relative rotation between body 11 realizes the second shell 12 and can be at relative to the first shell 11
The state opened or closed.Certainly, in order to mitigate main screw lift, since the first terminal pad 143 will be with the disk of steering engine disk 142
Flexible connection, therefore for the first terminal pad 143 using solid structure, and for the second terminal pad 18, due to
It need not connect with the disk of steering engine disk 142, therefore the structure of " hollow body " can be used to set as possible the second terminal pad 18
Meter, it is automatic to mitigate, such as：Second terminal pad includes：Cross type frame 181, support disk 182 are frame 183.Cross type frame
181 are used to connect the support disk 182 and the frame 183 as support frame so that the support disk 182 is fixed
In in the frame 183, replaces the solid structure of the first terminal pad 143 by the structure of cross type frame 181 with this, reach
Mitigate the technique effect of dead weight.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 may include a bearing 151 and a ring flange 152.Wherein, the bearing 151 and described
The bearing at the support disk 182 of ring flange 152 connects.For the bearing 151, the ring flange 152 and the support
The bearing of disk 182 connects, and with the relative rotation of the second terminal pad 18 of realization to be the prior art, details are not described herein again.It is worth
One is mentioned that, the bearing assembly 15 is arranged in the embodiment of the present invention, is in order to enable the bearing assembly 15 and the driving
Part 14 constitutes the balance fulcrum of a pair of of rotation at the both ends of the second shell 12, to avoid when there is only actuator 14, this is a
When pivot point, second shell 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 each meant
Fuselage bottom secure an ontology 1, but the quantity present invention of ontology 1 is not limited.Namely in the present invention, institute
The quantity for stating ontology 1 is can be a with n, and the bottom for being fixed on the unmanned plane that the n ontologies 1 can be parallel.Meanwhile institute
The quantity for stating actuator 14 is corresponding with the quantity of the ontology 1, and each described actuator 14 accordingly with described in one
The second shell 12 in ontology 1 is flexibly connected；Wherein, the n is more than or equal to 2, and each described actuator 14 is distinguished
Acquisition independently controls signal, accordingly controls the second shell 12 in an ontology 1 relative to accordingly one
The first shell 11 is rotated.
For example, with continued reference to Fig. 1-4, one embodiment of the present invention when as n=2, at this time for the ease of connection 2
A or multiple ontologies 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
Ontology 1 is parallel to be fixed on the connecting seat 4.
Specifically, the connecting seat may include：Pedestal 41, the first lid 42 and the second lid 43.
Wherein, the pedestal 41 includes：First side, second side, third side and the 4th side；And first side
The pedestal to form that an inside is in hollow-core construction is surrounded in face, the second side, the third side and the 4th side
41；The first side and the second side are two opposites, and the third side and the 4th side are two right
Facade；2 ontologies 1 are symmetrically fixed on the third side and the 4th side.The lid of first lid 42 closes
In the first side, and the connecting seat 4 is fixedly connected by first lid 42 with the bottom of the unmanned plane；Institute
It states the second lid 43 lid and closes and offer the first projection window 431 and the in the second side, and on second lid 43
Two projection windows 432.The positioning element 2 is fixed at the first projection window 431, and the photographic device 3 is fixed on institute
It states at the second projection window 432.Identical, the positioning element 2 can be laser designator；The photographic device 3 can be
Video camera.
It should be noted last that the above specific implementation mode is merely illustrative of the technical solution of the present invention and unrestricted,
Although being described the invention in detail with reference to example, it will be understood by those of ordinary skill in the art that, it can be to the present invention
Technical solution be modified or replaced equivalently, without departing from the spirit of the technical scheme of the invention and range, should all cover
In the scope of the claims of the present invention.
Claims (2)
1. a kind of more ontology delivery devices applied to unmanned plane, which is characterized in that more ontologies applied to unmanned plane are thrown
Putting device includes：
N ontology, each described ontology include：
Storage region, for storing object to be thrown；
First shell；
Second shell, the first shell and second shell flexible connection, and the two can relatively rotate, the first shell
Clearance space between the second shell constitutes the storage region, and the storage region is cylindrical；
N actuator, and in each described actuator accordingly with the second shell activity in an ontology
Connection；The n actuators obtain independently control signal respectively, accordingly control the second shell in an ontology
Body is rotated relative to an accordingly first shell；
Connecting seat, the n ontologies are fixed on the connecting seat, and the n ontologies are mutually parallel two-by-two；And the connection
Seat is fixed on the unmanned plane
Wherein, n is 2 or 3 or 4；
Further include：Positioning element, the positioning element are fixed on the connecting seat, with the placement position to the object to be thrown into
Row positioning；
Further include：Photographic device, the photographic device are fixed on the connecting seat, with the placement position to the object to be thrown into
Row real-time photography；
The positioning element is laser designator；The photographic device is video camera；
The second shell includes：Drive end and synchronous end, the driving end and the synchronous end are symmetrically distributed in described the
The both ends of two shells；
The ontology further includes：Bearing assembly；First cover body, first cover body is fixed on the driving end, and the drive
Moving part is fixed in first cover body；Second cover body, second cover body is fixed on the synchronous end, and the bearing group
Part is fixed in second cover body；Wherein, the actuator is flexibly connected in first cover body with the driving end, institute
It states bearing assembly to be flexibly connected with the synchronous end in second cover body, and the bearing assembly is in second cover body
It is rotated synchronously with the synchronous end；
First cover body is in hemispherical configuration, and first cover body includes one first circular open ends, and passes through described first
Circular open ends are fixed on the driving end；First circular open ends are diameter maximum one in the hemispherical configuration
A circular port；It is in hemispherical configuration with, second cover body, second cover body includes one second circular open ends, and is led to
Second circular open ends are crossed to be fixed on the synchronous end；Second circular open ends are straight in the hemispherical configuration
The maximum circular port of diameter；
The first shell is in semi-circular cylindrical, and one end of the first shell is fixedly connected with first circular open ends, separately
One end is fixedly connected with second circular open ends；The second shell is in semi-circular cylindrical, the inside radius of the first shell
Lateral surface more than the inside radius of the second shell, and the second shell is bonded the medial surface of the first shell and is turned
It is dynamic；
The actuator includes：Steering engine, the steering engine are fixed in first cover body；Steering engine disk, the steering engine disk are fixed on
It on the driving end, and is flexibly connected with the steering engine, to drive the driving end by steering engine disk described in the servo driving
It is rotated；
The actuator further includes：First terminal pad, first terminal pad is mutually clamped with first circular open ends, and institute
It states driving end to be fixed in first terminal pad, one end of the first shell is mutually clamped with first terminal pad；Wherein,
First terminal pad between the steering engine disk and the driving end, fix and connect by the steering engine disk and first terminal pad
It connects, to drive the steering engine disk, first terminal pad that the driving end is driven to be rotated successively by the steering engine；Second
Terminal pad, second terminal pad are mutually clamped with second circular open ends, and the synchronous end is fixed on described second and is connected
It connects on disk, the other end of the second shell is mutually clamped with second terminal pad；The bearing assembly is in second cover body
It is interior to be flexibly connected with the synchronous end by second terminal pad.
2. being applied to more ontology delivery devices of unmanned plane as described in claim 1, which is characterized in that the connecting seat packet
It includes：
Pedestal, the pedestal include：First side, second side, third side and the 4th side；And the first side, institute
It states second side, the third side and the 4th side and surrounds the pedestal to form that an inside is in hollow-core construction；It is described
First side and the second side are two opposites, and the third side and the 4th side are two opposites；Two
A ontology is symmetrically fixed on the third side and the 4th side；
First lid, first cover cap close in the first side, and the connecting seat by first lid with
The bottom of unmanned plane is fixedly connected；
Second lid, second cover cap closes in the second side, and offers the first projection on second lid
Window and the second projection window.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201610789848.6A CN106275437B (en) | 2016-08-31 | 2016-08-31 | More ontology delivery devices applied to unmanned plane |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610789848.6A CN106275437B (en) | 2016-08-31 | 2016-08-31 | More ontology delivery devices applied to unmanned plane |
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| CN106275437A CN106275437A (en) | 2017-01-04 |
| CN106275437B true CN106275437B (en) | 2018-11-13 |
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Citations (4)
| 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 |
| 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 |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS60193899U (en) * | 1984-06-05 | 1985-12-24 | 日本飛行機株式会社 | Aircraft payload launcher |
-
2016
- 2016-08-31 CN CN201610789848.6A patent/CN106275437B/en active Active
Patent Citations (4)
| 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 |
| 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 |
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| Publication number | Publication date |
|---|---|
| CN106275437A (en) | 2017-01-04 |
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