CN109606609A - A kind of unmanned plane - Google Patents
A kind of unmanned plane Download PDFInfo
- Publication number
- CN109606609A CN109606609A CN201811632613.1A CN201811632613A CN109606609A CN 109606609 A CN109606609 A CN 109606609A CN 201811632613 A CN201811632613 A CN 201811632613A CN 109606609 A CN109606609 A CN 109606609A
- Authority
- CN
- China
- Prior art keywords
- connecting pin
- unmanned plane
- fuselage
- hook
- function head
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Pivots And Pivotal Connections (AREA)
Abstract
The invention discloses a kind of unmanned planes, are related to air vehicle technique field.The unmanned plane includes fuselage, power device and function head, the first connecting pin is provided on fuselage, the side wall of first connecting pin is provided with hinge seat and multiple locks, second connection end is provided on function head, pelican hook and multiple latch hooks are provided on the side wall of second connection end, pelican hook is used to cooperate with hinge seat, so that the end wall that function head around hinge seat turns to second connection end is bonded with the end wall of the first connecting pin, lock is for when the end wall of second connection end is bonded with the end wall of the first connecting pin, it is detachably connected with latch hook, power device is set to the one end of fuselage far from the first connecting pin.The function head of unmanned plane provided by the invention is connect with fuselage more to be consolidated, and reduces influence of the power device to connective stability, improves job stability and the safety of unmanned plane.
Description
Technical field
The present invention relates to air vehicle technique fields, in particular to a kind of unmanned plane.
Background technique
Currently, unmanned plane on the market, gradually tends to modularization, unmanned plane is integrally divided into multiple modules, according to tool
The selectively replacement module of function and usage needed for body.Current unmanned plane function head and fuselage often use the connection side of plug-in type
Formula realizes the detachable installation of function head by the cooperation of plug connector and plug division.
The replaceable installation of function head realized using this connection type, connective stability is very poor, between head and fuselage
Easily there is larger gap, during unmanned plane during flying, the influence of the external environments such as wind-engaging, rain and Unmanned Aerial Vehicle Powerplants,
Often there is violent oscillatory motion in the function head of unmanned plane, influences the normal work of head function device, or even be detached from fuselage
Connection.
Summary of the invention
The purpose of the present invention is to provide a kind of unmanned plane, function head can be bonded with fuselage, and can
Reduce influence of the power device to stability.
The present invention provides a kind of technical solution:
A kind of unmanned plane, including fuselage, power device and function head are provided with the first connecting pin, institute on the fuselage
The side wall for stating the first connecting pin is provided with hinge seat and multiple locks, is provided with second connection end on the function head, described
Pelican hook and multiple latch hooks are provided on the side wall of second connection end, the pelican hook is used to cooperate with the hinge seat, so that
The function head is bonded around the end wall that the hinge seat turns to the second connection end with the end wall of first connecting pin,
The lock is removable with the latch hook for when the end wall of the second connection end is bonded with the end wall of first connecting pin
Connection is unloaded, the power device is set to the one end of the fuselage far from first connecting pin.
Further, it is provided with circuit card on the end wall of first connecting pin, be arranged on the circuit card
There is spliced eye, connection-peg is provided on the end wall of the second connection end, the connection-peg is used for when first connecting pin
It when end wall is bonded with the end wall of the second connection end, is inserted into the spliced eye, so that the function head is powered.
Further, battery is provided on the circuit card, the battery is electrically connected with the spliced eye.
Further, the hinge seat includes first base and first crossbeam, and the first base is set to described first
On the side wall of connecting pin, the first crossbeam is set in the first base, for cooperating with the pelican hook.
Further, the pelican hook includes arm hook and second base, and the second base is set to second connection
On the side wall at end, the arm hook is set in the second base, for being hooked on the first crossbeam, so that the function
Head is rotated around the first crossbeam.
Further, the lock includes third pedestal, pull-push piece and padlock part, and the third pedestal is set to described the
On the side wall of one connecting pin, one end of the pull-push piece and the third pedestal are hinged, the other end of the pull-push piece with it is described
One end of padlock part is hinged, and the pull-push piece is used for around the third base rotation, to drive the padlock part and the latch hook
Cooperation is detached from cooperation, and the other end of the padlock part is provided with second cross beam, and the second cross beam with the latch hook for matching
It closes.
Further, the latch hook includes the 4th pedestal and hook, and the 4th pedestal is set to the second connection end
Side wall on, the hook is set on the 4th pedestal, be used for and the second cross beam cooperate.
Further, equipped with function device on the function head, the function device and the function head are removable
Unload connection.
Further, the unmanned plane further includes flank, empennage and rotor arm, and the side wall of the flank and the fuselage can
Dismantling connection, the rotor arm are detachably connected with the flank, and the empennage and the fuselage are far from first connecting pin
One end be detachably connected.
Further, the empennage includes the flat wing and the vertical wing, and the vertical wing and the fuselage are far from first connecting pin
One end be detachably connected, the flat wing is detachably connected with the vertical wing far from one end of the fuselage.
Compared with prior art, unmanned plane provided by the invention is provided with the first connecting pin, the side of the first connecting pin on fuselage
Wall is provided with hinge seat and multiple locks, and second connection end is provided on function head, is provided on the side wall of second connection end
Pelican hook and multiple latch hooks, pelican hook is used to cooperate with hinge seat, so that function head around hinge seat turns to second connection end
End wall be bonded with the end wall of the first connecting pin, lock when the end wall of second connection end with the end wall of the first connecting pin for being bonded
When, it is detachably connected with latch hook, power device is set to the one end of fuselage far from the first connecting pin.Pass through hinge seat and pelican hook
Cooperation and the cooperation of latch hook and lock realize being bonded for function head and fuselage, meanwhile, power device is set to machine
The one end of body far from connection head, keeps its influence in the operating condition to function head smaller.Therefore, nothing provided by the invention
Man-machine beneficial effect is: the connection of its function head and fuselage is more firm, and reduces power device to stable connection
The influence of property, improves job stability and the safety of unmanned plane.
Detailed description of the invention
In order to illustrate the technical solution of the embodiments of the present invention more clearly, below will be to needed in the embodiment attached
Figure is briefly described.It should be appreciated that the following drawings illustrates only certain embodiments of the present invention, therefore it is not construed as pair
The restriction of range.It for those of ordinary skill in the art, without creative efforts, can also be according to this
A little attached drawings obtain other relevant attached drawings.
Fig. 1 is the structural schematic diagram for the unmanned plane that the embodiment of the present invention provides；
Fig. 2 is the structural schematic diagram of Fig. 1 middle fuselage；
Fig. 3 is the structural schematic diagram of function head in Fig. 1；
Fig. 4 is the fit structure schematic diagram of pelican hook and hinge seat in Fig. 1；
Fig. 5 is the fit structure schematic diagram of lock and latch hook in Fig. 1.
Icon: 100- unmanned plane；110- fuselage；The first connecting pin 111-；112- hinge seat；1121- first base；
1122- first crossbeam；113- lock；1131- third pedestal；1132- pull-push piece；1133- padlock part；1134- second cross beam；
114- circuit card；1141- spliced eye；1142- battery；120- power device；130- function head；The connection of 131- second
End；132- pelican hook；1321- arm hook；1322- second base；133- latch hook；The 4th pedestal of 1331-；1332- hook；134- function
It can equipment；140- flank；150- empennage；The flat wing of 151-；152- hangs down the wing；160- rotor arm.
Specific embodiment
In order to make the object, technical scheme and advantages of the embodiment of the invention clearer, below in conjunction with the embodiment of the present invention
In attached drawing, technical scheme in the embodiment of the invention is clearly and completely described.Obviously, described embodiment is
A part of the embodiment of the present invention, instead of all the embodiments.The present invention being usually described and illustrated herein in the accompanying drawings is implemented
The component of example can be arranged and be designed with a variety of different configurations.
Therefore, the detailed description of the embodiment of the present invention provided in the accompanying drawings is not intended to limit below claimed
The scope of the present invention, but be merely representative of selected embodiment of the invention.Based on the embodiments of the present invention, this field is common
Technical staff's every other embodiment obtained without creative efforts belongs to the model that the present invention protects
It encloses.
It should also be noted that similar label and letter indicate similar terms in following attached drawing, therefore, once a certain Xiang Yi
It is defined in a attached drawing, does not then need that it is further defined and explained in subsequent attached drawing.
In the description of the present invention, it is to be understood that, term " on ", "lower", "inner", "outside", "left", "right" etc. indicate
Orientation or positional relationship be based on the orientation or positional relationship shown in the drawings or the invention product using when usually put
Orientation or positional relationship or the orientation or positional relationship that usually understands of those skilled in the art, be merely for convenience of retouching
It states the present invention and simplifies description, rather than the equipment of indication or suggestion meaning or element must have a particular orientation, with specific
Orientation construction and operation, therefore be not considered as limiting the invention.
In addition, term " first ", " second " etc. are only used for distinguishing description, it is not understood to indicate or imply relatively important
Property.
In the description of the present invention, it is also necessary to which explanation is unless specifically defined or limited otherwise, " setting ", " even
Connect " etc. terms shall be understood in a broad sense, for example, " connection " may be a fixed connection, may be a detachable connection, or integrally connect
It connects；It can be mechanical connection, be also possible to be electrically connected；It can be and be directly connected to, can also be indirectly connected with by intermediary, it can
To be the connection inside two elements.For the ordinary skill in the art, can understand as the case may be above-mentioned
The concrete meaning of term in the present invention.
With reference to the accompanying drawing, detailed description of the preferred embodiments.
Embodiment
It please refers to shown in Fig. 1, unmanned plane 100 provided in this embodiment, including fuselage 110, power device 120, function machine
First 130, flank 140, empennage 150 and rotor arm 160.Function head 130 and one end of fuselage 110 are detachably connected, power dress
It sets 120 and is set to the one end of fuselage 110 far from function head 130, the quantity of flank 140 in the present embodiment is two, respectively
It is detachably connected with the side wall of fuselage 110.The quantity of rotor arm 160 in the present embodiment is also two, and respectively with one
Flank 140 is detachably connected, and empennage 150 is detachably connected with fuselage 110 far from one end of the first connecting pin 111.In this implementation
In example, empennage 150 is set to the ipsilateral of 110 connecting power device 120 of fuselage, and empennage 150 includes the flat wing 151 and the vertical wing 152, hangs down
The wing 152 is detachably connected with fuselage 110 far from one end of the first connecting pin 111, and the flat wing 151 is with the vertical wing 152 far from fuselage 110
One end is detachably connected.The connection of unmanned plane 100 provided in this embodiment, function head 130 and fuselage 110 is more firm, and
And influence of the power device 120 to connective stability is reduced, improve job stability and the safety of unmanned plane 100.
In the present embodiment, function head 130 is detachably connected with fuselage 110, and functional set is carried on function head 130
Standby 134, in practical applications, unmanned plane 100 completes task by function device 134, takes on different function heads 130
The function device 134 that can complete different operating task is carried, operator is according to the different task to be executed of unmanned plane 100 to function
Head 130 is replaced.This modularized design, compared to for task two design different complete machines, have it is at low cost, fit
Ying Xingguang, the advantages that being easy to remove and repair.
Unmanned plane 100 provided in this embodiment, function device 134 are detachably connected with function head 130.In the present embodiment
In, the function device 134 carried on function head 130 is camera, and function device 134 is detachably connected with function head 130,
I.e. function device 134 can be replaced very easily.In other embodiments, function device 134 can also for for exploring,
The other equipment device of other purposes such as detecting.Function device 134 can be replaced, so that unmanned plane provided in this embodiment 100
It is provided with stronger adaptability.
Shown in referring to figure 2., the first connecting pin 111 is provided on fuselage 110, the side wall of the first connecting pin 111 is provided with
Hinge seat 112 and multiple locks 113.In the present embodiment, the quantity of hinge seat 112 is one, and the quantity for latching 113 is two
It is a, also, two locks 113 are respectively arranged at the two neighboring side wall of the side wall of the first connecting pin 111 setting hinge seat 112
On.
It is additionally provided with circuit card 114 on first connecting pin 111, spliced eye 1141 is provided on circuit card 114,
In the present embodiment, battery 1142 is additionally provided on circuit card 114, battery 1142 is electrically connected with spliced eye 1141, i.e., electric
Pond 1142 is connected to spliced eye 1141.Spliced eye 1141 is used for for 130 grafting of function head, with to carrying on function head 130
Function device 134 power.
Shown in referring to figure 3., it is provided with second connection end 131 on function head 130, on the side wall of second connection end 131
Be provided with pelican hook 132 and multiple latch hooks 133, in the present embodiment, with the hinge seat 112 being arranged on the first connecting pin 111 and
Lock 113 is corresponding, and the quantity for the pelican hook 132 being arranged in second connection end 131 is one, and the quantity of latch hook 133 is two, and
And pelican hook 132 is correspondingly arranged with hinge seat 112, two latch hooks 133 are correspondingly arranged with two locks 113 respectively.
Pelican hook 132 is used to cooperate with hinge seat 112, so that 130 around hinge seat 112 of function head turns to the second connection
The end wall at end 131 is bonded with the end wall of the first connecting pin 111, and lock 113 when the end wall of second connection end 131 and first for connecting
When connecing the end wall fitting at end 111, it is detachably connected with latch hook 133.In actual installation process, function head 130 and fuselage 110
When connection, pelican hook 132 and hinge seat 112 are cooperated first, after working good, 112 rotating function head 130 of around hinge seat, until
The end wall of second connection end 131 is bonded with the end wall of the first connecting pin 111, when two end walls are bonded, by lock 113 and latch hook
133 connection cooperations, complete the installation of function head 130.
Connection-peg 134 is provided on the end wall of second connection end 131, connection-peg 134 is used for when the end of the first connecting pin 111
It when wall is bonded with the end wall of second connection end 131, is inserted into spliced eye 1141, so that function head 130 is powered.Connection-peg 134
It is corresponding with spliced eye 1141, it is rotated in 130 around hinge seat 112 of function head, the end face of second connection end 131 gradually connects with first
The end face at end 111 is connect during, connection-peg 134 is gradually inserted in spliced eye 1141, when the end face of second connection end 131
When being bonded completely with the end face of the first connecting pin 111 completely, connection-peg 134 is connect in place with spliced eye 1141, battery 1142 with
Function head 130 is connected.
In the present embodiment, by this connection type, the head and fuselage being different from existing capability Modularized unmanned machine
Socket connection mode the radial gravity of function head 130 is converted to by the cooperation of pelican hook 132 and hinge seat 112
The axial tension of fuselage 110, the arm of force increase, so that function head 130 is more firm.Furthermore pass through two locks 113 and two again
A latch hook 133 is corresponding to be connected and fixed, and a symmetrical circumferential pulling force is provided again to function head 130, by 130 jail of function head
The tension in jail is on fuselage 110.
The present embodiment use this connection type, be different from the prior art in socket connection mode, have it is higher
Stability, to function head 130 provide coupling mechanism force, when unmanned plane 100 in working flight state more stable, function device
134 have good working environment, so as to obtain more preferably achievement, such as in the present embodiment, function device
134 be camera, then can obtain apparent stable photographic picture or photo in actual operation.
Shown in referring to figure 4., hinge seat 112 includes first base 1121 and first crossbeam 1122, and first base 1121 is set
It is placed on the side wall of the first connecting pin 111, first crossbeam 1122 is set in first base 1121, for matching with pelican hook 132
It closes.In the present embodiment, first crossbeam 1122 is parallel with the end face of the first connecting pin 111.
Pelican hook 132 includes arm hook 1321 and second base 1322, and second base 1322 is set to second connection end 131
On side wall, arm hook 1321 is set in second base 1322, for being hooked on first crossbeam 1122, so that function head 130
It is rotated around first crossbeam 1122.In the present embodiment, function head 130 fires in the rotation process of first crossbeam 1122, the second connection
The end face at end 131 moves closer to or the end face far from the first connecting pin 111.
Shown in referring to figure 5., lock 113 includes third pedestal 1131, pull-push piece 1132 and padlock part 1133, third pedestal
1131 are set on the side wall of the first connecting pin 111, and one end of pull-push piece 1132 and third pedestal 1131 are hinged, pull-push piece 1132
The other end and padlock part 1133 one end it is hinged, pull-push piece 1132 be used for around third pedestal 1131 rotate, to drive padlock part
1133 cooperate with latch hook 133 or are detached from cooperation, and the other end of padlock part 1133 is provided with second cross beam 1134, second cross beam 1134
For cooperating with latch hook 133.
Latch hook 133 includes the 4th pedestal 1331 and hook 1332, and the 4th pedestal 1331 is set to the side of second connection end 131
On wall, hook 1332 is set on the 4th pedestal 1331, for cooperating with second cross beam 1134.
In practical applications, arm hook 1321 and first crossbeam 1122 cooperate, and the end face of second connection end 131 is connect with first
After the end face fitting at end 111, pull-push piece 1132 is rotated to the direction close to latch hook 133, pull-push piece 1132 drives padlock part 1133
Hook 1332 is moved closer to, after second cross beam 1134 crosses hook 1332, rotates pull-push piece to the direction far from latch hook 133
1132, pull-push piece 1132 drive second cross beam 1134 be caught in hook 1332 hook groove in, continue to rotate pressing pull-push piece 1132 to
Pull-push piece 1132 and padlock part 1133 are in the same plane, at this point, 1134 pairs of second cross beam hooks 1332 have one always
In the same plane, pull-push piece 1132 is locked under the action of this tightening force for tightening force, this tightening force and pull-push piece 1132.Lock
Button 113 locks latch hook 133, and function head 130 is strained and fixed on the end face of the first connecting pin 111 of fuselage 110.
During removing function head 130, as rotating pull-push piece 1132 close to the direction of latch hook 133, drive second cross beam 1134 de-
From the cooperation with hook 1332, after second cross beam 1134 crosses hook 1332, pull-push piece is rotated to the direction far from latch hook 133
1132, it drives second cross beam 113 to move go back to 110 side of fuselage, that is, completes the dismounting of function head 130.
In the present embodiment, function head 130 is cooperated by the hinge seat 112 of pelican hook 132 and fuselage 110, passes through latch hook
133 cooperate with the lock 113 of fuselage 110, realize more firm locking and connect and the power supply to function device 134, and
And installation process is simple to operation.In addition, power device 120 is set to the one end of fuselage 110 far from linkage function head 130,
It is different from the existing unmanned plane that power-equipment is set to head or fuselage interior, so that power device 120 is to function head 130
The influence of connective stability greatly reduce, in addition, in 100 flight course of unmanned plane, air drag that function head 130 is subject to
The thrust provided with power device 120 is in the two sides of itself and fuselage 110, so that function head 130 is more adjacent to fuselage 110.
Therefore, the connection of unmanned plane 100 provided in this embodiment, function head 130 and fuselage 110 is more firm, and reduces dynamic
Influence of the power device 120 to connective stability improves job stability and the safety of unmanned plane 100.
Therefore, the connection of unmanned plane 100 provided by the invention, function head 130 and fuselage 110 is more firm, and subtracts
Small influence of the power device 120 to connective stability, improves job stability and the safety of unmanned plane 100.
The foregoing is only a preferred embodiment of the present invention, is not intended to restrict the invention, for the skill of this field
For art personnel, the invention may be variously modified and varied.All within the spirits and principles of the present invention, made any to repair
Change, equivalent replacement, improvement etc., should all be included in the protection scope of the present invention.
Claims (10)
1. a kind of unmanned plane, which is characterized in that including fuselage, power device and function head, be provided with first on the fuselage
Connecting pin, the side wall of first connecting pin are provided with hinge seat and multiple locks, are provided with the second company on the function head
End is connect, pelican hook and multiple latch hooks are provided on the side wall of the second connection end, the pelican hook is used for and the hinge seat
Cooperation so that the function head around the hinge seat turn to the second connection end end wall and first connecting pin
End wall fitting, the lock is for when the end wall of the second connection end is bonded with the end wall of first connecting pin, with institute
It states latch hook to be detachably connected, the power device is set to the one end of the fuselage far from first connecting pin.
2. unmanned plane according to claim 1, which is characterized in that be provided with circuit on the end wall of first connecting pin and insert
Fishplate bar is provided with spliced eye on the circuit card, connection-peg, the grafting is provided on the end wall of the second connection end
Head is used for when the end wall of first connecting pin is bonded with the end wall of the second connection end, is inserted into the spliced eye, with
The function head is set to be powered.
3. unmanned plane according to claim 2, which is characterized in that be provided with battery, the electricity on the circuit card
Pond is electrically connected with the spliced eye.
4. unmanned plane according to claim 1, which is characterized in that the hinge seat includes first base and first crossbeam,
The first base is set on the side wall of first connecting pin, and the first crossbeam is set in the first base, is used
Cooperate in the pelican hook.
5. unmanned plane according to claim 4, which is characterized in that the pelican hook includes arm hook and second base, described
Second base is set on the side wall of the second connection end, and the arm hook is set in the second base, for being hooked on
On the first crossbeam, so that the function head is rotated around the first crossbeam.
6. unmanned plane according to claim 1, which is characterized in that the lock includes third pedestal, pull-push piece and padlock
Part, the third pedestal are set on the side wall of first connecting pin, and one end of the pull-push piece and the third pedestal are cut with scissors
It connecing, the other end of the pull-push piece and one end of the padlock part are hinged, and the pull-push piece is used for around the third base rotation,
Cooperated with driving the padlock part and the latch hook to cooperate or be detached from, the other end of the padlock part is provided with second cross beam, institute
Second cross beam is stated for cooperating with the latch hook.
7. unmanned plane according to claim 6, which is characterized in that the latch hook includes the 4th pedestal and hook, and described the
Four pedestals are set on the side wall of the second connection end, and the hook is set on the 4th pedestal, for described the
Two beam engagements.
8. unmanned plane according to claim 1, which is characterized in that described equipped with function device on the function head
Function device is detachably connected with the function head.
9. unmanned plane according to claim 1, which is characterized in that the unmanned plane further includes flank, empennage and rotor arm,
The side wall of the flank and the fuselage is detachably connected, and the rotor arm is detachably connected with the flank, the empennage with
The fuselage is detachably connected far from one end of first connecting pin.
10. unmanned plane according to claim 9, which is characterized in that the empennage includes the flat wing and the vertical wing, the vertical wing with
The fuselage is detachably connected far from one end of first connecting pin, the flat wing and the vertical wing far from the fuselage one
End is detachably connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811632613.1A CN109606609A (en) | 2018-12-29 | 2018-12-29 | A kind of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811632613.1A CN109606609A (en) | 2018-12-29 | 2018-12-29 | A kind of unmanned plane |
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| Publication Number | Publication Date |
|---|---|
| CN109606609A true CN109606609A (en) | 2019-04-12 |
Family
ID=66011106
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811632613.1A Pending CN109606609A (en) | 2018-12-29 | 2018-12-29 | A kind of unmanned plane |
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| CN109515706A (en) * | 2018-12-03 | 2019-03-26 | 成都纵横大鹏无人机科技有限公司 | A kind of Modularized unmanned machine |
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| GB2491129B (en) * | 2011-05-23 | 2014-04-23 | Blue Bear Systems Res Ltd | Air vehicle |
| US20130206921A1 (en) * | 2012-02-15 | 2013-08-15 | Aurora Flight Sciences Corporation | System, apparatus and method for long endurance vertical takeoff and landing vehicle |
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| CN108513557A (en) * | 2017-09-27 | 2018-09-07 | 深圳市大疆创新科技有限公司 | Wing components and unmanned vehicle |
| CN107963198A (en) * | 2017-12-26 | 2018-04-27 | 陶文英 | Shipping unmanned aerial vehicle body construction design method and its structure |
| CN108189999A (en) * | 2017-12-28 | 2018-06-22 | 宝鸡特种飞行器工程研究院有限公司 | A kind of split type unmanned plane |
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Application publication date: 20190412 |