CN208559765U

CN208559765U - Docking for unmanned plane emits load carrier

Info

Publication number: CN208559765U
Application number: CN201820898070.7U
Authority: CN
Inventors: 不公告发明人
Original assignee: Ewatt Technology Co Ltd
Current assignee: Ewatt Technology Co Ltd
Priority date: 2018-06-11
Filing date: 2018-06-11
Publication date: 2019-03-01
Anticipated expiration: 2028-06-11

Abstract

The utility model discloses a kind of docking for unmanned plane to emit load carrier, belongs to air vehicle technique field, including emission element, joint unit and load-supporting part.Emission element and joint unit.Emission element includes ejecting end, tube body, handling end and object to be penetrated.Tube body is provided with first side, second side and hollow portion；Handling end is provided with into bullet mouth and control switch；Object to be penetrated is connected with control switch；Joint unit includes the first interface, ontology and the second interface.First interface and fuselage are detachably connected, and ontology and the first interface are fixedly connected, and the second interface is fixedly connected with ontology.Load-supporting part includes the first support arm and the second support arm；Second support arm is provided with third end and the 4th end.The utility model reaches through unmanned plane emission element shattered glass door and window, reduces damage of the recoil to unmanned plane, stablizes the flight attitude of unmanned plane, be conducive to the technical effect succoured to the indicator of trapped personnel in high residential building.

Description

Docking for unmanned plane emits load carrier

Technical field

The utility model belongs to air vehicle technique field, in particular to a kind of docking transmitting load-bearing dress for unmanned plane It sets.

Background technique

Unmanned unmanned plane referred to as " unmanned plane ", is grasped using radio robot and the presetting apparatus provided for oneself Vertical not manned unmanned plane.Without cockpit on machine, but automatic pilot, presetting apparatus, information collecting device are installed etc. Equipment.On ground, naval vessels or machine tool remote control station personnel are by the equipment such as radar, it is tracked, is positioned, is remotely controlled, telemetering and Digital Transmission.It can take off as common unmanned plane under wireless remotecontrol or be launched with booster rocket, it can also be by machine tool Aerial launch is taken to fly.

For unmanned plane, unmanned aerial vehicle body in the prior art is formed using integrally formed structure fabrication.Nobody If owner is by fuselage, wing and positioned at the propeller of head, and is mounted in the video camera on unmanned plane to constitute.Usually From received professional training operator and with take off in the case where parasite power, the lift of flight be by wing and It is provided positioned at the propeller of head.When high-rise fire occurs, each building is observed by the video camera being mounted on unmanned plane The fire condition of layer, then indicator of trapped personnel is saved by aerial ladder.However the glass door and window of high residential building is difficult to smash, if leaning on nothing Man-machine fuselage goes to hit glass, then does not simply fail to shattered glass door and window, also result in damage unmanned plane.Meanwhile unmanned plane is penetrated It hits component and unmanned aerial vehicle body is fixed as one molding structure, if entire unmanned plane will be needed replacing when shooting parts damages, This will increase maintenance cost.

In conclusion in existing unmanned air vehicle technique, unmanned plane can not shattered glass door and window, carried out to glass door and window When shooting, generated recoil will damage unmanned plane, interfere the flight attitude of unmanned plane, cause unmanned plane that cannot succour in time Indicator of trapped personnel in high residential building；Meanwhile the maintenance cost of unmanned plane shooting component is high.

Utility model content

Technical problem to be solved in the utility model be unmanned plane can not shattered glass door and window, carried out to glass door and window When shooting, generated recoil will damage unmanned plane, interfere the flight attitude of unmanned plane, cause unmanned plane that cannot succour in time Indicator of trapped personnel in high residential building；Meanwhile the maintenance cost of unmanned plane shooting component is high.

In order to solve the above technical problems, the utility model provides a kind of docking transmitting load carrier for unmanned plane, The unmanned plane includes fuselage, and the docking transmitting load carrier for unmanned plane includes emission element, the emission element It include: ejecting end；Tube body, the tube body are provided with first side, second side and hollow portion, are provided in the first side First pedestal and the second pedestal；Third pedestal and the 4th pedestal are provided in the second side；End is loaded and unloaded, the handling end is set It is equipped with into bullet mouth and control switch；Object to be penetrated, the object to be penetrated are connected with the control switch, and the level to be penetrated is in described Enter in bullet mouth；Wherein, the tube body be located at the handling end and it is described enter bullet mouth between, the hollow portion pass through it is described enter bullet mouth With the ejecting end；Joint unit, the joint unit include: the first interface, and first interface and the fuselage can Dismantling connection；Ontology, the ontology are fixedly connected with first interface；Second interface, second interface and institute It states ontology to be fixedly connected, the first clamping seat and the second clamping seat is provided on second interface；Wherein, the ontology is located at Between first interface and second interface；The first clamping seat and the second clamping seat are relative to described the The centrosymmetric distribution of two interfaces；First interface and second interface symmetrically divide relative to the ontology Cloth；Load-supporting part, the load-supporting part include: the first support arm, and first support arm is provided with first end and second end, institute It states first end to be fixedly connected with the first clamping seat, the first mounting hole is provided in the second end；Second support arm, described second Support arm is provided with third end and the 4th end, and the third end is fixedly connected with the second clamping seat；It is provided on 4th end Second mounting hole；Wherein, the first end and the second end are the both ends of first support arm opposition, the third end and 4th end is the both ends of the second support arm opposition；First gag lever post passes through first mounting hole, and the second limit Bar passes through second mounting hole.

Further, the docking for unmanned plane emits load carrier further include: first laser transmitter；It is described to penetrate Outlet includes the first positioning area, and the first laser transmitter is fixed on first positioning area.

Further, the docking for unmanned plane emits load carrier further include: second laser transmitter；It is described to penetrate Outlet includes the second positioning area, and the second laser transmitter is fixed on second positioning area.

Further, the docking for unmanned plane emits load carrier further include: image pick-up device；The ejecting end includes Third positioning area, the image pick-up device are fixed on the third positioning area.

Further, the docking transmitting load carrier for unmanned plane includes: first positioning area and described the Two positioning areas are symmetrical relative to the third positioning area.

Further, the docking transmitting load carrier for unmanned plane includes: the hollow portion relative to ground Angular range is 30 ° -60 °.

Further, it is hollow out knot that the docking transmitting load carrier for unmanned plane, which includes: first interface, Structure, and/or, second interface is engraved structure, and/or, the ontology is engraved structure.

The utility model has the advantages that

The utility model provides a kind of docking transmitting load carrier for unmanned plane, by the first side of tube body First pedestal and the second pedestal are set, third pedestal and the 4th pedestal are set in the second side of tube body.It object to be penetrated and will set It sets the control switch at handling end to be connected, so that object to be penetrated is placed on handling end and enter in bullet mouth.By tube body setting at handling end And enter between bullet mouth, pass through hollow portion into bullet mouth and ejecting end.In actual operation, object (such as hoodle) to be penetrated is packed into dress After unloading the entering in bullet mouth of end, pass through control switch by the movement of unmanned plane to drive object to be penetrated to move together specified altitude assignment Object to be penetrated is excited, object to be penetrated is shot to target area (such as window), then smashes object (such as glass of target area Glass).Meanwhile being fixedly connected with the ontology of joint unit and the first interface, the second interface and ontology of joint unit are fixed The first clamping seat and the second clamping seat are arranged on the second interface, ontology is made to be located at the first interface and described second for connection Between interface, the centrosymmetric distribution of the first clamping seat and the second clamping seat relative to the second interface, the first interface It is symmetrical relative to ontology with the second interface.Since the first interface and fuselage of joint unit are detachably connected, if hair Component and/or joint unit damage are penetrated, then does not need replacement unmanned plane, it is only necessary to replace emission element and/or joint unit, just Unmanned plane can be made to can continue to smash the object (such as glass) of target area.Also, by being arranged first on the first support arm End and second end, are arranged the first mounting hole on the second end, so that first end is clamped seat with first and are fixedly connected；In the second support arm Upper setting third end and the 4th end, are arranged the second mounting hole on the 4th end, so that third end is clamped seat with second and are fixedly connected.? Target area (such as window) is shot at.Since the first gag lever post to pass through to the first mounting hole in second end, and by the Two gag lever posts pass through the second mounting hole on the 4th end.The recoil generated when being shot to target area (such as window), can To push the first mounting hole to move along the first gag lever post, the second mounting hole is moved along the second gag lever post, then drives first The movement of support arm and the second support arm reduces recoil to the unfavorable shadow of unmanned plane to consume energy caused by recoil It rings.To reach through the emission element of unmanned plane the glass door and window for smashing high residential building, after reduction is generated when shooting Damage of the recoil to unmanned plane stablizes the flight attitude of unmanned plane, is conducive to succour the indicator of trapped personnel in high residential building Technical effect.

Detailed description of the invention

In order to illustrate the embodiment of the utility model or the technical proposal in the existing technology more clearly, below will be to embodiment Needed in attached drawing be briefly described, it should be apparent that, the accompanying drawings in the following description is only the utility model Some embodiments for those of ordinary skill in the art without creative efforts, can also be according to this A little attached drawings obtain other attached drawings.

Fig. 1 is a kind of overall structure diagram of the grenade instrumentation for unmanned plane provided by the embodiment of the utility model；

Fig. 2 provides a kind of top view illustration of grenade instrumentation for unmanned plane for the utility model embodiment；

Fig. 3 provides a kind of left view schematic diagram of grenade instrumentation for unmanned plane for the utility model embodiment；

Fig. 4 provides a kind of right view schematic diagram of grenade instrumentation for unmanned plane for the utility model embodiment；

Fig. 5 provides a kind of front view schematic diagram of grenade instrumentation for unmanned plane for the utility model embodiment；

Fig. 6 provides a kind of rearview schematic diagram of grenade instrumentation for unmanned plane for the utility model embodiment；

Detailed description of the invention:

100-emission elements, 110-ejecting ends, 120-tube bodies, 121-first sides, 122-second sides, 123- Hollow portion, the 124-the first pedestal, the 125-the second pedestal, 126-third pedestals, the 127-the four pedestal, 130-handling ends, 131-enter bullet mouth, 132-control switches, 140-objects to be penetrated, the 150-the first positioning area, the 160-the second positioning area, and 170-the Three positioning areas, 180-baffles, the 181-the first trajectory, the 182-the second trajectory；

200-joint units, the 210-the first interface, 220-ontologies, the 230-the second interface, the 231-the first clamping Seat, the 232-the second clamping seat；

300-load-supporting parts, the 310-the first support arm, 311-first ends, 312-second ends, the 313-the first installation Hole, the 320-the second support arm, 321-third ends, the 322-the four end, the 323-the second mounting hole；

400-damping parts, the 410-the first gag lever post, the 411-the first fastening end, the 412-the second fastening end, 420-the Two gag lever posts, 421-third fastening ends, the 422-the four fastening end, the 430-the first elastic parts, the 440-the second elastic parts.

Specific embodiment

In order to elaborate to a kind of docking transmitting load carrier for unmanned plane provided by the utility model, with branch Utility model technical problem to be solved is held, in the following, being used for nobody to one kind first in embodiment provided by the utility model The grenade instrumentation of machine elaborates, and then during describing a kind of grenade instrumentation for unmanned plane, further there is needle A kind of docking for unmanned plane provided by the utility model to the extraction of property emits load carrier, to reach complete, clear, bright White purpose.

The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art's every other embodiment obtained, all belongs to In the range of the utility model protection；Wherein "and/or" keyword involved in this implementation, indicate and or two kinds of situations, change Sentence is talked about, and A mentioned by the utility model embodiment and/or B illustrate two kinds of A and B, A or B situations, describe A and B and deposited Three kinds of states, such as A and/or B, indicate: only including A does not include B；Only including B does not include A；Including A and B.

Meanwhile in the utility model embodiment, when component is referred to as " being fixed on " another component, it can be directly another On one component or there may also be components placed in the middle.When a component is considered as " connection " another component, it be can be It is directly connected to another component or may be simultaneously present component placed in the middle.When a component be considered as " being set to " another Component, it, which can be, is set up directly on another component or may be simultaneously present component placed in the middle.The utility model embodiment Used in term "vertical", "horizontal", "left" and "right" and similar statement be merely for purposes of illustration, not It is intended to limit the utility model.

It is first in order to which a kind of grenade instrumentation for unmanned plane provided by the embodiment of the utility model is described in detail Description below explanation first is done to technical term involved in the utility model embodiment:

Detachable connection, which may is that, to be bolted or is bonded；

It is fixedly connected and may is that welding or integrated molding；

Ground may is that ground when unmanned plane is parked；

It takes off the process that may is that unmanned plane reaches aerial rising from ground；

Landing may is that process of the unmanned plane from airborne to ground；

Object 140 to be penetrated can be the article for referring to shattered glass, such as glass marbles, metal hoodle, metal nail etc..

Referring to Figure 1, Fig. 1 is a kind of whole knot of grenade instrumentation for unmanned plane provided by the embodiment of the utility model Structure schematic diagram.A kind of grenade instrumentation for unmanned plane provided by the embodiment of the utility model, a kind of projection for unmanned plane Device includes emission element 100, joint unit 200, load-supporting part 300 and damping part 400.Now to emission element 100, docking Component 200, load-supporting part 300 and damping part 400 carry out following detailed description respectively:

For emission element 100:

Emission element 100 may include ejecting end 110, tube body 120, handling end 130 and object to be penetrated 140.

Tube body 120 is provided with first side 121, second side 122 and hollow portion 123, can be set in first side 121 There are the first pedestal 124 and the second pedestal 125；Third pedestal 126 and the 4th pedestal 127 can be set in second side 122；Dress Unloading end 130 can be set into bullet mouth 131 and control switch 132, and object 140 to be penetrated is connected with control switch 132, and wait penetrate Object 140 is located in bullet mouth 131.Wherein, tube body 120 can be located at handling end 130 and enter between bullet mouth 131, and hollow portion 123 can To pass through into bullet mouth 131 and ejecting end 110；

Ejecting end 110 can also include the first positioning area 150, the second positioning area 160 and third positioning area 170, and first is fixed Position is fixedly installed with first laser transmitter in area 150, and second laser transmitter is fixedly installed on the second positioning area 160, the Image pick-up device is fixedly installed on three positioning areas 170.Wherein, the first positioning area 150 and the second positioning area 160 can be relative to thirds Positioning area 170 is symmetrical；Hollow portion 123 can be 30 ° -60 ° relative to the angular range of second interface 230.

Go out baffle 180 can be installed entering bullet mouth 131, baffle 180 and entering is hinged at bullet mouth 131.And baffle 180 can be connected with control switch 132, and baffle 180 can be located between bullet mouth 131 and control switch 132.

Hollow portion 123 may include the first trajectory 181 and the second trajectory 182.First trajectory 181 and the second trajectory 182 can To be parallel to each other distribution relative to first side 121.Wherein, the first trajectory 181 can be passed through into bullet mouth 131 and ejecting end 110, And the second trajectory 182 can be passed through into bullet mouth 131 and ejecting end 110.

Referring to Figure 1 and Fig. 2, Fig. 1 are a kind of grenade instrumentations for unmanned plane provided by the embodiment of the utility model Overall structure diagram, Fig. 2 provide a kind of top view signal of grenade instrumentation for unmanned plane for the utility model embodiment Figure.Tube body 120 can be metal material and be made, and tube body 120 is rendered as hollow structure, and the hollow structure is for accommodating hoodle waiting Penetrate object 140.Tube body 120 has first side 121 and second side 122, and first side 121 and second side 122 can be distributed It is the face positioned at 120 left and right sides of tube body.The both ends of tube body 120 are handling end 130 respectively and enter bullet mouth 131, are entered at bullet mouth 131 Baffle 180 is can be set, baffle 180 and entering is hinged at bullet mouth 131, i.e., baffle 180 can be beaten relative to bullet mouth 131 is entered It opens or is closed.Baffle 180 is located between bullet mouth 131 and control switch 132, and has in the inside for entering bullet mouth 131 and hold Receive the space of object 140 to be penetrated.Object 140 to be penetrated can be connected with control switch 132, be swashed by the on-off of control switch 132 The object to be penetrated 140 being located in bullet mouth 131 is sent out, makes object 140 to be penetrated from bullet mouth 131 is entered along the arrival ejecting end of hollow portion 123 110, from 110 homed on its target region of ejecting end (such as glass edge of high residential building window).

First laser transmitter, the second positioning area 160 can be fixedly installed on first positioning area 150 of ejecting end 110 On can be fixedly installed with second laser transmitter, image pick-up device can be fixedly installed on third positioning area 170.First laser hair Emitter and second laser transmitter are symmetrical relative to image pick-up device.First laser transmitter and second laser transmitter can be Laser aiming utensil, such as beam of laser is emitted by first laser transmitter, the hot spot which generates in target area can To be the aiming point for indicating object 140 to be penetrated and coming to target.It can be improved by first laser transmitter and second laser transmitter Accuracy after penetrating object 140 and projecting.Image pick-up device can be camera, which can feed back in the region passed through to ground On the display of face operator, ground handling operator passes through the video image and first laser transmitter and second laser Aiming point caused by transmitter, precisely to be shot to target area.

Entering baffle 180 can be installed at bullet mouth 131, make baffle 180 and enter to be hinged at bullet mouth 131.And it keeps off Plate 180 can be connected with control switch 132, and baffle 180 can be located between bullet mouth 131 and control switch 132.In pipeline Can there are the first trajectory 181 and the second trajectory 182, the first trajectory 181 and the second trajectory 182 can be relative to first sides 121 Be parallel to each other distribution.Wherein, the first trajectory 181 can be passed through into bullet mouth 131 and ejecting end 110, and the second trajectory 182 can be with It passes through into bullet mouth 131 and ejecting end 110.In actual use, object 140 to be penetrated can be pre-loaded with the first trajectory 181 and second In trajectory 182, object 140 to be penetrated is blocked by baffle 180, such as two hoodles are respectively charged into the first trajectory 181 and the second bullet In road 182, then by the closure of baffle 180 it is separately fixed at two hoodles in the first trajectory 181 and the second trajectory 182.Baffle The control switch 132 of 180 sides can be connected with two hoodles respectively, when control switch 132 is closed, can excite positioned at the Object to be penetrated 140 in one trajectory 181 and the second trajectory 182 makes the first trajectory of hoodle approach 181 being located in the first trajectory 181, It is projected at a high speed from ejecting end 110, makes the second trajectory of hoodle approach 182 being located in the second trajectory 182, it is also high from ejecting end 110 Rapid fire goes out.Since there are two trajectories for tool, then entering to be packed into two objects 140 to be penetrated in bullet mouth 131, if which overcome only one It is a to be somebody's turn to do after penetrating object 140 when penetrating object 140 when projecting, when the shock strength wait penetrate object 140 is not enough to shattered glass, unmanned plane It is only drop to ground, object 140 to be penetrated of reloading takes off again to original position, is shot at, when this is both expended Between, also it is unfavorable for the technological deficiency succoured in time to indoor indicator of trapped personnel.When in pipeline have the first trajectory 181 and second When trajectory 182, if the shock strength wait penetrate object 140 for being located at the first trajectory 181 when being not enough to shattered glass, can make to be located at the The object to be penetrated 140 of two trajectories 182 emits simultaneously, bigger impact force is generated, then timely shattered glass, convenient for the people of indoor and outdoor Member's disengaging.To reach the glass that can quickly smash target area, the technical effect of indoor indicator of trapped personnel is succoured in time.

Referring to Figure 1, Fig. 1 is a kind of whole knot of grenade instrumentation for unmanned plane provided by the embodiment of the utility model Structure schematic diagram.Angle of the hollow portion 123 relative to the second interface 230 (the second interface 230 can be parallel to each other with ground) Range can be 30 ° -60 °, i.e. the angular range of route when penetrating object 140 and projecting and the second interface 230 can be 30°—60°.Assuming that hollow portion 123 is A relative to the angle of the second interface 230, then 30 °≤A≤60 °.When 30 ° of A <, If emitting object 140 to be penetrated, object 140 to be penetrated will generate recoil, the direction of the recoil and ejecting end 110 it is contrary, At this point, powerful recoil mutually seriously affects the balance of unmanned plane itself, or even the state of flight of unmanned plane is destroyed, leads to nobody Machine stops running well, to be unfavorable for the normal work of unmanned plane, influences the stability of ejecting end 110, reduces the standard of shooting True property.When 60 ° of A >, if emitting object 140 to be penetrated, makes ejecting end 110 and wall close to horizontal state, at this time can not The glass of target area is aimed at, but also powerful recoil caused by object to be penetrated 140 seriously affects unmanned plane itself Balance, or even destroy unmanned plane state of flight, cause unmanned plane stop run well, to be unfavorable for the normal of unmanned plane Work, influences the stability of ejecting end 110, reduces the accuracy of shooting.

For joint unit 200:

The joint unit 200 may include the first interface 210, ontology 220 and the second interface 230.

First interface 210 can be detachably connected with fuselage；Ontology 220 can be fixedly connected with the first interface 210； Second interface 230 can be fixedly connected with ontology 220, and the first clamping seat 231 and the second card are provided on the second interface 230 Joint chair 232；Wherein, ontology 220 can be between the first interface 210 and the second interface 230；First clamping 231 He of seat Second clamping seat 232 can be rendered as symmetrically being distributed relative to the center of the second interface 230；First interface 210 and Two interfaces 230 can be rendered as symmetrical relative to ontology 220.First interface 210 can be rendered as engraved structure, And/or second interface 230 can be rendered as engraved structure, and/or, ontology 220 can be rendered as engraved structure.

Referring to Figure 1 and Fig. 3, Fig. 1 are a kind of grenade instrumentations for unmanned plane provided by the embodiment of the utility model Overall structure diagram, Fig. 3 are that the utility model embodiment provides a kind of left view signal of grenade instrumentation for unmanned plane Figure.The clamping portion to match with the first interface 210 can be set in the fuselage bottom of unmanned plane, first interface 210 It can removably be connected with clamping portion.Ontology 220 can be fixedly connected with the first interface 210, and the second interface 230 can be with Ontology 220 is fixedly connected, and allows to constitute joint unit by the first interface 210, ontology 220 and the second interface 230 200.The first clamping seat 231 and the second clamping seat 232 can be set on the second interface 230.First clamping seat 231 can be with It is mutually permanently connected with the first end 311 of the first support arm 310, the second clamping seat 232 can be with the third of the second support arm 320 End 321 is mutually permanently connected.The center of second interface 230 can be the geometric center of the second interface 230, such as the second rank When the presentation of junction 230 is square, the center of second interface 230 can be the geometric center of square.Ontology 220 can be with It is the part between the first interface 210 and the second interface 230, it can be by the first interface 210, ontology 220 and Two interfaces 230 constitute joint unit 200.

First interface 210 can be rendered as engraved structure, and/or, the second interface 230 can be rendered as hollow out knot Structure, and/or, ontology 220 can be rendered as engraved structure.That is the first interface 210 and the second interface 230 can be rendered as Engraved structure or the first interface 210 and third interface can be rendered as engraved structure etc..Due to the first interface 210 can be rendered as engraved structure, and/or, the second interface 230 can be rendered as engraved structure, and/or, ontology 220 can be with It is rendered as engraved structure；When then the engraved structure can reduce the first interface 210 of production, ontology 220 and the second interface 230 Material, then reduce the weight of the first interface 210, ontology 220 and the second interface 230, when taking off to reduce unmanned plane The weight of entrained load is conducive to the flying height for promoting unmanned plane, increases the cruise duration of unmanned plane.

In order to the first interface 210 can and fuselage be detachably connected and be explained in detail, now said in detailed below Bright: unmanned plane can be multi-rotor unmanned aerial vehicle, and the fuselage of unmanned plane is segmented into including at least three sections, i.e. head, fuselage and machine Tail, and can be attached by the connection type of detachable connection between three sections, being constituted an internal structure with this can The fixed-wing unmanned plane of disassembly, so that when local damage occurs in the fuselage of unmanned plane, corresponding can remove and damage Bad position repairs, and has simple, convenient technical effect.And when the part of fuselage can not due to damaging When reparation, can also the position that can not repair of corresponding dismounting, i.e., the position that can not be repaired is substituted, to overcome In the prior art because fuselage is using integrated whole design, when so that there is fuselage local damage and can not repair, it has to more The technological deficiency for changing the entire fuselage of unmanned plane, reaches and significantly reduces the technical effect of maintenance cost.Also, in unmanned plane Head, and/or, fuselage, and/or, the attachment base to match with the first interface 210 can be set on tail, so that One interface 210 can be detachably connected with the fuselage.It then, must not when local damage, which occurs, in grenade instrumentation to be repaired It is changed without the technological deficiency of the entire fuselage of unmanned plane, reaches and significantly reduces the technical effect of maintenance cost.

For load-supporting part 300:

Load-supporting part 300 may include the first support arm 310 and the second support arm 320.

First end 311 and second end 312, first end 311 and the first clamping seat 231 has can be set in first support arm 310 It is fixedly connected, the first mounting hole 313 can be set in second end 312；

Third end 321 and the 4th end 322, third end 321 and the second clamping seat has can be set in second support arm 320 232 are fixedly connected；The second mounting hole 323 can be set on the 4th end 322；Wherein, first end 311 and second end 312 can be the both ends of the first support arm 310 opposition respectively, and third end 321 and the 4th end 322 can be the second support arm respectively The both ends of 320 opposition.First support arm 310 and/or the second support arm 320 can be and be rendered as engraved structure, to reduce nobody The weight of entrained load when machine takes off is conducive to the flying height for promoting unmanned plane, increases the cruise duration of unmanned plane.

First mounting hole 313 may include first through hole and the second through-hole, and first through hole and the second through-hole are relative to second The center at end 312 can be rendered as symmetrical.Wherein, the first gag lever post 410 passes through first through hole and the second through-hole；First is logical The diameter in hole can be greater than the diameter of the first gag lever post 410, and the diameter of the second through-hole can be greater than the first gag lever post 410 Diameter.Second mounting hole 323 may include third through-hole and fourth hole, and third through-hole and fourth hole are relative to the 4th The center at end 322 can be rendered as symmetrical.Wherein, the second gag lever post 420 can pass through third through-hole and fourth hole；The The diameter of three through-holes can be greater than the diameter of the second gag lever post 420, and the diameter of fourth hole can be greater than the second gag lever post 420 diameter.

Referring to Figure 1 and Fig. 4, Fig. 1 are a kind of grenade instrumentations for unmanned plane provided by the embodiment of the utility model Overall structure diagram, Fig. 4 are that the utility model embodiment provides a kind of right view signal of grenade instrumentation for unmanned plane Figure.First end 311 and second end 312 can be the both ends of the first support arm 310 respectively, and first end 311 can be with the first clamping Seat 231 is fixedly connected, and the first support arm 310 and joint unit 200 is made to link together, when relay part is moved with unmanned plane, The first support arm 310 is driven to move together.The first mounting hole 313, the first mounting hole 313 can be set in second end 312 It may include first through hole and the second through-hole.

In order to which the first gag lever post 410 is explained in detail across first through hole and the second through-hole, following two is now provided Embodiment is described in detail:

The first embodiment.It the aperture direction of first through hole can be with second end 312 close to the plane phase of first through hole It is mutually parallel.First through hole can be formed along the direction of the column body section by installing a column in first end 311, So that the aperture direction of first through hole is parallel to each other relative to ducted body.The diameter of first through hole can be greater than the first gag lever post 410 diameter, it is assumed that the diameter of the first gag lever post 410 is B, and the diameter of first through hole is C1, then C1 > B.Due to first through hole Diameter be greater than the first gag lever post 410 diameter, then the first gag lever post 410 can slide in first through hole, this to be arranged The first support arm 310 outside the first gag lever post 410 can be moved along the first gag lever post 410.When object 140 to be penetrated from After ejecting end 110 projects, it is mobile relative to the first support arm 310 that generated back pressure can push emission element 100, then leads to It crosses and first spring is set between the first fastening end 411 and the first mounting hole 313, in the second fastening end 412 and the first mounting hole Second spring is set between 313, by the deformation of the first spring and/or second spring, to absorb energy caused by object 140 to be penetrated Amount.To overcome the back pressure damage unmanned plane and load-supporting part 300 that generate when penetrating object 140 and projecting, reaches and be conducive to nothing The technical effect that man-machine normal flight and 300 joint unit 200 of load-supporting part work normally.

Second of embodiment.It the aperture direction of second through-hole can be with second end 312 close to the plane phase of first through hole It is mutually parallel.The second through-hole can be formed along the direction of the column body section by installing a column in second end 312, So that the aperture direction of the second through-hole is parallel to each other relative to ducted body.The diameter of second through-hole can be greater than the first gag lever post 410 diameter, it is assumed that the diameter of the first gag lever post 410 is B, and the diameter of the second through-hole is C2, then C2 > B.Due to the second through-hole Diameter be greater than the first gag lever post 410 diameter, then the first gag lever post 410 can slide in the second through-hole, this to be arranged The first support arm 310 outside the first gag lever post 410 can be moved along the first gag lever post 410.When object 140 to be penetrated from After ejecting end 110 projects, it is mobile relative to the first support arm 310 that generated back pressure can push emission element 100, then leads to It crosses and first spring is set between the first fastening end 411 and the first mounting hole 313, in the second fastening end 412 and the first mounting hole Second spring is set between 313, by the deformation of the first spring and/or second spring, to absorb energy caused by object 140 to be penetrated Amount.To overcome the back pressure damage unmanned plane and load-supporting part 300 that generate when penetrating object 140 and projecting, reaches and be conducive to nothing The technical effect that man-machine normal flight and 300 joint unit 200 of load-supporting part work normally.

It should be noted that first through hole and the second through-hole can be different relative to the distance of the first interface 210, such as First through hole is more farther than the distance of second the first interface of through-hole distance 210, then makes between first through hole and the second through-hole With difference in height, after the first gag lever post 410 being made to pass through first through hole and the second through-hole by the difference in height, relative to Ground is heeling condition.First gag lever post 410 can be 30 ° -60 ° relative to the tilt angle on ground.If the first limit Bar 410 is W1 relative to the tilt angle on ground, then 30 °≤W1≤60 °, can make so among the above sky portion 123 relative to The angular range of second interface 230 can be 30 ° -60 °.

After the first gag lever post 410 passes through first through hole and the second through-hole, it is assumed that extended line by first through hole and P1 point is intersected at by the extended line of the second through-hole, is connected by P1 point, first through hole and the second through-hole and forms a right angle trigonometry Shape, the first gag lever post 410 across first through hole and the second throughhole portions are the bevel edge of the right angled triangle.First through hole and The right-angle side that P1 point is formed is Y1, and the right-angle side that the second through-hole and P1 point are formed is Y2, then Y2:

Y1=Z1, then the range of Z1 can be (1/2)≤Z1≤(√ 3)/2.Due to (1/2)≤Z1≤(√ 3)/2, when After one gag lever post 410 passes through first through hole and the second through-hole, the first gag lever post 410 is heeling condition relative to ground, can be with So that hollow portion 123 can be 30 ° -60 ° relative to the angular range of the first interface 210, then ejecting end 110 can be at this time Than handling end 130 closer to ground, then allow the object to be penetrated 140 projected from ejecting end 110 relative to the first interface 210 shootings downwards, not only improve and aim in the sky the glass at door and window, and are conducive to make after penetrating object 140 and generating Recoil tilts upward, overcome recoil it is downward when, will push unmanned plane decline and bump against the technological deficiency of ground or metope.To Having reached makes unmanned plane safety, smooth flight, and the technical effect that object to be penetrated 140 steadily projects.

Continuing with being that a kind of projection for unmanned plane provided by the embodiment of the utility model fills referring to Fig. 1 and Fig. 4, Fig. 1 The overall structure diagram set, Fig. 4 are that the utility model embodiment provides a kind of right view of grenade instrumentation for unmanned plane Schematic diagram.In order to which the second gag lever post 420 is explained in detail across third through-hole and fourth hole, it is real now to provide following two The mode of applying is described in detail:

The first embodiment.It the aperture direction of third through-hole can be with the 4th end 322 close to the plane phase of third through-hole It is mutually parallel.Third through-hole can be formed along the direction of the column body section by installing a column on the 4th end 322, So that the aperture direction of third through-hole is parallel to each other relative to ducted body.The diameter of third through-hole can be greater than the second gag lever post 420 diameter, it is assumed that the diameter of the second gag lever post 420 is B, and the diameter of third through-hole is C3, then C3 > B.Due to third through-hole Diameter be greater than the second gag lever post 420 diameter, then the second gag lever post 420 can slide in third through-hole, this to be arranged The second support arm 320 outside the second gag lever post 420 can be moved along the second gag lever post 420.When object 140 to be penetrated from After ejecting end 110 projects, it is mobile relative to the second support arm 320 that generated back pressure can push emission element 100, then leads to The setting third spring between third fastening end 421 and the second mounting hole 323 is crossed, in the 4th fastening end 422 and the second mounting hole 4th spring is set between 323, by the deformation of third spring and/or the 4th spring, to absorb energy caused by object 140 to be penetrated Amount.To overcome the back pressure damage unmanned plane and load-supporting part 300 that generate when penetrating object 140 and projecting, reaches and be conducive to nothing The technical effect that man-machine normal flight and 300 joint unit 200 of load-supporting part work normally.

Second of embodiment.It the aperture direction of fourth hole can be with the 4th end 322 close to the plane phase of fourth hole It is mutually parallel.Fourth hole can be formed along the direction of the column body section by installing a column on the 4th end 322, So that the aperture direction of fourth hole is parallel to each other relative to ducted body.The diameter of fourth hole can be greater than the second gag lever post 420 diameter, it is assumed that the diameter of the second gag lever post 420 is B, and the diameter of third through-hole is C4, then C4 > B.Due to fourth hole Diameter be greater than the second gag lever post 420 diameter, then the second gag lever post 420 can slide in fourth hole, this to be arranged The second support arm 320 outside the second gag lever post 420 can be moved along the second gag lever post 420.When object 140 to be penetrated from After ejecting end 110 projects, it is mobile relative to the second support arm 320 that generated back pressure can push emission element 100, then leads to The setting third spring between third fastening end 421 and the second mounting hole 323 is crossed, in the 4th fastening end 422 and the second mounting hole 4th spring is set between 323, by the deformation of third spring and/or the 4th spring, to absorb energy caused by object 140 to be penetrated Amount.To overcome the back pressure damage unmanned plane and load-supporting part 300 that generate when penetrating object 140 and projecting, reaches and be conducive to nothing The technical effect that man-machine normal flight and 300 joint unit 200 of load-supporting part work normally.

Continuing with being that a kind of projection for unmanned plane provided by the embodiment of the utility model fills referring to Fig. 1 and Fig. 5, Fig. 1 The overall structure diagram set, Fig. 5 are that the utility model embodiment provides a kind of front view of grenade instrumentation for unmanned plane Schematic diagram.Third through-hole and fourth hole can be different relative to the distance of the first interface 210, such as third through-hole is than the 4th The distance of the first interface of through-hole distance 210 is farther, then makes have difference in height between third through-hole and fourth hole, passes through It is heeling condition relative to ground after the difference in height can make the second gag lever post 420 pass through third through-hole and fourth hole 's.Second gag lever post 420 can be 30 ° -60 ° relative to the tilt angle on ground.If i.e. the first gag lever post 410 relative to The tilt angle on ground is W2, then 30 °≤W2≤60 °, can make so among the above sky portion 123 relative to the second interface 230 angular range can be 30 ° -60 °.

After the second gag lever post 420 passes through third through-hole and fourth hole, it is assumed that by third through-hole extended line and P2 point is intersected at by the extended line of fourth hole, is connected by P2 point, third through-hole with fourth hole and forms a right angle trigonometry Shape, the second gag lever post 420 across third through-hole and fourth hole part are the bevel edge of the right angled triangle.Third through-hole and The right-angle side that P2 point is formed is Y3, and the right-angle side that fourth hole and P1 point are formed is Y4, then Y4:Y3=Z2, then the range of Z2 can To be (1/2)≤Z2≤(√ 3)/2.Due to (1/2)≤Z2≤(√ 3)/2, when the second gag lever post 420 passes through third through-hole and the After four through-holes, the second gag lever post 420 is heeling condition relative to ground, and hollow portion 123 can be made relative to the first linking The angular range in face 210 can be 30 ° -60 °, then ejecting end 110 can then make than handling end 130 closer to ground at this time Obtaining the object to be penetrated 140 projected from ejecting end 110 can be relative to the first shooting downwards of interface 210, and it is right in the sky to not only improve Glass at door and window is aimed at, and the recoil for being conducive to generate object 140 to be penetrated tilts upward, and it is downward to overcome recoil When, it will push the technological deficiency that unmanned plane decline bumps against ground or metope.Make unmanned plane safety, smooth flight to reach, And the technical effect that object 140 to be penetrated steadily projects.

For damping part 400:

The damping part 400 may include the first gag lever post 410, the second gag lever post 420,430 and of the first elastic parts Second elastic parts 440.

First gag lever post 410 can be set the first fastening end 411 and the second fastening end 412, and the first fastening end 411 can be with It is fixedly connected with the first pedestal 124, and the second fastening end 412 can be fixedly connected with the second pedestal 125, the first gag lever post 410 can pass through the first mounting hole 313；Third fastening end 421 and the 4th fastening end 422 has can be set in second gag lever post 420, Third fastening end 421 can be fixedly connected with third pedestal 126, and the 4th fastening end 422 can be with the 4th pedestal 127 It is fixedly connected, the second gag lever post 420 can pass through second mounting hole 323.

First elastic parts 430 can be set in the outside of first gag lever post 410, and the first elastic parts 430 can be with Between the first fastening end 411 and the second fastening end 412；Second elastic parts 440 can be set in the second gag lever post 420 Outside, the second elastic parts 440 can be between third fastening end 421 and the 4th fastening ends 422.Wherein, first is tight Fixed end 411 and the second fastening end 412 can be the both ends of the first gag lever post 410 opposition, third fastening end 421 and the 4th fastening end 422 can be the both ends of the second gag lever post 420 opposition.

First elastic parts 430 may include the first spring and second spring, and the first spring can be set in described first The outside of gag lever post 410, and second spring can be set in the outside of the first gag lever post 410；Wherein, the first spring can position Between the first fastening end 411 and the first mounting hole 313, and second spring can be located at the second fastening end 412 and the first peace It fills between hole 313.Second elastic parts 440 may include third spring and the 4th spring, and third spring can be set in second The outside of gag lever post 420, and the 4th spring can be set in the outside of the second gag lever post 420；Wherein, third spring can position Between third fastening end 421 and the second mounting hole 323, and the 4th spring can be located at the 4th fastening end 422 and the second peace It fills between hole 323.

Referring to Figure 1 and Fig. 6, Fig. 1 are a kind of grenade instrumentations for unmanned plane provided by the embodiment of the utility model Overall structure diagram, Fig. 6 are that the utility model embodiment provides a kind of rearview signal of grenade instrumentation for unmanned plane Figure.First gag lever post 410 and/or the second gag lever post 420, which can be, is rendered as cylindrical metal, rod-shaped stick.First fastening end 411 and second fastening end 412 can be respectively the first gag lever post 410 both ends, third fastening end 421 and the 4th fastening end 422 It can be the both ends of the second gag lever post 420 respectively.

First fastening end 411 of the first gag lever post 410 can be fixedly connected with the first pedestal 124, the first gag lever post 410 The second fastening end 412 be fixedly connected with the second pedestal 125, to make the tube body in the first gag lever post 410 and emission element 100 120 are fixed to each other.The third fastening end 421 of second gag lever post 420 is fixedly connected with the 4th pedestal 127, the second gag lever post 420 The 4th fastening end 422 be fixedly connected with the 4th pedestal 127, to make the tube body in the second gag lever post 420 and emission element 100 120 are fixed to each other.Then the first gag lever post 410 and the second gag lever post 420 is made to be separately fixed at the two sides of tube body 120, by tube body 120 are fixed between the first gag lever post 410 and the second gag lever post 420.

In order to be set in outside and the first elastic parts 430 packet of the first gag lever post 410 to the first elastic parts 430 It includes the first spring and second spring is explained in detail, following two embodiment is now provided and is described in detail respectively:

The first embodiment.It can be arranged with the first spring in the outside of the first gag lever post 410, the first spring can position Between the first fastening end 411 and the first mounting hole 313.One end of first spring can be clamped with the first fastening end 411, i.e., by One end of the first spring is kept out in first fastening end 411, is fixed on one end of the first spring at the first fastening end 411.First The other end of spring can be clamped with the second end 312 for being provided with the first mounting hole 313, i.e., keep out first by second end 312 The other end of spring is fixed on the other end of the first spring at second end 312.Make the both ends of the first spring respectively in this way and First fastening end 411, second end 312 are fixedly connected, when tube body 120 drives the first gag lever post 410 to move along the first mounting hole 313 When dynamic, also drive the first spring that elastic deformation occurs, it is mobile to absorb tube body 120 due to the elastic deformation that the first spring occurs The kinetic energy of generation reduces the generated mechanical energy pair when penetrating object 140 and projecting to reach the operating position of stable tube body 120 The damage of load-supporting part 300, joint unit 200, or influence the normal operating conditions of load-supporting part 300, joint unit 200；Together When, adverse effect when also reducing to unmanned plane stabilized flight or hovering.

Second of embodiment.It can be arranged with second spring in the outside of the first gag lever post 410, second spring can position Between the second fastening end 412 and the first mounting hole 313.One end of second spring can be clamped with the second fastening end 412, i.e., by One end of second spring is kept out in second fastening end 412, is fixed on one end of second spring at the second fastening end 412.Second The other end of spring can be clamped with the second end 312 for being provided with the first mounting hole 313, i.e., keep out second by second end 312 The other end of spring is fixed on the other end of second spring at second end 312.Make the both ends of second spring respectively in this way and Second fastening end 412, second end 312 are fixedly connected, when tube body 120 drives the first gag lever post 410 to move along the first mounting hole 313 When dynamic, also drive second spring that elastic deformation occurs, it is mobile to absorb tube body 120 due to the elastic deformation that second spring occurs The kinetic energy of generation reduces the generated mechanical energy pair when penetrating object 140 and projecting to reach the operating position of stable tube body 120 The damage of load-supporting part 300, joint unit 200, or influence the normal operating conditions of load-supporting part 300, joint unit 200；Together When, adverse effect when also reducing to unmanned plane stabilized flight or hovering.

Continuing with being that a kind of projection for unmanned plane provided by the embodiment of the utility model fills referring to Fig. 1 and Fig. 6, Fig. 1 The overall structure diagram set, Fig. 6 are that the utility model embodiment provides a kind of rearview of grenade instrumentation for unmanned plane Schematic diagram.Include to be set in outside and the second elastic parts 440 of the second gag lever post 420 to the second elastic parts 440 Third spring and the 4th spring are explained in detail, and now provide following two embodiment and are described in detail respectively:

The first embodiment.It can be arranged with third spring in the outside of the second gag lever post 420, third spring can position Between third fastening end 421 and the second mounting hole 323.One end of third spring can be clamped with third fastening end 421, i.e., by One end of third spring is kept out in third fastening end 421, is fixed on one end of third spring at third fastening end 421.Third The other end of spring can be clamped with the 4th end 322 for being provided with the second mounting hole 323, i.e., keep out third by the 4th end 322 The other end of spring is fixed on the other end of third spring at the 4th end 322.Make the both ends of third spring respectively in this way and Third fastening end 421, the 4th end 322 are fixedly connected, when tube body 120 drives the second gag lever post 420 to move along the second mounting hole 323 When dynamic, also drive third spring that elastic deformation occurs, it is mobile to absorb tube body 120 due to the elastic deformation that third spring occurs The kinetic energy of generation reduces the generated mechanical energy pair when penetrating object 140 and projecting to reach the operating position of stable tube body 120 The damage of load-supporting part 300, joint unit 200, or influence the normal operating conditions of load-supporting part 300, joint unit 200；Together When, adverse effect when also reducing to unmanned plane stabilized flight or hovering.

Second of embodiment.It can be arranged with the 4th spring in the outside of the second gag lever post 420, the 4th spring can position Between the 4th fastening end 422 and the second mounting hole 323.One end of 4th spring can be clamped with the 4th fastening end 422, i.e., by One end of the 4th spring is kept out in 4th fastening end 422, is fixed on one end of the 4th spring at the 4th fastening end 422.4th The other end of spring can be clamped with the 4th end 322 for being provided with the second mounting hole 323, i.e., keep out the 4th by the 4th end 322 The other end of spring is fixed on the other end of the 4th spring at the 4th end 322.Make the both ends of the 4th spring respectively in this way and 4th fastening end 422, the 4th end 322 are fixedly connected, when tube body 120 drives the second gag lever post 420 to move along the second mounting hole 323 When dynamic, also drive the 4th spring that elastic deformation occurs, it is mobile to absorb tube body 120 due to the elastic deformation that the 4th spring occurs The kinetic energy of generation reduces the generated mechanical energy pair when penetrating object 140 and projecting to reach the operating position of stable tube body 120 The damage of load-supporting part 300, joint unit 200, or influence the normal operating conditions of load-supporting part 300, joint unit 200；Together When, adverse effect when also reducing to unmanned plane stabilized flight or hovering.

First spring and second spring can all be rendered as cylinder, and the diameter of the first spring can be the straight of second spring Twice of diameter assumes that the diameter of the first spring is P1, the diameter of second spring is P2, then P1=2*P2.Due to the first spring Diameter be twice of diameter of second spring, when recoil pushes the first spring and elastic deformation occurs for second spring, the One spring can be more with respect to second spring absorption recoil energy, then reduce tube body 120 relative to the first mounting hole 313 mobile distances and speed are conducive to the flight for stablizing unmanned plane so that reaching reduces recoil to the impact force of unmanned plane State improves the technical effect of shooting accuracy.

Third spring and the 4th spring can all be rendered as cylinder, and the diameter of third spring can be the straight of the 4th spring The diameter of twice of diameter, i.e. hypothesis third spring is P3, and the diameter of the 4th spring is P4, then P3=2*P4.Due to third spring Diameter be twice of diameter of the 4th spring, when recoil pushes third spring and elastic deformation occurs for the 4th spring, the Three springs can be more with respect to the 4th spring absorption recoil energy, then reduce tube body 120 relative to the second mounting hole 323 mobile distances and speed are conducive to the flight for stablizing unmanned plane so that reaching reduces recoil to the impact force of unmanned plane State improves the technical effect of shooting accuracy.

In practical applications, when fire occurs for high residential building, object 140 to be penetrated can be packed into ejecting end 110 in advance, it will First interface 210 is fixedly connected with the bottom of unmanned aerial vehicle body in joint unit 200.Flight system is passed through by ground handling operator It unites to issue to unmanned plane and instruct, unmanned plane is made to take off to the story height that fire occurs.Then by being arranged in ejecting end 110 The floor external circumstances of fire occur to watch for image pick-up device on three positioning areas 170, when finding the external windows of fiery residence floor, Unmanned plane can be hovered to window.Emitted again by being located at the first laser in ejecting end 110 on first positioning area 150 Device, second laser transmitter on the second positioning area 160 aim at the glass of window, can choose the edge to glass Place is aimed at, such as is aimed at positioned at the junction of glass and wall, lesser shock strength can be used in this way to hit Cullet.If by the spatial position of mobile unmanned plane, so that first laser transmitter and second laser transmitter are targeted to window The glass of mouth then can issue shooting instruction to unmanned plane by ground handling operator.At this point, being located at outside baffle 180 Control switch 132 is closed, since control switch 132 and object to be penetrated 140 connect, then the closure of control switch 132 can excite to It penetrates object 140 and reaches ejecting end 110 along the first trajectory 181 and/or the second trajectory 182 from entering bullet mouth 131, it is high from ejecting end 110 Rapid fire goes out.The glass at window can be smashed by the powerful kinetic energy of object 140 to be penetrated, has then got through and has been located in fire floor room The window that indicator of trapped personnel is connected to the external world, allows indoor indicator of trapped personnel to escape from window；It is also possible that being located at room Outer fire fighter is entered the room from window by equipment such as aerial ladders and is succoured.To reach by unmanned plane with transmitting Component 100, joint unit 200, load-supporting part 300 and damping part 400.Now to emission element 100, joint unit 200, load-bearing Component 300 and the flight of damping part 400 make object to be penetrated at the high residential building door and window that fire occurs, then through control switch 132 140 shattered glass door and windows carry out the technical effect for helping the indicator of trapped personnel in high residential building to escape in time.

It should be noted last that the above specific embodiment is only to illustrate the technical solution of the utility model rather than limits System, although the utility model is described in detail referring to example, those skilled in the art should understand that, it can be right The technical solution of the utility model is modified or replaced equivalently, without departing from the spirit and model of technical solutions of the utility model It encloses, should all cover in the scope of the claims of the utility model.

Claims

1. a kind of docking for unmanned plane emits load carrier, the unmanned plane includes fuselage, which is characterized in that described to be used for The docking of unmanned plane emits load carrier

Emission element, the emission element include:

Ejecting end；

Tube body, the tube body are provided with first side, second side and hollow portion, the first pedestal are provided in the first side With the second pedestal；Third pedestal and the 4th pedestal are provided in the second side；

End is loaded and unloaded, the handling end is provided with into bullet mouth and control switch；

Object to be penetrated, the object to be penetrated are connected with the control switch, the level to be penetrated in it is described enter bullet mouth in；

Wherein, the tube body be located at the handling end and it is described enter bullet mouth between, the hollow portion pass through it is described enter bullet mouth and institute State ejecting end；

Joint unit, the joint unit include:

First interface, first interface and the fuselage are detachably connected；

Ontology, the ontology are fixedly connected with first interface；

Second interface, second interface are fixedly connected with the ontology, are provided with the first card on second interface Joint chair and the second clamping seat；

Wherein, the ontology is between first interface and second interface；The first clamping seat and described Centrosymmetric distribution of the second clamping seat relative to second interface；First interface and second interface It is symmetrical relative to the ontology；

Load-supporting part, the load-supporting part include:

First support arm, first support arm are provided with first end and second end, and the first end and the first clamping seat are fixed It connects, is provided with the first mounting hole in the second end；

Second support arm, second support arm are provided with third end and the 4th end, and the third end and the second clamping seat are fixed Connection；The second mounting hole is provided on 4th end；

Wherein, the first end and the second end are the both ends of first support arm opposition, the third end and described the Four ends are the both ends of the second support arm opposition；First gag lever post passes through first mounting hole, and the second gag lever post passes through Second mounting hole.

2. emitting load carrier for the docking of unmanned plane as described in claim 1, which is characterized in that described to be used for unmanned plane Docking emit load carrier further include:

First laser transmitter；

The ejecting end includes the first positioning area, and the first laser transmitter is fixed on first positioning area.

3. emitting load carrier for the docking of unmanned plane as claimed in claim 2, which is characterized in that described to be used for unmanned plane Docking emit load carrier further include:

Second laser transmitter；

The ejecting end includes the second positioning area, and the second laser transmitter is fixed on second positioning area.

4. emitting load carrier for the docking of unmanned plane as claimed in claim 3, which is characterized in that described to be used for unmanned plane Docking emit load carrier further include:

Image pick-up device；

The ejecting end includes third positioning area, and the image pick-up device is fixed on the third positioning area.

5. emitting load carrier for the docking of unmanned plane as claimed in claim 4, which is characterized in that described to be used for unmanned plane Docking transmitting load carrier include:

First positioning area and second positioning area are symmetrical relative to the third positioning area.

6. emitting load carrier for the docking of unmanned plane as claimed in claim 5, which is characterized in that described to be used for unmanned plane Docking transmitting load carrier include:

The hollow portion is 30 ° -60 ° relative to the angular range on ground.

7. emitting load carrier for the docking of unmanned plane as described in claim 1, which is characterized in that described to be used for unmanned plane Docking transmitting load carrier include:

First interface is engraved structure, and/or, second interface is engraved structure, and/or, the ontology is Engraved structure.