CN209634732U - Unmanned plane throwing device - Google Patents

Unmanned plane throwing device Download PDF

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Publication number
CN209634732U
CN209634732U CN201822007491.9U CN201822007491U CN209634732U CN 209634732 U CN209634732 U CN 209634732U CN 201822007491 U CN201822007491 U CN 201822007491U CN 209634732 U CN209634732 U CN 209634732U
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China
Prior art keywords
unmanned plane
switch arm
throwing device
loading plate
jettisoninging
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CN201822007491.9U
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Chinese (zh)
Inventor
蒋海霞
石翔
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Goertek Robotics Co Ltd
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Goertek Robotics Co Ltd
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Priority to CN201822007491.9U priority Critical patent/CN209634732U/en
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Abstract

The utility model discloses a kind of unmanned plane throwing device, and for object of jettisoninging, the guide wire including jettisoning component and the connection switch arm and the object of jettisoninging with switch arm, the switch arm is obliquely installed.Cooperate the switch arm being obliquely installed using guide wire, realizes accurate, the quick release of object of jettisoninging.

Description

Unmanned plane throwing device
Technical field
The utility model relates to aircraft throwing object in high sky technical fields, and in particular to a kind of unmanned plane throwing device.
Background technique
Current some scenes of fire, the rescue of earthquake field, fire extinguishing etc. is problem, depends on manpower operation in the past, very tired Difficulty, and have limitation, inefficiency.
Therefore, it is necessary to a kind of precisely dispensing, quickly and effectively unmanned plane throwing device be provided, to solve the above problems.
Utility model content
The main purpose of the utility model is to provide a kind of precisely dispensing, quickly and effectively unmanned plane throwing device.
To achieve the above object, the utility model proposes a kind of unmanned plane throwing device, for object of jettisoninging, including The guide wire of jettisoning component and the connection switch arm and the object of jettisoninging with switch arm, the switch arm inclination are set It sets.
Preferably, the unmanned plane throwing device includes the loading plate of connected unmanned plane main body, and the component of jettisoninging includes The component of jettisoninging is fixed on to the fixing seat of the loading plate, the fixing seat have connect the upper surface of the loading plate with And the lower end surface of the connection switch arm, the fixing seat have close to the inner face at the center of the loading plate and far from described The outer end face at the center of loading plate, the lower end surface of the fixing seat tilt obliquely from inside to outside.
Preferably, the switch arm is located at the lower section of the fixing seat, and closes on the inner face setting of the fixing seat.
Preferably, the unmanned plane throwing device includes the cable guiding device for guiding the guide wire trend, and the cable guiding device is in Tubbiness, the conducting wire bottom including being equipped with wire outlet, the conducting wire wall equipped with wiring inlet, and by the conducting wire bottom and the conducting wire The inner cavity that wall surrounds, one of the guide wire are annularly sheathed on the switch arm, and other end enters from the wiring inlet The inner cavity, and jettisoning object described in connection after being pierced by the cable guiding device from the wire outlet.
Preferably, on gravity direction, the switch arm is located at the top of the wire outlet, and the wiring inlet is located at Between the switch arm and the wire outlet.
Preferably, in the junction of the guide wire and the switch arm, angle between the two is acute angle.
Preferably, the geometric center of the cable guiding device is aligned setting, institute with the center of gravity of the object of jettisoninging on gravity direction The conducting wire wall for stating cable guiding device is in gradually taper up shape from top to bottom, and the cable guiding device protrudes out to be formed admittedly from its conducting wire wall to the inner cavity The even loading plate interconnecting piece.
Preferably, the component of jettisoninging includes steering engine, and the steering engine is equipped with the steering engine arm for connecting the switch arm, the rudder Machine drives the switch arm to open or close by the steering engine arm, and the steering engine is additionally provided with mounting portion, to the fixation The lower end surface of seat is connected and fixed.
Preferably, the unmanned plane throwing device further includes camera system, and the camera system includes being installed on described hold Holder camera below support plate and the figure transmission module being installed on above the loading plate.
Preferably, the unmanned plane throwing device includes component and the holder camera of jettisoninging described in three, described Three components of jettisoninging are symmetrically distributed in the lower section of the loading plate with one holder camera with 90 degree of angles.
Cooperate the switch arm being obliquely installed using guide wire, realizes accurate, the quick release of object of jettisoninging.
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 Or attached drawing needed to be used in the description of the prior art is briefly described, it should be apparent that, the accompanying drawings in the following description is only It is some embodiments of the utility model, for those of ordinary skill in the art, in the premise not made the creative labor Under, the structure that can also be shown according to these attached drawings obtains other attached drawings.
Fig. 1 be the utility model unmanned plane throwing device it is standby when structural schematic diagram;
Structural schematic diagram when Fig. 2 is the work of the unmanned plane throwing device of the utility model;
Fig. 3 is the decomposition diagram of the unmanned plane throwing device of the utility model.
The embodiments will be further described with reference to the accompanying drawings for the realization, functional characteristics and advantage of the utility model aim.
Specific embodiment
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 describing, it is clear that described embodiment is only a part of the embodiment of the utility model, rather than all Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are not making creative work premise Under every other embodiment obtained, fall within the protection scope of the utility model.
It is to be appreciated that the directional instruction (such as up, down, left, right, before and after ...) of institute in the utility model embodiment It is only used for explaining in relative positional relationship, the motion conditions etc. under a certain particular pose (as shown in the picture) between each component, such as When the fruit particular pose changes, then directionality instruction also correspondingly changes correspondingly.In the description of the present invention, The meaning of " plurality " is at least two, such as two, three etc., unless otherwise specifically defined.
In the present invention unless specifically defined or limited otherwise, term " connection ", " fixation " etc. should do broad sense reason Solution, for example, " fixation " may be a fixed connection, may be a detachable connection, or integral;It can be mechanical connection, it can also To be electrical connection;It can be directly connected, the connection inside two elements can also be can be indirectly connected through an intermediary Or the interaction relationship of two elements, unless otherwise restricted clearly.It for the ordinary skill in the art, can be with The concrete meaning of above-mentioned term in the present invention is understood as the case may be.
In addition, the description for being such as related to " first ", " second " in the present invention is used for description purposes only, and cannot manage Solution is its relative importance of indication or suggestion or the quantity for implicitly indicating indicated technical characteristic.Define as a result, " the One ", the feature of " second " can explicitly or implicitly include at least one of the features.
As shown in Figure 1, the utility model provides a kind of unmanned plane throwing device 100, for object 6 of jettisoninging, including it is solid Even the loading plate 1 of unmanned plane main body (not shown), the component 2 of jettisoninging that loading plate 1 is respectively fixedly connected, cable guiding device 4, camera system and Connect the guide wire 3 of jettisoning component 2 and object 6 of jettisoninging.Herein, the jettisoning center of gravity of object 6 of definition is in the orthographic projection of horizontal plane The center of loading plate 1, the cable guiding device 4, camera system and component 2 of jettisoninging are arranged around the center.In the horizontal plane, definition is leaned on The direction at the nearly center is " inside ", and the direction far from the center is " outside ".
As shown in Fig. 2, above-mentioned object 6 of jettisoninging includes the string bag 61 and places in one embodiment provided by the utility model Fire extinguishing ball 62 in the string bag 61, that is, unmanned plane throwing device 100 is used to fire extinguishing ball 62 of jettisoninging, and fire extinguishing ball 62 is placed on the string bag Scene of fire is transported to by unmanned plane in 61, fire extinguishing ball 62 is precisely launched after locking fire source point by camera system, thus quickly Efficiently control the intensity of a fire.In the present embodiment, the string bag 61 is basket, and certainly in other embodiments, the string bag 61 can also be by line Rope weaves.
As shown in figure 3, component 2 of jettisoninging includes switch arm 21, to folding and unfolding guide wire 3, when switch arm 21 is opened, guiding Line 3 is released, and when switch arm 21 is closed, guide wire 3 is tightened.Specifically, component 2 of jettisoninging is opened including control switch arm 21 The fixing seat 23 of loading plate 1 is fixed on the steering engine 22 of closing and by component 2 of jettisoninging.
Preferably, loading plate 1 is horizontally disposed, and switch arm 21 is obliquely installed.Jettisoning component 2 switch arm 21 and loading plate 1 In default angle.Specifically, on gravity direction, fixing seat 23 has the upper surface 231 of connection 1 lower surface of loading plate and connects The lower end surface 232 of switch arm 21 is connect, the upper surface 231 of fixing seat 23 is horizontally disposed, and lower end surface 232 is obliquely installed, fixing seat 23 are additionally provided with the inner face 233 and outer end face 234 of connection upper surface 231 and lower end surface 232, and the height of inner face 233 is less than outer End face 234, that is, lower end surface 232 tilts obliquely from inside to outside.At this point, the angle system between upper surface 231 and lower end surface 232 Above-mentioned default angle.The switch arm 21 that compares is horizontally disposed, and the switch arm 21 and loading plate 1 of the utility model are in default angle, The frictional force between guide wire 3 and switch arm 21 is advantageously reduced, switch arm 21 is quickly opened, and then 3 energy of guide wire It is enough rapidly separated switch arm 21, avoids the occurrence of the improper situation that switch arm 21 can not be opened due to being directed to line 3 and holding.
In the present embodiment, switch arm 21 is located at the lower section of fixing seat 23, and the inner face 233 for closing on fixing seat 23 is set It sets.
Specifically, steering engine 22 is equipped with the steering engine arm 221 of connection switch arm 21, and steering engine 22 passes through 221 driving switch of steering engine arm Arm 21 opens or closes.Steering engine 22 is additionally provided with mounting portion 222, is connected and fixed to the lower end surface 232 with fixing seat 23, thus will Component 2 of jettisoninging is fixed on fixing seat 23.
Preferably, unmanned plane throwing device 100 is equipped with multiple components 2 of jettisoninging, and the center around loading plate 1 is equally spaced, That is, center of the component 2 away from loading plate 1 of each jettisoninging is equidistant.
It please join shown in Fig. 1, one of guide wire 3 is set to switch arm 21 in ring set and leads under the action of jettisoninging 6 gravity of object Lead 3 is straightened, at this point, guide wire 3 and switch arm 21 are in first angle, it is preferable that and first angle is acute angle, so set, It is to be conducive to guide wire 3 in order to reduce the frictional force between switch arm 21 and guide wire 3 and be rapidly separated switch arm 21.
Cable guiding device 4 is equipped with wiring inlet 420 and wire outlet (not shown) for guiding the trend of guide wire 3.Specifically Ground, cable guiding device 4 are in tubbiness, have conducting wire bottom 41 and conducting wire wall 42, and the inner cavity 40 surrounded by conducting wire bottom 41 and conducting wire wall 42, Cable guiding device 4 protrudes out the interconnecting piece 43 to form connected loading plate 1 from its conducting wire wall 42 to inner cavity 40, and wiring inlet 420 is located at conducting wire On wall 42, wire outlet is located on conducting wire bottom 41.One connection switch arm 21 of guide wire 3, other end from wiring inlet 420 into After entering 4 inner cavity 40 of cable guiding device, is come out from wire outlet and connect the string bag 61 for placing fire extinguishing ball 62.In the present embodiment, each throwing Throw the corresponding guide wire 3 of component 2.The wiring inlet 420 of corresponding every guide wire 3 is located at identical height, wire outlet also position In identical height, and wire outlet is uniformly distributed relative to the above-mentioned center of gravity for jettisoninging object 6.
Preferably, on gravity direction, the geometric center of the cable guiding device 4 is conllinear with the center of gravity of object 6 of jettisoninging.In gravity side Upwards, the conducting wire wall 42 of cable guiding device 4 gradually tapers up from top to bottom, so set, being conducive to guaranteeing cable guiding device 4 and loading plate 1 While connective stability, space is saved.
Preferably, on gravity direction, switch arm 21 is located at the top of wire outlet, and wiring inlet 420 is located at switch arm Between 21 and wire outlet.
Unmanned plane throwing device 100 provided by the utility model, after 22 control switch arm 21 of steering engine opening, guide wire 3 It can be rapidly separated switch arm 21, to achieve the purpose that precisely dispensing, quick extinguishing.
It please join Fig. 1 to camera system shown in Fig. 3, including being installed on the holder camera 51 of 1 lower section of loading plate and installing The figure transmission module 52 above loading plate 1 obtains the location information of fire source point for shooting image, and the location information is passed through Figure transmission module 52 is sent to control system (not shown).
Above-mentioned control system control unmanned plane hovering controls 22 driving switch arm 21 of steering engine in the surface of fire source point It opens, so that the guide wire 3 of the connection string bag 61 is released, in turn, fire extinguishing ball 62 drops down onto fire source point with the string bag 61, realizes fire extinguishing function Energy.
In the present embodiment, unmanned plane throwing device 100 includes three jettisoning component 2 and a holder cameras 51, with 90 degree Angle is symmetrically distributed in the lower section of loading plate 1.
As shown in Figure 1,3 both ends of guide wire are separately connected the string bag 61 and switch arm when unmanned plane throwing device 100 is standby 21, at this point, the string bag 61 is tightened and is located at the underface of cable guiding device 4.
As shown in Fig. 2, firstly, camera system detects fire source point, controlling nobody when unmanned plane throwing device 100 works Machine hovers over the surface of fire source point, secondly, control steering engine 22 turns on the switch arm 21, guide wire 3 automatically disengages switch arm 21, leads After line device 4, fire extinguishing ball 62 is freely fallen with the string bag 61, finally, fire extinguishing ball 62 falls in the fire source point that camera system observes.
The above is only the preferred embodiments of the utility model, and therefore it does not limit the scope of the patent of the utility model, all Under the design of the utility model, equivalent structure transformation made based on the specification and figures of the utility model, or directly/ Other related technical areas are used in indirectly to be included in the scope of patent protection of the utility model.

Claims (10)

1. a kind of unmanned plane throwing device, for object of jettisoninging, which is characterized in that the unmanned plane throwing device includes having The guide wire of jettisoning component and the connection switch arm and the object of jettisoninging of switch arm, the switch arm are obliquely installed.
2. unmanned plane throwing device as described in claim 1, which is characterized in that the unmanned plane throwing device includes the nothing that is connected The loading plate of man-machine main body, the component of jettisoninging includes the fixing seat that the component of jettisoninging is fixed on to the loading plate, described Fixing seat has the lower end surface of the upper surface for connecting the loading plate and the connection switch arm, and the fixing seat has close The outer end face of the inner face at the center of the loading plate and the center far from the loading plate, the lower end surface of the fixing seat is in It tilts obliquely outward.
3. unmanned plane throwing device as claimed in claim 2, which is characterized in that the switch arm is located under the fixing seat Side, and close on the inner face setting of the fixing seat.
4. unmanned plane throwing device as claimed in claim 2 or claim 3, which is characterized in that the unmanned plane throwing device includes drawing The cable guiding device of the guide wire trend is led, the cable guiding device is in tubbiness, and the conducting wire bottom including being equipped with wire outlet enters equipped with conducting wire The conducting wire wall of mouth, and the inner cavity surrounded by the conducting wire bottom and the conducting wire wall, one of the guide wire are annularly arranged In the switch arm, other end enters the inner cavity from the wiring inlet, and is pierced by the conducting wire from the wire outlet It jettisonings object described in connection after device.
5. unmanned plane throwing device as claimed in claim 4, which is characterized in that on gravity direction, the switch arm is located at The top of the wire outlet, the wiring inlet is between the switch arm and the wire outlet.
6. unmanned plane throwing device as claimed in claim 5, which is characterized in that in the company of the guide wire and the switch arm Place is met, angle between the two is acute angle.
7. unmanned plane throwing device as claimed in claim 6, which is characterized in that the geometric center of the cable guiding device and the throwing The center of gravity for throwing object is aligned setting on gravity direction, and the conducting wire wall of the cable guiding device is in gradually taper up shape from top to bottom, described to lead Line device protrudes out to form the loading plate interconnecting piece that is connected from its conducting wire wall to the inner cavity.
8. unmanned plane throwing device as claimed in claim 7, which is characterized in that the component of jettisoninging includes steering engine, the rudder Machine is equipped with the steering engine arm for connecting the switch arm, and the steering engine drives the switch arm to open or close by the steering engine arm, The steering engine is additionally provided with mounting portion, to be connected and fixed with the lower end surface of the fixing seat.
9. unmanned plane throwing device as claimed in claim 8, which is characterized in that the unmanned plane throwing device further includes camera System, the camera system include the holder camera being installed below the loading plate and are installed on above the loading plate Figure transmission module.
10. unmanned plane throwing device as claimed in claim 9, which is characterized in that the unmanned plane throwing device includes three Jettisoning component and the holder camera, described three components of jettisoninging are with one holder camera with 90 degree of angles pair Claim the lower section for being distributed in the loading plate.
CN201822007491.9U 2018-11-30 2018-11-30 Unmanned plane throwing device Active CN209634732U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201822007491.9U CN209634732U (en) 2018-11-30 2018-11-30 Unmanned plane throwing device

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Application Number Priority Date Filing Date Title
CN201822007491.9U CN209634732U (en) 2018-11-30 2018-11-30 Unmanned plane throwing device

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111025984A (en) * 2019-12-23 2020-04-17 中国科学院光电研究院 Near space ball carries control device that jettisonings
CN115675872A (en) * 2022-11-07 2023-02-03 西北核技术研究所 Unmanned aerial vehicle carries high altitude dust particulate matter ration supply ware

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111025984A (en) * 2019-12-23 2020-04-17 中国科学院光电研究院 Near space ball carries control device that jettisonings
CN115675872A (en) * 2022-11-07 2023-02-03 西北核技术研究所 Unmanned aerial vehicle carries high altitude dust particulate matter ration supply ware
CN115675872B (en) * 2022-11-07 2024-06-07 西北核技术研究所 Unmanned aerial vehicle carries high altitude dust particulate matter quantitative supply ware

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