CN206528615U - The unmanned machine frame of fixed-wing and fixed-wing unmanned plane - Google Patents
The unmanned machine frame of fixed-wing and fixed-wing unmanned plane Download PDFInfo
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- CN206528615U CN206528615U CN201720213995.9U CN201720213995U CN206528615U CN 206528615 U CN206528615 U CN 206528615U CN 201720213995 U CN201720213995 U CN 201720213995U CN 206528615 U CN206528615 U CN 206528615U
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Abstract
The utility model provides a kind of unmanned machine frame of fixed-wing and fixed-wing unmanned plane, it is related to unmanned air vehicle technique field, the unmanned machine frame of fixed-wing, including body bearing frame, the body bearing frame is built in the body of fixed-wing unmanned plane, and structural strength of the structural strength more than the body of the body bearing frame；The wing bracing piece of the body bearing frame and the body is connected.Because fixed-wing unmanned plane is in flying for long time or landing, the link position stress of wing and fuselage is larger, and because causing wing to be easily broken the reason for its material, so the higher body bearing frame of structural strength is fastened on wing bracing piece, for increasing the structural strength of fixed-wing unmanned plane body.
Description
Technical field
The utility model is related to unmanned air vehicle technique field, more particularly, to a kind of unmanned machine frame of fixed-wing and fixed-wing without
It is man-machine.
Background technology
UAV is to be manipulated using radio robot and have autonomous flight ability referred to as " unmanned plane "
Not manned aircraft.Without driving cabin on machine, but the equipment such as flight-control computer, sensoring are installed.Unmanned plane can be divided into
MAV, light-duty unmanned plane, SUAV and large-scale unmanned plane.MAV refers to that empty weight is less than or equal to
7kg, light-duty unmanned plane quality be more than 7kg, SUAV refer to empty weight be less than or equal to 5700kg unmanned plane, it is large-scale nobody
Machine refers to the unmanned plane that empty weight is more than 5700kg.And by flying platform configuration classification, unmanned plane can be divided into again fixed-wing nobody
Machine and rotor wing unmanned aerial vehicle etc..
At present, the body of existing miniature (take-off weight 7kg or following) fixed-wing unmanned plane is mainly used on the market
It is made of the expanded materials such as EPO, fuselage quality is reduced as far as possible, in the case of stand-by electric energy identical, improves fixed-wing unmanned plane
Flight time, so as to more adapt to different aerial missions.
But there is problems with when in use in existing miniature fixed-wing unmanned plane：On the one hand, because miniature fixed-wing
The body of unmanned plane is mainly made of fragility EPO expanded materials, and structural strength is low, in prolonged flight course or high
During the frequent landing of intensity, fatigue fracture easily occurs for fuselage and the fixed-wing of fixed-wing unmanned plane.
Utility model content
The purpose of this utility model is to provide a kind of unmanned machine frame of fixed-wing and fixed-wing unmanned plane, existing to solve
The miniature fixed-wing unmanned plane being made up of EPO expanded materials in prolonged flight course or the frequent landing of high intensity
When, due to impinged upon including contingency the fuselage of fixed-wing unmanned plane under interior external impacts easily deformed upon with wing or
The technical problem of fatigue fracture.
The unmanned machine frame of fixed-wing that the utility model is provided, including body bearing frame, the body bearing frame are built in
In the body of fixed-wing unmanned plane, and structural strength of the structural strength more than the body of the body bearing frame；The machine
The wing bracing piece of body bearing frame and the body is connected.
Further, the body bearing frame includes the first side plate and the second side plate being oppositely arranged, first side plate
Two vertical opposed inner walls with the plate face of the second side plate respectively with the head parallel to unmanned plane to tail direction offset；
Transverse connection is provided between first side plate and the second side plate, the transverse connection is described for preventing
First side plate and/or the second side plate after external force by producing relative motion.
Further, fixing hole is correspondingly arranged on first side plate and the second side plate, for fixing the body
Wing bracing piece.
Further, lightening hole is provided with the body bearing frame, the weight for mitigating the body bearing frame.
The fixed-wing unmanned plane that the utility model is provided, including body and the unmanned machine frame of above-mentioned fixed-wing.
Further, image collecting device, and the fixed-wing unmanned plane are provided with the unmanned machine frame of the fixed-wing
Framework is used for the mirror for avoiding described image harvester with being correspondingly arranged on the first avoidance hole, the first avoidance hole on fuselage
Head, so that described image harvester can be acquired to body outside environment.
Further, the second avoidance hole is correspondingly arranged on the unmanned machine frame of the fixed-wing and fuselage, for avoiding
State the operation interface of image collecting device.
Further, the unmanned machine frame of the fixed-wing includes locating rack, and the locating rack is plugged in body bearing frame,
And described image harvester is placed in locating rack.
Further, set flexible anti-on the lateral wall of the locating rack, or on the inwall of the body bearing frame
Deformation is produced after sliding cushion, the elastic anti-slip cushion stress, after external force is removed, shape is recovered, described fixed for hindering
Position frame is skidded off out of body bearing frame.
Further, the locating rack includes the first placement region and the second placement region, and first placement region is used
In placing video camera, second placement region is used to place camera.
The unmanned machine frame of fixed-wing that the utility model is provided, the structural strength for strengthening fixed-wing unmanned plane, including
Body bearing frame, the body bearing frame is built in the body of fixed-wing unmanned plane, and the structure of the body bearing frame is strong
Degree is more than the structural strength of the body, and the wing bracing piece of the body bearing frame and the body is connected, to wing
Bracing piece carries out secondary reinforcement and fixed.Because fixed-wing unmanned plane is in flying for long time or landing, the connection position of fixed-wing
Put stress larger, and because cause wing to be easily broken the reason for its material, by the higher body of structural strength
Bearing frame is fastened on wing bracing piece, for increasing the structural strength of fixed-wing unmanned plane.
The fixed-wing unmanned plane that the utility model is provided, including body and the unmanned machine frame of above-mentioned fixed-wing, because fixed
Wing unmanned plane is in flying for long time or landing, and the link position stress of fixed-wing is larger, and because the reason for its material
Cause wing to be easily broken, so the higher body bearing frame of structural strength is fastened on wing bracing piece, use
To increase the structural strength of fixed-wing unmanned plane.
Brief description of the drawings
, below will be right in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art
The accompanying drawing used required in embodiment or description of the prior art is briefly described, it should be apparent that, describe below
In accompanying drawing be some embodiments of the present utility model, for those of ordinary skill in the art, do not paying creativeness
On the premise of work, other accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 for the body bearing frame of the unmanned machine frame of fixed-wing that the utility model embodiment is provided schematic diagram；
Fig. 2 is the internal structure schematic diagram for the fixed-wing unmanned plane that the utility model embodiment 1 is provided；
Fig. 3 is the schematic diagram of the locating rack for the fixed-wing unmanned plane that the utility model embodiment 2 is provided；
Before Fig. 4 is body bearing frame in the fixed-wing unmanned plane of the offer of the utility model embodiment 2 and locating rack grafting
Schematic diagram；
After Fig. 5 is body bearing frame in the fixed-wing unmanned plane of the offer of the utility model embodiment 2 and locating rack grafting
Schematic diagram；
After Fig. 6 is body bearing frame in the fixed-wing unmanned plane of the offer of the utility model embodiment 2 and locating rack grafting
Upward view.
Icon：100- body bearing frames；The side plates of 110- first；111- fixing holes；112- lightening holes；The side plates of 120- second；
130- connectors；131- bottom plates；200- wing bracing pieces；300- bodies；400- first avoids hole；500- second avoids hole；
600- locating racks；610- elastic anti-slip cushions；The placement regions of 620- first；The placement regions of 630- second.
Embodiment
The technical solution of the utility model is clearly and completely described below in conjunction with accompanying drawing, it is clear that described
Embodiment is a part of embodiment of the utility model, rather than whole embodiments.Based on the embodiment in the utility model, sheet
The every other embodiment that field those of ordinary skill is obtained under the premise of creative work is not made, belongs to this practicality
Novel protected scope.
, it is necessary to explanation in description of the present utility model, term " " center ", " on ", " under ", it is "left", "right", " perpendicular
Directly ", the orientation or position relationship of the instruction such as " level ", " interior ", " outer " are, based on orientation shown in the drawings or position relationship, to be only
Described for the ease of description the utility model and simplifying, rather than to indicate or imply that signified device or element must have specific
Orientation, with specific azimuth configuration and operation, therefore it is not intended that to limitation of the present utility model.In addition, term " the
One ", " second ", " the 3rd " are only used for describing purpose, and it is not intended that indicating or implying relative importance.
The unmanned machine frame of fixed-wing that the utility model is provided, the structural strength for strengthening fixed-wing unmanned plane, including
Body bearing frame 100, the body bearing frame 100 is built in the body of fixed-wing unmanned plane, and the body bearing frame 100
Structural strength be more than the fixed-wing unmanned plane body structural strength.The machine of the body bearing frame 100 and the body
Wing bracing piece 200 is connected, and secondary reinforcement is carried out to wing bracing piece 200 and is fixed.Because fixed-wing unmanned plane is for a long time
Flight or when landing, the link position stress of fixed-wing is larger, and because causes wing easily to occur the reason for its material
Fracture, so the higher body bearing frame 100 of structural strength is fastened on wing bracing piece 200, for increasing fixation
The structural strength of wing unmanned plane, so as to reach the technique effect of extension fixed-wing unmanned plane service life.
As shown in figure 1, body bearing frame 100 can be used for increasing the anti-collision performance of the fuselage of fixed-wing unmanned plane, institute
State the first side plate 110 and the second side plate 120 that body bearing frame 100 includes being oppositely arranged, the side of the first side plate 110 and second
The plate face of plate 120 offsets with two vertical opposed inner walls of the head parallel to fixed-wing unmanned plane to tail direction respectively,
It is exactly the side wall of left and right two of body, so that above-mentioned internal body be supported.The side plate 120 of first side plate 110 and second
Between be provided with connector 130, the connector 130 be used to preventing the side plate 120 of the first side plate 110 and/or second by
Relative motion is produced after external force, the stability of body bearing frame 100 is kept, and then adds the knot of the body of fixed-wing unmanned plane
Structure intensity.When fixed-wing unmanned plane flying for long time or it is born after, the outer wall of body can by ecto-entad external force, and by
The first side plate 110 and the second side plate 120 that connector 130 is connected prop up relative two inwalls of fixed-wing unmanned plane body, from
And prevent that two inwalls of above-mentioned body from occurring the structural damage of ecto-entad, has reached the use for adding fixed-wing unmanned plane
Long lifespan technique effect.
The connector 130 can include bottom plate 131, and the bottom plate 131 is arranged on the side of the first side plate 110 and second
The bottom of plate 120, and offseted with the bottom surface of the body of fixed-wing unmanned plane, the structure for increasing body bottom surface is strong
Degree, is prevented during landing, and the external force of ecto-entad is by the structural damage of body.
Explanation is needed, body bearing frame 100 not only has the effect for strengthening fixed-wing unmanned plane housing construction intensity, also
It can play a part of that protection is fixed to the task device inside fixed-wing unmanned plane.By the task in fixed-wing unmanned plane
Equipment is fixed on inside body bearing frame 100, when accident, which occurs, for fixed-wing unmanned plane falls, though body is damaged, but
Be because the structural strength of body bearing frame 100 is higher, be arranged at its internal task device can by certain protection,
Damaged condition is preferably minimized, or even can not be damaged, so that task device can be used again.
Fixing hole 111 is correspondingly arranged on the side plate 120 of first side plate 110 and second, the wing of the body is strengthened
Bar 200 passes through fixing hole 111, so that wing bracing piece 200 has been carried out secondary fixation by the body bearing frame 100, so as to increase
The fixing for having added wing to be connected with body.Because the material of existing miniature fixed-wing unmanned plane is EPO expanded materials, wing
Bracing piece 200 is directly connected with fuselage, cause fixed-wing and fuselage link position be very easy to be broken, fixed-wing without
Man-machine fixed-wing fractures.And utilize the structural strength body bearing frame 100 pair bigger than fixed-wing unmanned aerial vehicle body structural strength
Fixed-wing carries out secondary fixation, can effectively prevent the phenomenon of the disconnected wing from occurring.
Preferably, the material of the body bearing frame 100 can be wooden, and wood materials structural strength is than EPO foaming material
Material is high, and proportion is lighter than metal, and is easily worked out variously-shaped, the inner-cavity structure better adaptability with fixed-wing unmanned plane, together
When, it is also more environmentally friendly.
Lightening hole 112 is provided with the body bearing frame 100, the weight for mitigating the body bearing frame 100.It is micro-
The quality of type fixed-wing unmanned plane is less than or equal to 7kg, and fuselage quality is reduced as far as possible, in the case of stand-by electric energy identical, improves
The flight time of fixed-wing unmanned plane, so as to more adapt to different aerial missions.So solid in extra increase in order to ensure
In the case of determining the unmanned machine frame of the wing, the weight of fixed-wing unmanned plane is also not too large, so setting on body bearing frame 100
Put multiple lightening holes 112.
Explanation is needed, by setting lightening hole 112 can be so that body bearing frame 100 is when being hit, Neng Gou
Certain deformation is produced in default scope, absorbed by the overall deformation of body bearing frame 100 its on some point by
The impulsive force arrived.Meanwhile, and original EPO expanded materials fuselage bonding mutual cooperation later, so as to obtain preferably overall anti-
Impact capacity, after aircraft generation accident, can at utmost reduce to the greatest extent the damaged condition of fixed-wing unmanned plane.So in body
Lightening hole 112 is provided with bearing frame 100, the weight for mitigating fixed-wing unmanned plane on the basis of increase body bulk strength is reached
Amount.
Preferably, on body bearing frame 100 is ensured on the premise of each lateral plate structure intensity, set circular or oval
The lightening hole 112 of shape is, it is necessary to note avoiding the position of main stress.So as to reach on the premise of structural strength is ensured, reduce
The technique effect of the weight of body bearing frame 100.
The utility model provides a kind of fixed-wing unmanned plane, is given below what two embodiments were provided the utility model
The structure of fixed-wing unmanned plane is described in detail.
Embodiment 1
As shown in Fig. 2 the fixed-wing unmanned plane that the utility model is provided, including body 300 and above-mentioned fixed-wing unmanned plane
Framework, the unmanned machine frame of fixed-wing, the structural strength for strengthening fixed-wing unmanned plane, including body bearing frame 100, the machine
Body bearing frame 100 is built in the body 300 of fixed-wing unmanned plane, and the structural strength of the body bearing frame 100 is more than institute
The structural strength of body 300 is stated, the wing bracing piece 200 of the body bearing frame 100 and the body 300 is connected, right
Wing bracing piece 200 carries out secondary reinforcement and fixed.Because fixed-wing unmanned plane is in flying for long time or landing, fixed-wing
Link position stress is larger, and because causing wing to be easily broken the reason for its material, structural strength is higher
Body bearing frame 100 be fastened on wing bracing piece 200, for increasing the structural strength of fixed-wing unmanned plane.
Mucigel can be increased between the outer wall of the fuselage inwall and body bearing frame 100, such as by glue by machine
Together with body inwall is sticky in the outer wall of body bearing frame 100, so as to increase the stability of fixed-wing unmanned plane, prevent in flight
During, body bearing frame 100 is subjected to displacement relative to fuselage, causes the unbalance of fixed-wing unmanned plane, and flight occurs
Shaking phenomenon.
Preferably, image collecting device is provided with the unmanned machine frame of the fixed-wing, so as to so that the utility model
The fixed-wing unmanned plane of offer is acquired during flight to scene on the way.The unmanned machine frame of fixed-wing with
The first avoidance hole 400 is correspondingly arranged on fuselage, the first avoidance hole 400 is used for the mirror for avoiding described image harvester
Head, so that described image harvester can be acquired to the outside environment of body 300.
Preferably, the first avoidance hole 400 can be arranged on the bottom surface of the fixed-wing unmanned plane, so when solid
When determining wing unmanned plane horizontal flight, what image collecting device can collect scenery on ground just takes the photograph image, to investigation, exploration,
The work such as positioning have great help.
Further, the second avoidance hole 500 is correspondingly arranged on the unmanned machine frame of the fixed-wing and fuselage, for avoiding
The operation interface of described image harvester.So before take off, operator can not take fixed-wing unmanned aerial vehicle body apart
In the case of, the function to image collecting device is set, very convenient.
Preferably, the second avoidance aperture position of hole 500 of the fuselage is provided with flap shutter, and the flap shutter is closed
Afterwards, hole 500 is avoided for blocking described second.
Embodiment 2
The fixed-wing unmanned plane that the utility model is provided, including body 300 and the unmanned machine frame of above-mentioned fixed-wing, fixed-wing
Unmanned machine frame, the structural strength for strengthening fixed-wing unmanned plane, including body bearing frame 100, the body bearing frame 100
It is built in the body 300 of fixed-wing unmanned plane, and the structural strength of the body bearing frame 100 is more than the body 300
Structural strength, the wing bracing piece 200 of the body bearing frame 100 and the body 300 is connected, to wing bracing piece
200, which carry out secondary reinforcement, fixes.Because fixed-wing unmanned plane is in flying for long time or landing, the link position of fixed-wing by
Power is larger, and because causes wing to be easily broken the reason for its material, by the higher body load-bearing of structural strength
Frame 100 is fastened on wing bracing piece 200, for increasing the structural strength of fixed-wing unmanned plane.
As in Figure 3-5, difference from Example 1 is, the unmanned machine frame of fixed-wing includes locating rack 600,
The locating rack 600 is plugged in body bearing frame 100, and described image harvester is placed in locating rack 600.The machine
Body bearing frame 100 is reserved with grafting region, and the width in the grafting region is more than the width of the locating rack 600, so that described
Locating rack 600 can be plugged in the grafting region of body bearing frame 100.Because body bearing frame 100 needs to strengthen with wing
Bar 200 is connected, so it is not easy to separate with fuselage, and the locating rack 600 being plugged in body bearing frame 100 can be light
Being removed from body bearing frame 100 for pine, it is more convenient that image collecting device is installed and adjusted.
Specifically, the locating rack 600 can be used for fixing a variety of image collecting devices, such as photograph of various different models
Camera, video camera or other work in the task devices such as the remote sensing harvester of non-visible because locating rack 600 and machine
Body bearing frame 100 be by socket connection together, so removing and installing very easy.By taking image collecting device as an example,
Since it is desired that according to different aerial mission demands, the image collecting device of selection is also different, it is possible in advance by a variety of figures
As harvester is separately fixed in multiple locating racks 600, by changing locating rack 600, realize to fixed-wing unmanned plane image
The replacing of harvester, whole process is simple, convenient, fast.By the cooperation of body bearing frame 100 and locating rack 600, realize
The technique effect quickly removed and installed to fixed-wing unmanned plane internal task equipment.
Image collecting device is seated in locating rack 600, the convenient effect of replacing can be not only played, can also be effectively
Protection image collecting device, the material of locating rack 600 can be identical with the material of body bearing frame 100, and their structure is strong
Degree is higher than the intensity of body 300, can increase considerably the security of image collecting device, runs into the fortuitous events such as crash, can
Effectively improve the survival probability of image collecting device.
Preferably, bullet is provided with the lateral wall of the locating rack 600, or on the inwall of the body bearing frame 100
Property anti-skidding cushion 610, produce deformation after the stress of elastic anti-slip cushion 610, after external force is removed, shape is recovered.With institute
It is provided with exemplified by elastic anti-slip cushion 610, is held when locating rack 600 is inserted into body on the inwall for stating body bearing frame 100
When in weight frame 100, the thickness of elastic anti-slip cushion 610 is compressed, and after locating rack 600 is fully-inserted, elasticity is anti-
Sliding cushion 610 sufficiently occupies the lateral wall of locating rack 600 to the space between the inwall of body bearing frame 100, so that
The frictional force between elastic anti-slip cushion 610 and the outer wall of locating rack 600 is added, so that reaching prevents locating rack 600 from skidding off
The technique effect of body bearing frame 100.
Inside from the inlet port of locating rack 600 to the body bearing frame 100, the elastic anti-slip cushion 610
Thickness gradually increases, so as to facilitate the insertion of locating rack 600.
Preferably, the cross section of the elastic anti-slip cushion 610 is triangle.Locating rack 600 is entering body load-bearing
During frame 100, the resistance for most starting to be subject to is minimum, and the resistance being then subject to is increasing, so as to reach the technology effect of convenient insertion
Really.
The material of the elastic anti-slip cushion 610 can be EVA foams or rubber.Slip layer prevents positioning except playing
Frame 600 is skidded off outside the technique effect of body bearing frame 100, and cushioning effect is also played to collision therebetween.Preferably, institute
Stating anti-skidding cushion can be arranged on five outer surfaces of locating rack 600, after body 300 is collided, by impact force according to
It is secondary to be forwarded to body bearing frame 100 and locating rack 600, and because being arranged on locating rack 600 and the support of body bearing frame 100
The cushioning effect of EVA foams or rubber, the impact force that locating rack 600 is subject to relative can be reduced, so as to increase considerably image
The security of harvester, effectively improves the survival probability of image collecting device.
The locating rack 600 includes the first placement region 620 and the second placement region 630, first placement region 620
For placing video camera, second placement region 630 is used to place camera.So as to reach, fixed-wing unmanned plane is same
When technique effect that environment on the way is taken pictures and recorded a video.
As shown in fig. 6, being correspondingly arranged on the first avoidance hole 400 on the bottom surface of locating rack 600 and body bearing frame 100
Hole 500 is avoided with second.
To sum up state institute, the fixed-wing unmanned plane that the utility model is provided, including body 300 and the unmanned machine frame of above-mentioned fixed-wing
Frame, the unmanned machine frame of fixed-wing, the structural strength for strengthening fixed-wing unmanned plane, including body bearing frame 100, the body
Bearing frame 100 is built in the body 300 of fixed-wing unmanned plane, and the body bearing frame 100 structural strength be more than it is described
The structural strength of body 300, the wing bracing piece 200 of the body bearing frame 100 and the body 300 is connected, to machine
Wing bracing piece 200 carries out secondary reinforcement and fixed.Because fixed-wing unmanned plane is in flying for long time or landing, the company of fixed-wing
Connect position stress larger, and because causing wing to be easily broken the reason for its material, structural strength is higher
Body bearing frame 100 is fastened on wing bracing piece 200, for increasing the structural strength of fixed-wing unmanned plane.It is described solid
Determining wing unmanned plane includes image collecting device, and described image harvester can be fit directly on body bearing frame 100, also may be used
To add a locating rack 600, locating rack 600 and the grafting of body bearing frame 100 are allowed, image collecting device is fixed on positioning
On frame 600, so as to realize the technique effect that image collecting device is conveniently removed.
Finally it should be noted that：Various embodiments above is only limited to illustrate the technical solution of the utility model, rather than to it
System；Although the utility model is described in detail with reference to foregoing embodiments, one of ordinary skill in the art should
Understand：It can still modify to the technical scheme described in foregoing embodiments, or to which part or whole
Technical characteristic carries out equivalent substitution；And these modifications or replacement, the essence of appropriate technical solution is departed from this practicality newly
The scope of each embodiment technical scheme of type.
Claims (10)
1. a kind of unmanned machine frame of fixed-wing, it is characterised in that including body bearing frame, the body bearing frame is built in fixation
In the body of wing unmanned plane, and structural strength of the structural strength more than the body of the body bearing frame；The body is held
The wing bracing piece of weight frame and the body is connected.
2. the unmanned machine frame of fixed-wing according to claim 1, it is characterised in that the body bearing frame includes relative set
The first side plate and the second side plate put, the plate face of first side plate and the second side plate respectively with parallel to fixed-wing unmanned plane
Head offsets to two vertical opposed inner walls in tail direction；
Transverse connection is provided between first side plate and the second side plate, the transverse connection is used to prevent described first
Side plate and/or the second side plate after external force by producing relative motion.
3. the unmanned machine frame of fixed-wing according to claim 2, it is characterised in that on first side plate and the second side plate
Fixing hole is correspondingly arranged on, the wing bracing piece for fixing the body.
4. the unmanned machine frame of fixed-wing according to claim 1, it is characterised in that be provided with and subtract on the body bearing frame
Repeated hole, the weight for mitigating the body bearing frame.
5. a kind of fixed-wing unmanned plane, it is characterised in that including the fixed-wing described in body and claim 1-4 any one without
People's machine frame.
6. fixed-wing unmanned plane according to claim 5, it is characterised in that be provided with the unmanned machine frame of fixed-wing
Image collecting device, and the unmanned machine frame of the fixed-wing, with being correspondingly arranged on the first avoidance hole on fuselage, described first avoids
Hole is used for the camera lens for avoiding described image harvester, so that described image harvester can be adopted to body outside environment
Collection.
7. fixed-wing unmanned plane according to claim 6, it is characterised in that on the unmanned machine frame of fixed-wing and fuselage
The second avoidance hole is correspondingly arranged on, the operation interface for avoiding described image harvester.
8. fixed-wing unmanned plane according to claim 6, it is characterised in that the unmanned machine frame of fixed-wing includes positioning
Frame, the locating rack is plugged in body bearing frame, and described image harvester is placed in locating rack.
9. fixed-wing unmanned plane according to claim 8, it is characterised in that on the lateral wall of the locating rack, Huo Zhesuo
Deformation is produced after elastic anti-slip cushion, the elastic anti-slip cushion stress are provided with the inwall for stating body bearing frame, outside
After power is removed, shape is recovered, for hindering the locating rack to be skidded off out of body bearing frame.
10. fixed-wing unmanned plane according to claim 8, it is characterised in that the locating rack includes the first placement region
With the second placement region, first placement region is used to place video camera, and second placement region is used to place camera.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720213995.9U CN206528615U (en) | 2017-03-07 | 2017-03-07 | The unmanned machine frame of fixed-wing and fixed-wing unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720213995.9U CN206528615U (en) | 2017-03-07 | 2017-03-07 | The unmanned machine frame of fixed-wing and fixed-wing unmanned plane |
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| Publication Number | Publication Date |
|---|---|
| CN206528615U true CN206528615U (en) | 2017-09-29 |
Family
ID=59918732
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720213995.9U Expired - Fee Related CN206528615U (en) | 2017-03-07 | 2017-03-07 | The unmanned machine frame of fixed-wing and fixed-wing unmanned plane |
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| Country | Link |
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| CN (1) | CN206528615U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106628106A (en) * | 2017-03-07 | 2017-05-10 | 厦门南羽科技有限公司 | Fixed wing unmanned aerial vehicle framework and fixed wing unmanned aerial vehicle |
-
2017
- 2017-03-07 CN CN201720213995.9U patent/CN206528615U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106628106A (en) * | 2017-03-07 | 2017-05-10 | 厦门南羽科技有限公司 | Fixed wing unmanned aerial vehicle framework and fixed wing unmanned aerial vehicle |
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Granted publication date: 20170929 |