CN207328813U - Foot stool and unmanned plane - Google Patents
Foot stool and unmanned plane Download PDFInfo
- Publication number
- CN207328813U CN207328813U CN201720946491.8U CN201720946491U CN207328813U CN 207328813 U CN207328813 U CN 207328813U CN 201720946491 U CN201720946491 U CN 201720946491U CN 207328813 U CN207328813 U CN 207328813U
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- CN
- China
- Prior art keywords
- foot stool
- fuselage
- support structure
- fastener
- supporter
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/04—Arrangement or disposition on aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Orthopedics, Nursing, And Contraception (AREA)
- Toys (AREA)
- Accessories Of Cameras (AREA)
Abstract
The utility model discloses a kind of foot stool and unmanned plane.Foot stool is used for unmanned plane, and the unmanned plane includes fuselage and connects the fuselage foot stool of the fuselage, and the foot stool includes being used for the fastener being detachably connected with the fuselage foot stool.The foot stool of the utility model embodiment, when unmanned plane runs into miriness, shallow water hole, meadow, snowfield when it is poor take off environment when, increase the fulcrum height of fuselage foot stool, so as to increase the distance of fuselage from the ground, help to make unmanned plane work normally under poor environment.
Description
Technical field
It the utility model is related to vehicle technology field, more particularly to a kind of foot stool and unmanned plane.
Background technology
In correlation technique, the foot stool of unmanned plane is highly usually what cannot be adjusted, and when running into miriness, shallow water hole, meadow, is avenged
Ground when it is poor take off environment when, the height of foot stool is unable to meet demand, influences the normal work of unmanned plane.
Utility model content
The utility model embodiment provides a kind of foot stool and unmanned plane.
A kind of foot stool of the utility model embodiment, for unmanned plane, the unmanned plane is included described in fuselage and connection
The fuselage foot stool of fuselage, the foot stool are used to connect the fuselage foot stool and including for being detachably connected with the fuselage foot stool
Fastener, the foot stool includes supporter and auxiliary support structure, and the fastener is arranged on the supporter or the auxiliary branch
Support structure.
Above-mentioned foot stool, when unmanned plane runs into miriness, shallow water hole, meadow, snowfield when it is poor take off environment when, increase fuselage foot
The fulcrum height of frame, so as to increase the distance of fuselage from the ground, helps to make unmanned plane work normally under poor environment.
In some embodiments, the foot stool be equipped with for the spacing fuselage foot stool holding part, the fastener with
The fuselage foot stool fastens, to prevent the fuselage foot stool from deviating from out of described holding part.
In some embodiments, the fastener is elastic fastener.
In some embodiments, the auxiliary support structure is connected to the side of the supporter, the support bodily form
Into there is the fastener.
In some embodiments, the auxiliary support structure is hollow and offer upward opening.
In some embodiments, the fastener is arranged on the upper end of the supporter.
In some embodiments, the supporter is hollow and offers upward opening, the supporter and institute
State auxiliary support structure hollow space and be collectively forming the holding part.
In some embodiments, the auxiliary support structure is connected to the upper end of the supporter, the Auxiliary support
Structure is formed with the fastener.
In some embodiments, the auxiliary support structure includes guidance part, and the fastener is arranged on the guidance part
Both sides, the guide portion be used for carry the fuselage foot stool.
In some embodiments, the fastener includes limiting section, and the limiting section is arranged at intervals with the guidance part, institute
State and form institute formed with the limit space for fuselage foot stool insertion, the limit space between limiting section and the guidance part
State holding part.
In some embodiments, the supporter offers lightening hole.
A kind of unmanned plane of the utility model embodiment includes：
Fuselage；
Fuselage foot stool, the fuselage foot stool are connected to the fuselage；
Foot stool, the foot stool are used to connect the fuselage foot stool and including fastener, and the fastener and the fuselage foot stool can
Releasably connect；The foot stool further includes supporter and auxiliary support structure, and the fastener is arranged on the supporter or described
Auxiliary support structure.
Above-mentioned unmanned plane, when unmanned plane runs into miriness, shallow water hole, meadow, snowfield when it is poor take off environment when, foot stool connection
In the fulcrum height that can increase fuselage foot stool to end of fuselage foot stool, so as to increase the distance of fuselage from the ground, help to make nothing
It is man-machine to be worked normally under poor environment.
In some embodiments, the foot stool includes the first foot stool, and first foot stool includes the supporter and institute
Auxiliary support structure is stated, the auxiliary support structure is connected to the side of the supporter, and the supporter is formed with the button
Part, the fuselage foot stool include the first fuselage foot stool, and the first fuselage foot stool forms connecting platform, and the fastener is used to fasten
In the connecting platform.
In some embodiments, the auxiliary support structure is hollow and offer upward opening described first
Fuselage foot stool includes connector and ruggedized construction, and the connector is connected to formed with the connecting platform, the ruggedized construction
The side of the connector, the ruggedized construction are used to be at least partially inserted into the auxiliary support structure from the opening and hold
It is loaded in the auxiliary support structure.
In some embodiments, the fastener is arranged on the upper end of the supporter, the auxiliary support structure connection
In the upper side of the supporter, the connecting platform is arranged on the ruggedized construction and the side of the junction of the connector
Side.
In some embodiments, the supporter is hollow and offers upward opening, and the connector is used for
The supporter is at least partially inserted into from the opening.
In some embodiments, the foot stool includes the second foot stool, and second foot stool includes the supporter and institute
State auxiliary support structure, the auxiliary support structure is connected to the upper end of the supporter, the auxiliary support structure formed with
The fastener, the upper end of the auxiliary support structure offer opening, and the fuselage foot stool includes the second fuselage foot stool, and described
Two fuselage foot stools are at least partially inserted into the auxiliary support structure from the opening, and the fastener is used to be fastened on described second
Fuselage foot stool.
In some embodiments, the auxiliary support structure includes guidance part, and the fastener is arranged on the guidance part
Both sides, the second fuselage foot stool includes support column and bracing piece, and the bracing piece is used to tilt relative to the support column
The side of the support column is connected to, the bracing piece is used to be carried on the guidance part and is fastened on the fastener.
In some embodiments, the fastener includes limiting section, and the limiting section is arranged at intervals with the guidance part, institute
State formed with limit space between limiting section and the guidance part, the bracing piece is used to be fastened in the limit space.
The additional aspect and advantage of the utility model embodiment will be set forth in part in the description, partly will be under
Become obvious in the description in face, or recognized by the practice of the utility model.
Brief description of the drawings
In description of the above-mentioned and/or additional aspect and advantage of the utility model from combination accompanying drawings below to embodiment
It will be apparent and be readily appreciated that, wherein：
Fig. 1 is the schematic perspective view of the foot stool of the utility model embodiment；
Fig. 2 is another schematic perspective view of the foot stool of the utility model embodiment；
Fig. 3 is the another schematic perspective view of the foot stool of the utility model embodiment；
Fig. 4 is the part-structure decomposition diagram of the unmanned plane of the utility model embodiment；
Fig. 5 is the part-structure schematic perspective view of the unmanned plane of the utility model embodiment；
Fig. 6 is another decomposition diagram of part-structure of the unmanned plane of the utility model embodiment；
Fig. 7 is another schematic perspective view of part-structure of the unmanned plane of the utility model embodiment；
Fig. 8 is the schematic perspective view of the unmanned plane of the utility model embodiment.
Main element symbol description：
Unmanned plane 100, foot stool 10, holding part 101, fastener 11, limiting section 112,
First foot stool 12, supporter 122, side 1221, opening 1222, plug division 1224, supporting part 1226, through hole
1226a, auxiliary support structure 124, opening 1242, top surface 1244, inclined-plane 1246, side 1248,
Second foot stool 14, supporter 142, lateral surface 1421, lightening hole 1422, auxiliary support structure 144, guidance part
1442, limit space 1443, top surface 1444, be open 1444a, side 1446, sidepiece 1448,
Fuselage foot stool 20, the first fuselage foot stool 22, connecting platform 222, connector 224, side 2241, ruggedized construction 226,
Second fuselage foot stool 24, support column 242, bracing piece 244,
Fuselage 30.
Embodiment
The embodiment of the utility model is described below in detail, the example of the embodiment is shown in the drawings, wherein
Same or similar label represents same or similar element or has the function of same or like element from beginning to end.Lead to below
Cross the embodiment being described with reference to the drawings to be exemplary, be only used for explaining the utility model, and it is not intended that to this practicality
New limitation.
In the description of the utility model, it is to be understood that term " " center ", " longitudinal direction ", " transverse direction ", " length ",
" width ", " thickness ", " on ", " under ", "front", "rear", "left", "right", " vertical ", " level ", " top ", " bottom ", " interior ",
The orientation or position relationship of the instruction such as " outer ", " clockwise ", " counterclockwise " are based on orientation shown in the drawings or position relationship, only
It is to be described for the ease of description the utility model with simplified, rather than indicates or imply that the device of meaning or element must be with spies
Fixed orientation, with specific azimuth configuration and operation, therefore it is not intended that limitation to the utility model.In addition, term " the
One ", " second " is only used for description purpose, and it is not intended that instruction or imply relative importance or it is implicit indicate it is indicated
The quantity of technical characteristic.Thus, " first " is defined, the feature of " second " can be expressed and either implicitly include one or more
Multiple features.In the description of the utility model, " multiple " are meant that two or more, unless otherwise clearly having
The restriction of body.
, it is necessary to which explanation, unless otherwise clearly defined and limited, term " are pacified in the description of the utility model
Dress ", " connected ", " connection " should be interpreted broadly, for example, it may be fixedly connected or be detachably connected, or integratedly
Connection；Can mechanically connect or be electrically connected or can mutually communicate；It can be directly connected, can also be in
Between medium be indirectly connected, can be the interaction relationship of connection inside two elements or two elements.For this area
For those of ordinary skill, concrete meaning of the above-mentioned term in the utility model can be understood as the case may be.
In the description of the utility model, unless otherwise clearly defined and limited, fisrt feature second feature it
" on " or it " under " can directly be contacted including the first and second features, it is not directly to connect that can also include the first and second features
Touch but pass through the other characterisation contact between them.Moreover, fisrt feature second feature " on ", " top " and " on
Face " includes fisrt feature directly over second feature and oblique upper, or to be merely representative of fisrt feature level height special higher than second
Sign.Fisrt feature second feature " under ", " lower section " and " below " include fisrt feature immediately below second feature and obliquely downward
Side, or be merely representative of fisrt feature level height and be less than second feature.
Following disclosure provides many different embodiments or example is used for realizing the different structure of the utility model.
In order to simplify the disclosure of the utility model, hereinafter the component and setting of specific examples are described.Certainly, they are only
Example, and purpose does not lie in limitation the utility model.In addition, the utility model can in different examples repeat reference numerals
And/or reference letter, this repetition are for purposes of simplicity and clarity, itself not indicate discussed various embodiments
And/or the relation between setting.In addition, various specific techniques and the example of material that the utility model provides, but this
Field those of ordinary skill can be appreciated that the application of other techniques and/or the use of other materials.
Please refer to Fig.1 and Fig. 8, a kind of foot stool 10 of the utility model embodiment, for unmanned plane 100, unmanned plane 100
Fuselage foot stool 20 including fuselage 30 and connection fuselage 30, foot stool 10 include being used for the fastener being detachably connected with fuselage foot stool 20
11。
Above-mentioned foot stool 10, when unmanned plane 100 runs into miriness, shallow water hole, meadow, snowfield when it is poor take off environment when, increase
The fulcrum height of fuselage foot stool 20, so as to increase the distance of fuselage 30 from the ground, helps to make unmanned plane 100 in poor environment
Lower normal work.
The lower section of fuselage 30 of unmanned plane 100 is provided with the structures such as holder, and when running into miriness, shallow water is cheated, meadow, the field such as snowfield
Jing Shi, fuselage foot stool are easily trapped into muddy, shallow water hole, meadow or snowfield, cause to be arranged on holder below fuselage etc. other
Structure, which easily collides ground or is also absorbed in muddy, shallow water hole, meadow or snowfield, causes structural failure.Therefore, this practicality is new
The foot stool 10 of type embodiment can run into miriness, shallow water hole in unmanned plane 100, and meadow, snowfield is installed to fuselage when scene
20 lower end of foot stool, the fulcrum height of increase fuselage foot stool 20, for other structures such as holder of the protection setting below fuselage 30,
It is easy to use and dismounting is simple.
In some embodiments, foot stool 10 is equipped with the holding part 101 for spacing fuselage foot stool 20, fastener 11 and fuselage
Foot stool 20 fastens, to prevent the abjection out of holding part 101 of fuselage foot stool 20.
In this way, the connection between foot stool 10 and fuselage foot stool 20 is set more to stablize.
In some embodiments, fastener 11 is elastic fastener 11.
In this way, fastener 11 can preferably snap into fuselage foot stool 20 so that the connection of foot stool 10 and fuselage foot stool 20 is more
Add stabilization.
In some embodiments, incorporated by reference to Fig. 1, foot stool 10 includes supporter 122 and auxiliary support structure 124, auxiliary
Supporting structure 124 is connected to the side 1221 of supporter 122, and supporter 122 is formed with fastener 11.
In this way, auxiliary support structure 124 can strengthen the intensity of foot stool 10, the bearing capacity of foot stool 10 is improved, so that
When foot stool 10 is supported on fuselage 20 lower end of foot stool, fuselage 30 is more stablized.
Specifically, supporter 122 is in prism-frustum-shaped is inverted, and from top to bottom, the cross section of supporter 122 is gradually reduced.So
Preferably bearing capacity can be reached, it helps reduce the weight of supporter 122, make the portable performance of foot stool 10 good, also have
When helping to make the foot stool 10 be installed on fuselage foot stool 20, the load of unmanned plane 100 is reduced as far as possible.
In the utility model embodiment, auxiliary support structure 124 is substantially in triangular shape.In this way, make the structure of foot stool 10
More stable, bearing capacity is more preferable.Certainly, in other embodiments, the shape of auxiliary support structure 124 is not limited to triangular shape,
Can also be other shapes.
In some embodiments, auxiliary support structure 124 is hollow and offer upward first opening 1242.
In this way, hollow auxiliary support structure 124 can mitigate the weight of foot stool 10, transport easy to carry, helps to carry
User experience is risen, the first opening 1242 is inserted into for the fuselage foot stool 20 of unmanned plane.
Specifically, the cross-sectional area of auxiliary support structure 124 is gradually reduced from top to bottom.Auxiliary support structure 124 includes
Top surface 1244, inclined-plane 1246 and side 1248, side 1248 are overlapped with the side 1221 of supporter 122, and 1246 lower end of inclined-plane connects
The side 1221 of supporter 122 is connected on, is tilted from bottom to top towards the direction of the side 1221 away from supporter 122, top surface 1244
Connect the upper end of side 1248 and the upper end on inclined-plane 1246.First opening 1242 is opened on top surface 1244.
In some embodiments, fastener 11 is arranged on the upper end of supporter 122.
In this way, fastener 11 is set preferably to be fastened on fuselage foot stool 20, easy to which foot stool 10 is installed on fuselage foot stool 20
Disassembled with by foot stool 10 from fuselage foot stool 20.
In some embodiments, supporter 122 is hollow and offers upward second opening 1222, supporter
122 are collectively forming holding part 101 with the hollow space of auxiliary support structure 124.
In this way, hollow supporter 122 can mitigate the weight of foot stool 10, transport easy to carry, helps to lift user
Experience, the second opening 1222 are inserted into for the fuselage foot stool 20 of unmanned plane.
Specifically, supporter 122 includes plug division 1224 and the supporting part 1226 for being connected to 1224 lower end of plug division, grafting
Portion 1224 is hollow and offers upward second opening 1222.Supporting part 1226 is in inverted prism-frustum-shaped, supporting part 1226
Offer through hole 1226a.This structure make it that the enabling capabilities of supporter 122 are preferable, can also reduce the weight of supporter 122
Amount.
Fig. 1 foot stool 10 in use, the fuselage foot stool 20 of 30 rear end of fuselage can be mounted on as the first foot stool 12
On, as shown in Figure 5.
Fig. 2 and Fig. 3 is referred to, in some embodiments, foot stool includes supporter 142 and auxiliary support structure 144, auxiliary
Supporting structure 144 is helped to be connected to the upper end of supporter 142, auxiliary support structure 144 is formed with fastener 11.
In this way, auxiliary support structure 144 can strengthen the intensity of foot stool 10, the bearing capacity of foot stool 10 is improved, so that
When foot stool 10 is supported on fuselage 20 lower end of foot stool, fuselage 30 is more stablized.
Specifically, auxiliary support structure 144 is hollow, to reduce the weight of foot stool 10, so that foot stool 10 is just
It is more preferable to take performance.
In the utility model embodiment, auxiliary support structure 144 is substantially in triangular shape.In this way, make the structure of foot stool 10
More stable, bearing capacity is more preferable.Certainly, in other embodiments, the shape of auxiliary support structure 144 is not limited to triangular shape,
Can also be other shapes.
In some embodiments, auxiliary support structure 144 includes guidance part 1442, and fastener 11 is arranged on guidance part 1442
Both sides, guide portion 14442 be used for carry fuselage foot stool 20.
In this way, guidance part 1442 can be used for guiding fuselage foot stool 20 to be inserted into foot stool 10, so that fastener 11 is preferably detained
Together in fuselage foot stool 20.
Specifically, lateral surface 1421 of the auxiliary support structure 144 including top surface 1444 and self-supporter 142 upwardly extends
Side 1446, top surface 1444 are connected to the upper end of side 1446 and guidance part 1442 to form auxiliary support structure 144.Top surface
The 3rd opening 1444a is offered on 1444 so that fuselage foot stool 20 is carried on guidance part 1442 through top surface 1444.
In some embodiments, fastener 11 includes limiting section 112, and limiting section 112 is arranged at intervals with guidance part 1442, limit
Formed between position portion 112 and guidance part 1442 formed with the limit space 1443 being inserted into for fuselage foot stool 20, limit space 1443
Holding part 101.
In this way, fastener 11 is set preferably to be fastened on fuselage foot stool 20, so that the connection of fuselage foot stool 20 and foot stool 10
More stablize.
Specifically, fastener 11 includes two sidepieces that the two sides in self-aiming portion 1442 extend perpendicular to guidance part 1442
1448, limiting section 112 is arranged on the inner surface of sidepiece 1448.It is each on two sidepieces 1448 in the utility model embodiment
It is provided with a limiting section 112.It is appreciated that limiting section is to protrude from the convex block that two sidepieces 1448 are set.Guidance part 1442,
Sidepiece 1448 and limiting section 112 cooperatively form limit space 1443.
Certainly, in other embodiments, the quantity of limiting section 112 is not limited to 1, can be any number of.
In some embodiments, supporter 142 offers lightening hole 1422.
In this way, the weight of foot stool 10 on the one hand can be mitigated, help to mitigate when foot stool 10 is installed on fuselage foot stool 20
The load of unmanned plane 100；On the other hand the cross-sectional area of supporter 142 can also be reduced, contribute to reduction supporter 142 to bring
Resistance.
Fig. 2 and Fig. 3 foot stool 10 in use, the fuselage foot of 30 front end of fuselage can be mounted on as the second foot stool 14
On frame 20, as shown in Figure 7.
In some embodiments, when foot stool 10 is applied to unmanned plane, the height of the supporting part 1226 of the first foot stool 12
It is inconsistent with the height of the supporter 142 of the second foot stool 14.
In the utility model embodiment, the height of supporting part 1226 is less than the height of supporter 142.First foot stool 12
The height of supporting part 1226 is 25mm, and the height of the supporter 142 of the second foot stool 14 is 17mm.
Certainly, in other embodiments, the height of supporting part 1226 and the height of supporter 142 are not limited to above-mentioned height
Degree, could be provided as other any height.
Fig. 4, Fig. 5 and Fig. 8 are referred to, a kind of unmanned plane 100 of the utility model embodiment includes fuselage 30, fuselage foot
Frame 20 and foot stool 10.Fuselage foot stool 20 is connected to fuselage 30.Foot stool 10 includes fastener 11, the lower end of fastener 11 and fuselage foot stool 20
It is detachably connected.
Above-mentioned unmanned plane 100, when unmanned plane 100 runs into miriness, shallow water hole, meadow, snowfield when it is poor take off environment when, foot
The lower end that frame 10 is connected to fuselage foot stool 20 can increase the fulcrum height of fuselage foot stool 20, so as to increase fuselage 30 from the ground
Distance, helps to make unmanned plane 100 work normally under poor environment.
Specifically, unmanned plane 100 further includes the holder that fuselage lower end is connected and be arranged on fuselage 30, and holder is used to load
Picture pick-up device.When running into miriness, shallow water hole, meadow, for snowfield when scene, fuselage foot stool is easily trapped into muddy, shallow water hole, meadow
Or in snowfield so that height reduction of the fuselage away from ground, the sight for the picture pick-up device for causing to be arranged on holder is blocked, or even meeting
Picture pick-up device and holder is caused to collide ground or be also absorbed in muddy, shallow water hole, meadow or snowfield and damage.The utility model
The unmanned plane 100 of embodiment, foot stool 10 are connected to the lower end of fuselage foot stool 20, increase holder and picture pick-up device from the ground away from
From the realization for helping avoid picture pick-up device is blocked, and is effectively prevented from protection holder and picture pick-up device.
In some embodiments, Fig. 1, Fig. 4 and Fig. 5 please be join, foot stool 10 includes the first foot stool 12, and the first foot stool includes branch
Support body 122 and auxiliary support structure 124, auxiliary support structure 124 are connected to the side 1221 of supporter 122,122 shape of supporter
Into there is fastener 11, fuselage foot stool 20 includes the first fuselage foot stool 22, and the first fuselage foot stool 22 forms connecting platform 222, fastener 11
For being fastened on connecting platform 222.
In this way, the first foot stool 12 is set more stably to be connected with the first fuselage foot stool 22.
It is appreciated that when fastener 11 is fastened on connecting platform 222, the first fuselage foot stool 22 is carried on the first foot stool 12
On.
In some embodiments, auxiliary support structure 124 is hollow and offers the first upward opening 1242, the
One fuselage foot stool 22 includes connector 224 and ruggedized construction 226, and connector 224 is formed with connecting platform 222, ruggedized construction 226
The side 2241 of connector 224 is connected to, ruggedized construction 226 is used to be at least partially inserted into Auxiliary support from the first opening 1242
Structure 124 is simultaneously carried on auxiliary support structure 124.
In this way, ruggedized construction 226 be inserted into auxiliary support structure 124 so that the first foot stool 12 compared with the first fuselage foot stool 22
Connection is more firm.
Specifically, the cross-sectional area of auxiliary support structure 124 is gradually reduced from top to bottom.Auxiliary support structure 124 includes
Top surface 1244, inclined-plane 1246 and side 1248, side 1248 are overlapped with the side 1221 of supporter 122, and 1246 lower end of inclined-plane connects
The side 1221 of supporter 122 is connected on, is tilted from bottom to top towards the direction of the side 1221 away from supporter 122, top surface 1244
Connect the upper end of side 1248 and the upper end on inclined-plane 1246.First opening 1242 is opened on top surface 1244.Ruggedized construction 226 is held
It is loaded on inclined-plane 1246.
In some embodiments, fastener 11 is arranged on the upper end of supporter 122, and auxiliary support structure 124 is connected to branch
The upper side 1221 of support body 122, connecting platform 222 are arranged on ruggedized construction 226 and the side of the junction of connector 224.
In this way, when ruggedized construction 226 is inserted into auxiliary support structure 124, it is flat that fastener 11 can preferably be fastened on connection
Platform 222.
In some embodiments, supporter 122 is hollow and offers upward second opening 1222, connector
224 are used to be at least partially inserted into supporter 122 from the second opening 1222.
In this way, further reinforce the connection of the first foot stool 12 and the first fuselage foot stool 22.
Specifically, supporter 122 includes plug division 1224 and the supporting part 1226 for being connected to 1224 lower end of plug division, grafting
Portion 1224 is hollow and offers upward second opening 1222.Supporting part 1226 is in inverted prism-frustum-shaped, supporting part 1226
Offer through hole 1226a.
When first foot stool 12 is connected to the lower end of the first fuselage foot stool 22, connector 224 is inserted from the second opening 1222
Enter plug division 1224, ruggedized construction 226 is inserted into auxiliary support structure 124, and fastener 11 is fastened on connecting platform 222, and assembling is simple
It is convenient.
Fig. 2, Fig. 3, Fig. 6 and Fig. 7 are referred to, in some embodiments, foot stool includes the second foot stool 14, the second foot stool 14
Including supporter 142 and auxiliary support structure 144, auxiliary support structure 144 is connected to the upper end of supporter 142, Auxiliary support
For structure 144 formed with fastener 11, the upper end of auxiliary support structure 144 offers the 3rd opening 1444a, and fuselage foot stool 20 includes the
Two fuselage foot stools 24, the second fuselage foot stool 24 are at least partially inserted into auxiliary support structure 144, fastener from the 3rd opening 1444a
11 are used to be fastened on the second fuselage foot stool 24.
In this way, the second foot stool 14 is set more stably to be connected with the second fuselage foot stool 24.
Specifically, auxiliary support structure 144 is hollow the size of auxiliary support structure 144 and the second fuselage foot stool 24
Size it is corresponding so that the second fuselage foot stool 24 from the 3rd opening 1444a be at least partially inserted into auxiliary support structure 144 when, the
Two fuselage foot stools 24 will not rock.When fastener 11 is fastened on connecting platform 333, the second fuselage foot stool 24 is carried on Auxiliary support
In structure 144.
In some embodiments, auxiliary support structure 144 includes guidance part 1442, and fastener 11 is arranged on guidance part 1442
Both sides, the second fuselage foot stool 24 includes support column 242 and bracing piece 244, and bracing piece 244 is used to incline relative to support column 242
The side of support column 242 is tiltedly connected to, bracing piece 244 is used to be carried on guidance part 1442 and is fastened on fastener 11.
In this way, guidance part 1442 coordinates with bracing piece 244, the second foot stool 14 is set more stably to connect with the second fuselage foot stool 24
Connect.
Specifically, auxiliary support structure 144 further includes top surface 1444 and the lateral surface 1421 of self-supporter 142 upwardly extends
Side 1446, top surface 1444 is connected to the upper end of side 1446 and guidance part 1442 to form auxiliary support structure 144.Guiding
Spacing between the fastener 11 of 1442 both sides of portion is corresponding with the width of bracing piece 244.The 3rd opening is offered on top surface 1444
1444a, the second fuselage foot stool 24 laterally 1446 insertion auxiliary support structures 144 and make bracing piece 244 from the 3rd opening 1444a
It is carried on guidance part 1442.
In some embodiments, fastener 11 includes limiting section 112, and limiting section 112 is arranged at intervals with guidance part 1442, limit
Set between position portion 112 and guidance part 1442 formed with the limit space 1443 being inserted into for fuselage foot stool 20, bracing piece 244 for card
In limit space 1443.
In this way, fastener 11 is set preferably to be fastened on bracing piece 244, so that the connection of fuselage foot stool 20 and foot stool 10 is more
Add stabilization.
Specifically, fastener 11 includes two sidepieces that the two sides in self-aiming portion 1442 extend perpendicular to guidance part 1442
1448, limiting section 112 is arranged on the inner surface of sidepiece 1448.It is each on two sidepieces 1448 in the utility model embodiment
It is provided with a limiting section 112.Guidance part 1442, sidepiece 1448 and limiting section 112 cooperatively form limit space 1443.Spacing sky
Between 1443 size it is corresponding with the size of bracing piece 244 so as to will not be rocked when bracing piece 244 is fastened in limit space 1443.
Certainly, in other embodiments, the quantity of limiting section 112 is not limited to 1, can be any number of.
When second foot stool 14 is connected to the lower end of the second fuselage foot stool 24, the second fuselage foot stool 24 is open from the 3rd
1444a laterally 1446 insertion auxiliary support structures 144, and make bracing piece 244 be fastened in limit space 1443, assembling
It is simple and convenient.
In the description of this specification, reference term " embodiment ", " certain embodiments ", " schematically implementation
The description of mode ", " example ", " specific example " or " some examples " etc. means to combine embodiment or example describe it is specific
Feature, structure, material or feature are contained at least one embodiment or example of the utility model.In this specification
In, schematic expression of the above terms is not necessarily referring to identical embodiment or example.Moreover, the specific spy of description
Sign, structure, material or feature can combine in an appropriate manner in any one or more embodiments or example.
While there has been shown and described that the embodiment of the utility model, those of ordinary skill in the art can manage
Solution：A variety of to the progress of these embodiments can change in the case where not departing from the principle and objective of the utility model, change,
Replace and modification, the scope of the utility model are limited by claim and its equivalent.
Claims (19)
1. a kind of foot stool, for unmanned plane, the unmanned plane includes fuselage and connects the fuselage foot stool of the fuselage, its feature exists
In the foot stool is used to connect the fuselage foot stool and including the fastener for being detachably connected with the fuselage foot stool, described
Foot stool includes supporter and auxiliary support structure, and the fastener is arranged on the supporter or the auxiliary support structure.
2. foot stool according to claim 1, it is characterised in that the foot stool is equipped with the appearance for the spacing fuselage foot stool
Portion is put, the fastener fastens with the fuselage foot stool, to prevent the fuselage foot stool from deviating from out of described holding part.
3. foot stool according to claim 2, it is characterised in that the fastener is elastic fastener.
4. foot stool according to claim 2, it is characterised in that the auxiliary support structure is connected to the side of the supporter
Face, the supporter is formed with the fastener.
5. foot stool according to claim 4, it is characterised in that the auxiliary support structure is hollow and offers upwards
Opening.
6. foot stool according to claim 4, it is characterised in that the fastener is arranged on the upper end of the supporter.
7. foot stool according to claim 5, it is characterised in that the supporter is hollow and offers upward open
Mouthful, the supporter is collectively forming the holding part with the auxiliary support structure hollow space.
8. foot stool according to claim 2, it is characterised in that the auxiliary support structure is connected to the supporter
Upper end, the auxiliary support structure are provided with the fastener.
9. foot stool according to claim 8, it is characterised in that the auxiliary support structure includes guidance part, the fastener
The both sides of the guidance part are arranged on, the guidance part is used to carry the fuselage foot stool.
10. foot stool according to claim 9, it is characterised in that the fastener includes limiting section, the limiting section with it is described
Guidance part is arranged at intervals, the limit space formed with confession fuselage foot stool insertion between the limiting section and the guidance part,
The limit space forms the holding part.
11. the foot stool according to claim 4 or 8, it is characterised in that the supporter offers lightening hole.
A kind of 12. unmanned plane, it is characterised in that including：
Fuselage；
Fuselage foot stool, the fuselage foot stool are connected to the fuselage；
Foot stool, the foot stool are used to connect the fuselage foot stool and detachable including fastener, the fastener and the fuselage foot stool
Connection；The foot stool further includes supporter and auxiliary support structure, and the fastener is arranged on the supporter or the auxiliary branch
Support structure.
13. unmanned plane according to claim 12, it is characterised in that the foot stool includes the first foot stool, first foot
Frame includes the supporter and the auxiliary support structure, and the auxiliary support structure is connected to the side of the supporter, institute
Supporter is stated formed with the fastener, the fuselage foot stool includes the first fuselage foot stool, and the first fuselage foot stool forms connection
Platform, the fastener are used to be fastened on the connecting platform.
14. unmanned plane according to claim 13, it is characterised in that the auxiliary support structure is hollow and opens up
There is upward opening, the first fuselage foot stool includes connector and ruggedized construction, and the connector is flat formed with the connection
Platform, the ruggedized construction are connected to the side of the connector, and the ruggedized construction is used to insert at least in part from the opening
Enter the auxiliary support structure and be carried on the auxiliary support structure.
15. unmanned plane according to claim 14, it is characterised in that the fastener is arranged on the upper end of the supporter,
The auxiliary support structure is connected to the upper side of the supporter, and the connecting platform is arranged on the ruggedized construction and institute
State the side of the junction of connector.
16. unmanned plane according to claim 15, it is characterised in that the supporter is hollow and offers upward
Opening, the connector are used to be at least partially inserted into the supporter from the opening.
17. unmanned plane according to claim 12, it is characterised in that the foot stool includes the second foot stool, the crus secunda
Frame includes the supporter and the auxiliary support structure, and the auxiliary support structure is connected to the upper end of the supporter, institute
State auxiliary support structure and offer opening, the fuselage foot stool bag formed with the fastener, the upper end of the auxiliary support structure
The second fuselage foot stool is included, the second fuselage foot stool is at least partially inserted into the auxiliary support structure from the opening, described
Fastener is used to be fastened on the second fuselage foot stool.
18. unmanned plane according to claim 17, it is characterised in that the auxiliary support structure includes guidance part, described
Fastener is arranged on the both sides of the guidance part, and the second fuselage foot stool includes support column and bracing piece, and the bracing piece is used for
The side for being connected to the support column is tilted relative to the support column, the bracing piece is used to be carried on the guidance part and block
It is located at the fastener.
19. unmanned plane according to claim 18, it is characterised in that the fastener includes limiting section, the limiting section with
The guidance part is arranged at intervals, and formed with limit space between the limiting section and the guidance part, the bracing piece is used to block
It is located in the limit space.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720946491.8U CN207328813U (en) | 2017-07-31 | 2017-07-31 | Foot stool and unmanned plane |
| CN201780085552.9A CN110267875A (en) | 2017-07-31 | 2017-09-21 | Foot prop and unmanned plane |
| PCT/CN2017/102810 WO2019024200A1 (en) | 2017-07-31 | 2017-09-21 | Foot stand and unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720946491.8U CN207328813U (en) | 2017-07-31 | 2017-07-31 | Foot stool and unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207328813U true CN207328813U (en) | 2018-05-08 |
Family
ID=62377632
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720946491.8U Expired - Fee Related CN207328813U (en) | 2017-07-31 | 2017-07-31 | Foot stool and unmanned plane |
| CN201780085552.9A Pending CN110267875A (en) | 2017-07-31 | 2017-09-21 | Foot prop and unmanned plane |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201780085552.9A Pending CN110267875A (en) | 2017-07-31 | 2017-09-21 | Foot prop and unmanned plane |
Country Status (2)
| Country | Link |
|---|---|
| CN (2) | CN207328813U (en) |
| WO (1) | WO2019024200A1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110267875A (en) * | 2017-07-31 | 2019-09-20 | 深圳市大疆创新科技有限公司 | Foot prop and unmanned plane |
| WO2021143449A1 (en) * | 2020-01-17 | 2021-07-22 | 深圳市道通智能航空技术股份有限公司 | Drone landing gear and drone |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104787309B (en) * | 2015-05-12 | 2016-11-09 | 厦门大学 | Rotor wing unmanned aerial vehicle undercarriage |
| KR101743585B1 (en) * | 2015-10-16 | 2017-06-05 | 주식회사 숨비 | Drone taking off and landing system having blance maintenance function |
| CN205602095U (en) * | 2016-05-05 | 2016-09-28 | 新野宇丰实业有限公司 | Electronic foot rest that receive and releases of unmanned aerial vehicle |
| CN106864735A (en) * | 2017-02-24 | 2017-06-20 | 中山市恒辉自动化科技有限公司 | A kind of telescopic unmanned plane undercarriage |
| CN106697267A (en) * | 2017-03-10 | 2017-05-24 | 太仓韬信信息科技有限公司 | Dual-purpose landing gear for unmanned aerial vehicle |
| CN106976562A (en) * | 2017-03-24 | 2017-07-25 | 西安旋飞电子科技有限公司 | A kind of dust-proof security protection unmanned plane |
| CN106927018A (en) * | 2017-04-07 | 2017-07-07 | 厦门南羽科技有限公司 | A kind of foldable unmanned plane |
| CN106945824A (en) * | 2017-05-09 | 2017-07-14 | 昊翔电能运动科技(昆山)有限公司 | A kind of unmanned plane undercarriage and method of rising and falling |
| CN207328813U (en) * | 2017-07-31 | 2018-05-08 | 深圳市大疆创新科技有限公司 | Foot stool and unmanned plane |
-
2017
- 2017-07-31 CN CN201720946491.8U patent/CN207328813U/en not_active Expired - Fee Related
- 2017-09-21 CN CN201780085552.9A patent/CN110267875A/en active Pending
- 2017-09-21 WO PCT/CN2017/102810 patent/WO2019024200A1/en active Application Filing
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110267875A (en) * | 2017-07-31 | 2019-09-20 | 深圳市大疆创新科技有限公司 | Foot prop and unmanned plane |
| WO2021143449A1 (en) * | 2020-01-17 | 2021-07-22 | 深圳市道通智能航空技术股份有限公司 | Drone landing gear and drone |
| US11858618B2 (en) | 2020-01-17 | 2024-01-02 | Autel Robotics Co., Ltd. | UAV foot stand and UAV |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2019024200A1 (en) | 2019-02-07 |
| CN110267875A (en) | 2019-09-20 |
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| CF01 | Termination of patent right due to non-payment of annual fee |
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