CN206031745U - Unmanned vehicles's frame and unmanned vehicles - Google Patents
Unmanned vehicles's frame and unmanned vehicles Download PDFInfo
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- CN206031745U CN206031745U CN201620740089.XU CN201620740089U CN206031745U CN 206031745 U CN206031745 U CN 206031745U CN 201620740089 U CN201620740089 U CN 201620740089U CN 206031745 U CN206031745 U CN 206031745U
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- compartment
- frame
- unmanned vehicle
- fuselage
- unmanned vehicles
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Abstract
The utility model provides an unmanned vehicles's frame and unmanned vehicles relates to unmanned air vehicle technique. Unmanned vehicles's frame includes: the fuselage, be equipped with at least one compartment on the fuselage, and the compartment has at least an opening for but optionally accomodates the part of one or more type in the part of a plurality of different grade types of unmanned vehicles. Unmanned vehicles includes above -mentioned unmanned vehicles's frame. Through set up on the fuselage the compartment be equipped with on the compartment the opening makes the compartment optionally accomodate the part of unmanned vehicles's one or more type to help reducing the external shared space of part helps reducing unmanned vehicles's volume, and then improves unmanned vehicles's portability.
Description
Technical field
The utility model is related to unmanned air vehicle technique, more particularly to a kind of frame of unmanned vehicle and unmanned vehicle.
Background technology
Unmanned vehicle, is not carried people to fly using what radio robot and the presetting apparatus provided for oneself were manipulated
Device, is widely used in the fields such as military affairs, the people's livelihood, the operation such as performs detection, takes photo by plane.
Unmanned vehicle includes frame, and load bearing component of the frame for unmanned vehicle, frame are provided with unmanned vehicle
Multiple functional modules, such as inertial navigation module, camera etc..Specifically, frame includes：Main casing, the side of main casing is extended with props up
Arm housing, arm housing are used for installing screw, and the bottom surface of main casing is extended with foot rest, and foot rest is for landing in unmanned vehicle
When support unmanned vehicle, main casing, an arm housing, foot rest are wholely set；And inertial navigation module, camera are fixedly installed on master
On the outer surface of housing.The unmanned vehicle of existing this structure, volume are larger, in its transportation, take larger
Space, causes its portability poor.
Utility model content
For drawbacks described above of the prior art, the utility model provides a kind of frame of unmanned vehicle and unmanned flight
Device, contributes to reducing the volume of unmanned vehicle, improves the portability of unmanned vehicle.
One side of the present utility model is to provide a kind of frame of unmanned vehicle, including：Fuselage, on the fuselage
It is provided with least one compartment；And
The compartment has at least one opening, for optionally receiving multiple inhomogeneities of the unmanned vehicle
The part of one or more types in the part of type.
Further, with the first opening, described first is open for receiving the first kind part compartment.
Further, the first kind part includes following at least one：Load, the carrier for supporting load, use
Horn, foot rest in the propulsion plant for supporting unmanned vehicle.
Further, the carrier is head or bracing frame；And/or, the load is including following at least one：Image is passed
Sensor, sonic sensor, electromagnetic sensor.
Further, described first it is opened in the bottom or side of the fuselage.
Further, with the second opening, described second is open for receiving Second Type part the compartment.
Further, the Second Type part includes following at least one：Battery, flight controller；
And/or, described second is opened in the top or side of the fuselage.
Further, the unmanned vehicle has the mode of operation of multiple different conditions, selects the described of respective type
Member storage produces the mode of operation of different conditions in the compartment.
Further, the part changes the mode of operation when inserting or be retracted in the compartment.
Further, when the first kind part is inserted or is retracted in the compartment, the unmanned vehicle is in
Off-mode or inactive state.
Further, the first kind part includes following at least one：Load, the carrier for supporting load, use
Horn, foot rest in the propulsion plant for supporting unmanned vehicle.
Further, when Second Type part is inserted or is retracted in the compartment, the unmanned vehicle is in start
State or motion state.
Further, the Second Type part includes following at least one：Battery, flight controller.
Further, when the part takes out from the compartment or stretches out, change the mode of operation.
Further, the compartment can only receive a type of part at any time.
Further, when Second Type part inserts or retract the compartment, triggering first kind part is from the compartment
Inside stretch out.
Further, the first kind part is driven and stretched out by an actuator；Or, the first kind part quilt
Second Type part is pushed and is stretched out.
Further, Second Type part from the compartment stretch out or take out when, triggering first kind part is retracted described
In compartment.
Further, the first kind part is driven and retracted by an actuator；Or, the first kind part quilt
Second Type part is pulled and is retracted.
Further, the compartment receives multiple parts simultaneously.
Further, the compartment receives the different types of part simultaneously.
Further, the part is the functional part with complete function.
Further, the part is multiple, including first kind part and Second Type part, the bottom of the fuselage
Portion offers the first opening, offers the second opening at the top of the fuselage, first opening and second opening with
The compartment connection, from the described first opening into the compartment, the Second Type part is from institute for the first kind part
The second opening is stated into the compartment.
Further, the first kind part includes head and the head mounting seat for installing the head, institute
State head mounting seat to be connected by bindiny mechanism with fuselage, and the head mounting seat can be moved with respect to fuselage, so that the cloud
Platform is by the described first opening storage to the compartment.
Further, the bindiny mechanism is telescoping mechanism, and the head mounting seat is down to by the telescoping mechanism liter
In the compartment；
Or, the bindiny mechanism is switching mechanism, and the head mounting seat is overturn to described by the switching mechanism
In compartment.
Further, the Second Type part includes battery, when the battery inserts the compartment, by the first kind
Type part is ejected from the compartment.
Further, when the battery inserts the bottom of the compartment, the connector that the battery is carried and the compartment
Interior connector electrical connection.
Further, the frame of the unmanned vehicle also include two foot rests, the foot rest can doubling in the fuselage
Bottom.
Further, each described foot rest is U-shaped mechanism, when two foot rests are folded in the bottom of the fuselage,
An opening around the compartment is arranged.
Further, the foot rest is provided with flexible restoring organ, and it is elastic that the flexible restoring organ is used for offer one
Restoring force gives the foot rest, so that the foot rest is stably folded in the bottom of the fuselage；And/or, two foot rest energy
Enough to stacking, to reduce the thickness of the unmanned vehicle after folding.
Other side of the present utility model is to provide a kind of unmanned vehicle, including the frame of above-mentioned unmanned vehicle.
The frame of the unmanned vehicle that the utility model is provided and unmanned vehicle, by arranging described on the fuselage
Compartment, is provided with the opening on the compartment, makes the compartment optionally receive of the unmanned vehicle or many
The part of individual type, so as to contribute to reducing the external shared space of the part, contributes to reducing the body of unmanned vehicle
Product, and then improve the portability of unmanned vehicle.
Description of the drawings
In order to more clearly the present invention will be described, below by the accompanying drawing based on each embodiment and correlation to the present invention
Content be described.Obviously, drawings in the following description only relate to some embodiments of the present utility model, general for this area
For logical technical staff, without having to pay creative labor, equivalent transformation can also be carried out to these accompanying drawings, and is obtained
The other accompanying drawings for being equal to relevant art content must be described.
Structural representations of the Fig. 1 for the utility model unmanned vehicle embodiment one；
Fig. 2 is the structural representation of compartment storage head in the utility model unmanned vehicle embodiment two；
Fig. 3 is by the exploded perspective view under disassembling with horn slave in the utility model unmanned vehicle embodiment two；
Fig. 4 is the structural representation of compartment storage horn in the utility model unmanned vehicle embodiment two；
Fig. 5 be the utility model unmanned vehicle embodiment three in prepare by Second Type part from fuselage roof insert every
The structural representation of room；
Fig. 6 is that Second Type part is inserted compartment from fuselage roof in the utility model unmanned vehicle embodiment three
Structural representation；
Fig. 7 be the utility model unmanned vehicle embodiment three in prepare by Second Type part from fuselage side insert every
The structural representation of room；
Fig. 8 is that Second Type part is inserted compartment from fuselage side in the utility model unmanned vehicle embodiment three
Structural representation；
The structural representation that Fig. 9 is taken out from compartment for Second Type part in the utility model unmanned vehicle embodiment five
Figure；
Figure 10 is the structural representation of Second Type part insertion compartment in the utility model unmanned vehicle embodiment five；
Structural representations of the Figure 11 for the utility model unmanned vehicle embodiment eight；
Figure 12 is the distribution schematic diagram of expansion link in the utility model unmanned vehicle embodiment eight；
Structural representations of the Figure 13 for the utility model unmanned vehicle embodiment nine；
Structural representation when Figure 14 is folded for foot rest in the utility model unmanned vehicle embodiment ten；
Structural representation when Figure 15 launches for foot rest in the utility model unmanned vehicle embodiment ten.
Wherein, 1000- frames；1100- fuselages；1110- compartments；1111- guide grooves；1112- second is open；1200- first
Type components；1210- horns；1220- heads；1221- head mounting seats；1222- expansion links；1223- connecting shafts；1230- pin
Frame；1231- flexible restoring organs；1231a- back-moving springs；1231b- clips；1232- jointed shafts；1233- avoids mouth；
1300- Second Type parts；1310- batteries；2000- propulsion plants；2100- screws；2200- motors.
Specific embodiment
It is for making purpose, technical scheme and the advantage of the utility model embodiment clearer, new below in conjunction with this practicality
Accompanying drawing in type embodiment, is clearly and completely described to the technical scheme in the utility model embodiment, it is clear that retouched
The embodiment stated is a part of embodiment of the utility model, rather than the embodiment of whole.It is in the case where not conflicting, following
Feature in embodiment and embodiment can be mutually combined.
Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment for being obtained, belongs to the scope of the utility model protection.Wherein, " on ", the term of D score etc., be to use
In description each structure relative position relation in the accompanying drawings, only understanding for ease of narration, and it is not used to limit this practicality newly
The enforceable scope of type, being altered or modified for its relativeness are under without essence change technology contents, new when this practicality is also considered as
The enforceable category of type.
Embodiment one
Structural representations of the Fig. 1 for the utility model unmanned vehicle embodiment one.
Fig. 1 is refer to, the present embodiment provides a kind of unmanned vehicle, including frame 1000 and one or more propulsion dresses
Put 2000.Frame 1000 includes fuselage 1100.Propulsion plant 2000 is arranged in the frame 1000, for providing thrust to institute
State unmanned vehicle.Specifically in the illustrated embodiment, unmanned plane during flying device is illustrated by taking many rotor unmanned aircrafts as an example；
For multiple, each propulsion plant 2000 includes screw 2100 and motor 2200 to the propulsion plant 2000, motor 2200 with
Screw 2100 connects, and motor 2200 is used for driving screw 2100 to rotate.Motor 2200 can be inner rotor motor, outer rotor
Motor etc..Screw 2100 can be folding oar, straight oar etc..Connection between screw 2100 and motor 2200 can be removable
Unload connection.
Fuselage 1100 is provided with least one compartment 1110.Compartment 1110 has at least one opening, for alternative
The part of one or more types in the multiple different types of part of ground storage unmanned vehicle.
Wherein, fuselage 1100 is formed around horn 1210, and horn 1210 is used for carrying propulsion plant 2000.Fuselage 1100
Upside or downside can be provided with compartment 1110, compartment 1110 can be rectangle, rhombus, ellipse perpendicular to the section of short transverse
Circle etc..The shape of the opening of compartment 1110 can be rectangle, ellipse etc..The present embodiment is for compartment 1110 and the shape of opening
Shape is not specifically limited, and those skilled in the art can be configured according to actual needs, as long as compartment 1110 can receive nothing
The part of people's aircraft, as long as opening can make the part of unmanned vehicle pass through and enter compartment 1110.
When fuselage 1100 is provided with a compartment 1110, compartment 1110 can be the chamber for being arranged on 1100 center of fuselage
Body, the opening of compartment 1110 can be arranged on roof, diapire and/or the side wall of compartment 1110.What is be open specifically opens up position,
Can be configured according to the position by the part of the opening on unmanned vehicle, smoothly stretch out or contract in order to part
Return.
When fuselage 1100 is provided with multiple compartments 1110, multiple compartments 1110 can be arranged side by side, for example can be with left and right simultaneously
Row is arranged, it is also possible to which left and right is arranged side by side, and multiple compartments 1110 are respectively used to accommodate different parts, to avoid different parts
Between interfere.
The type of part can be divided according to the set-up mode of part, for example：One class is removable component, that is, do not needing in fact
During existing its function, the part of fuselage 1100 can be departed from；It is another kind of for fixed component, i.e., when its function need not be realized, inconvenience
In dismounting, the part being still connected with fuselage 1100 from fuselage 1100.The type of part can with according to the function of part divide,
For example：One class is power supply part, and a class is control unit, and a class is execution unit.Those skilled in the art can be according to reality
It is determined that the type of the part being contained.
It is understood that part is the functional part that can realize complete function, part can be made up of multiple components；
A type of part can include multiple different parts, and the compartment 1110 in the present embodiment can receive one or more
One or more component in part.
The unmanned vehicle that the present embodiment is provided, by being provided with compartment 1110 on fuselage 1100, sets on compartment 1110
There is opening, make compartment 1110 optionally receive the part of one or more types of unmanned vehicle, so as to contribute to reducing
The external shared space of these parts, contributes to reducing the volume of unmanned vehicle, and then improves the portable of unmanned vehicle
Property.Additionally it is possible to avoid the part being incorporated in compartment 1110 from rocking, collide in transportation, contribute to protection
Part is not damaged by.
Embodiment two
Fig. 2 is the structural representation of compartment storage head in the utility model unmanned vehicle embodiment two；Fig. 3 is this reality
With in new unmanned vehicle embodiment two by the exploded perspective view under disassembling with horn slave；Fig. 4 be the utility model without
In people's aircraft embodiment two, compartment receives the structural representation of horn.
Fig. 2-4 are refer to, on the basis of embodiment one, with the first opening, first is open for receiving compartment 1110
First kind part 1200.Wherein, compartment 1110 can have one or more first openings.
Specifically, first kind part 1200 can include following at least one：Load, for support load carrier,
For supporting the horn 1210, foot rest of the propulsion plant 2000 of unmanned vehicle.Carrier can be head 1220 or bracing frame.
Load can include following at least one：Imageing sensor, sonic sensor, electromagnetic sensor.
Wherein, in order to avoid compartment 1110 is interfered with the screw on horn 1210, compartment 1110 can be arranged
On the downside of fuselage 1100.First opening open up position can according to compartment 1110 storage part be configured；Specifically,
One opening can be opened in top, bottom or the side of fuselage 1100.
For example：As shown in Fig. 2 when first kind part 1200 is head 1220, as head 1220 is generally arranged at
The underface of fuselage 1100, it is preferred that the first opening can be arranged on the bottom of fuselage 1100, namely the first opening be arranged on every
The bottom of room 1110, in order in 1220 retraction compartment 1110 of head.As shown in Figure 3-4, when first kind part 1200 is machine
During arm 1210, horn 1210 is detachably connected with fuselage 1100, the first opening can be arranged on the sidepiece of fuselage 1100 in order to
The horn 1210 for disassembling is inserted into compartment 1110, or the first opening be arranged on the top or bottom of fuselage 1100 so as to
In the horn for disassembling 1210 is accommodated in compartment 1110.When first kind part 1200 is foot rest, foot rest and fuselage
1100 are detachably connected, and the first opening can be arranged on the sidepiece of fuselage 1100 in order to the foot rest for disassembling is inserted compartment
1110, or the first opening is arranged on the top or bottom of fuselage 1100 in order to the foot rest for disassembling is accommodated in compartment
In 1110.
Wherein, at least two in foot rest, horn 1210 and head 1220 can be contained simultaneously, further to reduce nothing
The volume of people's aircraft.So that horn 1210 and head 1220 are contained simultaneously as an example：Specifically, can offer on fuselage 1100
At least two compartments 1110, horn 1210 are incorporated in a compartment 1110, and head 1220 is incorporated in another compartment 1110,
For example, receive head 1220 compartment 1110 can with storage horn 1210 compartment 1110 can with setting side by side up and down, or
The compartment 1110 of storage head 1220 is set in the compartment 1110 of storage horn 1210；Or, horn 1210 and head 1220
It is incorporated in same compartment 1110 simultaneously, horn 1210 is placed around head 1220.
Additionally, load can also be inertial navigation module, the load such as image that inertial navigation module is used for measuring on head 1220 is passed
The attitude information of sensor.Inertial navigation module is may be mounted on head 1220, is moved up and down with head 1220, when head 1220 it is complete
When be accommodated in compartment 1110 entirely, inertial navigation module just can be fitted with 1100 upper surface of fuselage, further to avoid inertial navigation mould
Block collides with transportation.Inertial navigation module can also be arranged on bracing frame.The present embodiment to the structure of bracing frame not
It is specifically limited, as long as bracing frame can realize its supporting role.
In the present embodiment, when unmanned vehicle is in off working state, first kind part 1200 is taken in into compartment
In 1110, to reduce the volume of unmanned vehicle, the portability of unmanned vehicle is improved, and is avoided first in transportation
Type components 1200 such as rock, collide at the colliding with of causing.
Embodiment three
Fig. 5 be the utility model unmanned vehicle embodiment three in prepare by Second Type part from fuselage roof insert every
The structural representation of room；Fig. 6 be the utility model unmanned vehicle embodiment three in Second Type part is inserted from fuselage roof
Enter the structural representation of compartment；Fig. 7 be the utility model unmanned vehicle embodiment three in prepare Second Type part slave
Insert the structural representation of compartment in body side；Fig. 8 is by Second Type part in the utility model unmanned vehicle embodiment three
The structural representation of compartment is inserted from fuselage side.
Fig. 5-8 are refer to, on the basis of embodiment one, compartment 1110 is with the second opening 1112, the second opening 1112
For receiving Second Type part 1300.
Specifically, Second Type part 1300 includes following at least one：Battery, flight controller.For the ease of battery
And/or flight controller is picked and placeed, the second opening 1112 can be opened in the top or side of fuselage 1100.When Second Type portion
When part 1300 includes battery, compartment 1110 can be battery compartment.
In the present embodiment, on the basis of embodiment two, compartment 1110 can also be opened with the first opening and second simultaneously
Mouth 1112, the first opening and the second opening 1112 are respectively arranged on two apparent surfaces of fuselage 1100 or two adjacently situated surfaces, example
Such as, the first opening place plane is vertical or parallel with the second 1112 place planes of opening.When the first opening receives the first kind
During part 1200, Second Type part 1300 can be triggered and stretched out, wherein, stretching out for Second Type part 1300 can be real manually
It is existing, it is also possible to be automatically obtained.When the second opening 1112 receives Second Type part 1300, first kind part can be triggered
1200 stretch out, and wherein, stretching out for Second Type part 1300 can be with manually implemented, it is also possible to is automatically obtained.By compartment 1110
Different parts are received at the different moment, fully using the space of compartment 1110 can be contributed to reducing unmanned vehicle
Volume, reduce unmanned vehicle and take up room.
Example IV
On the basis of aforementioned any embodiment, unmanned vehicle can have the mode of operation of multiple different conditions, choosing
The member storage of respective type is selected in compartment, the mode of operation of different conditions is produced.
Specifically, it is the first mode of operation when unmanned vehicle is in shutdown and/or inactive state；Unmanned vehicle is in
It is the second mode of operation when energization and/or state of flight.The mode of operation of unmanned vehicle is based on storage in compartment 1110
What part was realized.
When unmanned vehicle is in the first mode of operation, unmanned vehicle is in off working state, and compartment 1110 can be with
First kind part 1200 is received in selection, and first kind part 1200 can be for load, for supporting the carrier for loading, for propping up
The horn 1210, foot rest of the propulsion plant 2000 of support unmanned vehicle；Wherein, carrier can be head 1220 or bracing frame,
Load can be imageing sensor, sonic sensor, electromagnetic sensor or its any combination.As unmanned vehicle is in non-
During working condition, first kind part 1200 need not realize its corresponding function, therefore, by head 1220, foot rest and/or machine
Arm is accommodated in compartment 1110, to protect first kind part 1200 and reduce taking up room for unmanned vehicle.
When unmanned vehicle is in the second mode of operation, unmanned vehicle is in running order, and compartment 1110 can be selected
Storage Second Type part 1300 is selected, Second Type part 1300 includes following at least one：Battery, flight controller.Due to
When aircraft is in running order, first kind part 1200 needs to stretch out compartment 1110 realizes its corresponding function, Second Type
Part 1300 needs insertion or retraction compartment 1110 to realize its corresponding function.
In the present embodiment, when a part is when inserting or be retracted in compartment, change mode of operation.When a part is from compartment
Interior taking-up or when stretching out, changes mode of operation.For example：When battery is inserted or when being retracted in compartment, unmanned vehicle is by first
Mode of operation is changed into the second mode of operation；When battery from compartment takes out or stretches out, unmanned vehicle is by the second mode of operation
It is changed into the first mode of operation.
Embodiment five
The structural representation that Fig. 9 is taken out from compartment for Second Type part in the utility model unmanned vehicle embodiment five
Figure；Figure 10 is the structural representation of Second Type part insertion compartment in the utility model unmanned vehicle embodiment five.
Fig. 9-10 are refer to, on the basis of aforementioned any embodiment, compartment can only receive a type at any one time
Part.
As the mode of operation of unmanned vehicle is that the part based on storage in compartment 1110 is realized, unmanned vehicle
When mode of operation is different, in compartment 1110, the part of storage is also differed.By compartment is set to receive at any one time
Receive a kind of type components, it is ensured that at any one time, the mode of operation of unmanned vehicle is predictable, determines, is helped
In avoid occur maloperation.
For example：Unmanned vehicle in shutdown and/or during inactive state, compartment 1110 can select to receive horn 1210,
The first kind parts 1200 such as foot rest, head 1220；Unmanned vehicle is in being powered and/or compartment 1110 can be with during state of flight
Select the Second Type parts 1300 such as storage battery, flight controller.So, shut down and/or static when unmanned vehicle is in
During state, even if the unexpected switch or button for having touched unmanned vehicle of operation, unmanned vehicle cannot also be performed accordingly
Operation, effectively prevent the generation of maloperation.
Further, Second Type part 1300 is inserted or during retraction compartment, can trigger first kind part 1200 from
Stretch out in compartment.Wherein, first kind part 1200 can be driven by an actuator and be stretched out, for example：Second Type part
During 1300 insertion compartment 1110, signal is stretched out in generation, stretches out signal enabling actuator by this and drives first kind part 1200
Stretch out；Or, first kind part 1200 can be pushed by Second Type part 1300 and be stretched out, for example：In Second Type portion
During part 1300 is inserted, when Second Type part 1300 enters into 1110 certain position of compartment, Second Type part
1300 can apply to first kind part 1200 with active force, be stretched out with pushing first kind part 1200.
Correspondingly, when Second Type part 1300 stretches out from compartment or takes out, triggering first kind part 1200 is retracted
In compartment.Wherein, first kind part 1200 can be driven by an actuator and be retracted, for example：Second Type part 1300 is inserted
When entering compartment 1110, retraction signal is produced, drive first kind part 1200 to shrink by the retraction signal enabling actuator；Or
Person, first kind part 1200 are pulled and retracted by Second Type parts 1300.
Embodiment six
On the basis of previous embodiment, in the present embodiment, compartment can receive multiple parts simultaneously.
For example：First kind part 1200 can include：Head 1220, horn 1210, foot rest, Second Type part 1300
Battery, flight controller can be included.Compartment 1110 can receive head 1220, horn 1210 and foot rest, or compartment simultaneously
1110 receive battery and flight controller simultaneously.It is understandable that：Compartment 1110 can also receive different types of portion simultaneously
Part, for example：Compartment 1110 can receive head 1220 and flight controller simultaneously, wherein, flight controller can be fixed on every
On the inwall of room 1110, to simplify using assembling process during unmanned vehicle.
Embodiment seven
On the basis of aforementioned any embodiment, the part that can be chosen to be accommodated in compartment 1110 is multiple, and part can
With including first kind part 1200 and Second Type part 1300.
The bottom of fuselage 1100 offers the first opening, and the top of fuselage 1100 or sidepiece offer the second opening
1112, the first opening and the second opening 1112 connects with compartment, and first kind part 1200 is open from first and enters compartment, the
Two type components 1300 enter compartment from the second opening 1112.
Specifically, first kind part 1200 can include that head 1220 and the head for installing head 1220 are installed
Seat 1221, head mounting seat 1221 is connected by bindiny mechanism with fuselage 1100, and head mounting seat 1221 can be with respect to fuselage
1100 motions, so that head 1220 is received to compartment 1110 by the first opening.Wherein, head mounting seat 1221 can be in plate
Shape, bindiny mechanism can be telescoping mechanism or switching mechanism.
Second Type part 1300 can include battery, during battery insertion compartment 1110, head 1220 be pushed up from compartment 1110
Go out；And during the bottom of battery insertion compartment 1110, the connector that battery is carried is electrically connected with the connector in compartment 1110, is thought
The a certain part of unmanned vehicle or unmanned vehicle is powered.
When wherein, in the insertion of Second Type part 1300 compartment 1110, first kind part 1200 can be triggered from compartment
Stretch out in 1110；When first kind part 1200 is stretched out from compartment 1110, first kind part 1200 can be triggered and performed
Its corresponding function, for example, can trigger imageing sensor and start to gather image, can trigger inertial navigation module and start measuring speed
Information and/or positional information.
In the present embodiment, when being in shutdown and/or inactive state due to unmanned vehicle, it will usually take out battery, with
Battery is charged, and avoids maloperation.The present embodiment takes full advantage of what is formed after battery is taken out from compartment 1110
Remaining space, head 1220 is accommodated in the remaining space, can preferably protect what head 1220 and head 1220 were carried
Imageing sensor, Inertial Measurement Unit etc..
Embodiment eight
Structural representations of the Figure 11 for the utility model unmanned vehicle embodiment eight；For the utility model, nobody flies Figure 12
The distribution schematic diagram of expansion link in row device embodiment eight.
Figure 11-12 are refer to, on the basis of embodiment seven, bindiny mechanism is telescoping mechanism, and head mounting seat 1221 is led to
Cross bindiny mechanism's liter to be down in compartment.Bindiny mechanism can include：At least two expansion links 1222, the two ends point of expansion link 1222
It is not hinged with head mounting seat 1221 and fuselage 1100, so that head 1220 slips into receiving space.As shown in figure 12, connect
Mechanism can include four expansion links 1222, so that head 1220 smoothly slips into receiving space.
Specifically, expansion link 1222 includes at least two points of bars, at least two points of bars it is end to end successively and adjacent two
Individual point of bar is slidably connected.So that expansion link 1222 includes two points of bars as an example, when head 1220 stretches out compartment 1110, one point of bar edge
Slide away from the direction of another point of bar；When head 1220 is retracted to compartment 1110, one point of bar is along towards the direction of another point of bar
Slide.
Wherein, adjacent two be divided between bar be additionally provided with for drive between two points of adjacent bars with respect to slide drive
Moving part.The actuator can be the common actuators such as cylinder, motor, as long as can realize that the function of driving point bar to slide relatively is
Can.
For example：Expansion link 1222 can be gas strut；Head mounting seat 1221 includes relative two seating side；It is flexible
Part is four, arranges two expansion links 1222 in each seating side；The head end of two expansion links 1222 on same mounting surface
Be hinged in head mounting seat 1221 by same rotating shaft, tail end mutually away from stretch out and be hinged on two of receiving space it is relative
On the wall of side.Guiding work is played it is preferred that surrounding and can open up the movement to head 1220 on the 1100 side wall of fuselage of compartment 1110
Compartment 1111.
In the present embodiment, when user is needed using unmanned vehicle, when battery 1310 is inserted compartment 1110, gas strut
Extended configuration is become by compressive state, and promotes head 1220 to move to 1100 bottom of fuselage, wherein, battery 1310 is fully-inserted
During compartment 1110, head 1220 is located exactly at the lowermost end of compartment 1110；When battery 1310 is extracted by user, can be by user
1220 retraction compartment 1110 of head is promoted, wherein, after 1220 motion certain distance of head, head 1220 can be promoted by gas strut
Until head 1220 withstands on 1100 top of fuselage, now, gas strut is compressive state.
Embodiment nine
Structural representations of the Figure 13 for the utility model unmanned vehicle embodiment nine.
Figure 13 is refer to, on the basis of embodiment seven, bindiny mechanism is switching mechanism, and head mounting seat 1221 is by connecting
Connection mechanism is overturn to compartment.Bindiny mechanism can include connecting shaft 1223, and head mounting seat 1221 is cut with scissors by connecting shaft 1223
It is connected on the side wall of compartment 1110, overturn around connecting shaft 1223 by head mounting seat 1221 to enter accommodation space.
Wherein, connecting shaft 1223 can be arranged on the side wall of the opening of compartment 1110, on the opening, away from connection
Stopper section can be set on the opposite side wall of axle 1223, for when head 1220 stretches out compartment 1110, limiting head mounting seat
1221 overturn in horizontality, and head mounting seat 1221 is played a supportive role；The stopper section can be at least one bar
Shape structure or platy structure.
In the present embodiment, head mounting seat 1221 can be promoted manually to overturn；It is preferred that switching mechanism can also include lock
Fixed structure, after latch-up structure is for being retracted to compartment 1110 in head 1220, locked and fixed head mounting seat 1221, with more
Well in transportation protect head 1220；For example：Latch-up structure can be the buckle knot being arranged on 1110 inwall of compartment
Structure, to engage head mounting seat 1221.Or, head mounting seat 1221 can be driven to overturn by motor etc., in order to automatic
The flip angle of control head mounting seat 1221.
Embodiment ten
Structural representation when Figure 14 is folded for foot rest in the utility model unmanned vehicle embodiment ten；Figure 15 is this reality
Structural representation when being launched with foot rest in new unmanned vehicle embodiment ten.
Figure 14-15 are refer to, on the basis of aforementioned any embodiment, unmanned vehicle frame 1000 also includes two pin
Frame 1230, foot rest 1230 can be with doublings in the bottom of fuselage 1100.When unmanned vehicle is in off working state, foot rest 1230
Can be taken up room with reducing unmanned vehicle with doubling in 1100 bottom of fuselage, reduce the volume of unmanned vehicle, improve nobody
The portability of aircraft.
Each foot rest 1230 is U-shaped mechanism, when two foot rests 1230 are folded in the bottom of fuselage 1100, around compartment
1110 opening is arranged, so that the part being accommodated in compartment 1110 such as head smoothly can stretch out.
Specifically, frame 1000 is provided with flexible restoring organ 1231, and flexible restoring organ 1231 is used for providing a bullet
Property restoring force makes foot rest 1230 stably be folded in the bottom of fuselage 1100 to foot rest 1230.For example：Flexible restoring organ 1231
Including back-moving spring 1231a and clip 1231b；Fuselage 1100 is provided with chute, and the cross section of chute can be rectangle, semicircle
Shape, U-shaped etc., clip 1231b are slided and are arranged in chute, the telescopic direction of back-moving spring 1231a and the bearing of trend one of chute
Cause, namely one end of back-moving spring 1231a is offseted with the roof of chute, the other end of back-moving spring 1231a supports clip
1231b；Foot rest 1230 is provided with fixing groove towards the side of one end of fuselage 1100, when 1230 doubling of foot rest is in 1100 bottom of fuselage
When, back-moving spring 1231a is pressed on clip 1231b in the fixing groove of foot rest 1230, so that foot rest 1230 is stably folded
In the bottom of fuselage 1100.
Wherein, back-moving spring 1231a can for example have resilient rubber parts to be replaced by other elastic components.Clip
1231b can include stop part and connecting portion, connecting portion for coordinating with the chute on fuselage 1100, stop part for fixation
Groove is rotated with prevention foot rest 1230 is merged.
Additionally, foot rest 1230 is hinged with fuselage 1100 by jointed shaft 1232, clip 1231b is arranged on jointed shaft 1232
Top, moves down distance to limit clip 1231b by jointed shaft 1232, prevents the clip 1231b from coming off.When opening foot rest
When 1230, need to pull up clip 1231b so that clip 1231b departs from fixing groove, when foot rest 1230 is fully opened, pine
Clip 1231b is opened, in the presence of the elastic-restoring force of back-moving spring 1231a, clip 1231b is moved down and fixed foot rest
1230, prevent foot rest 1230 from rocking.
Wherein, the telescopic direction of back-moving spring 1231a can be with vertical with the bearing of trend of chute, namely back-moving spring
One end of 1231a is offseted or is connected with the side wall of chute, the other end of back-moving spring 1231a support with clip 1231b or
Person connects；Now, after clip 1231b being snapped in fixing groove manually, can by its elastic-restoring force in back-moving spring 1231a
To prevent clip 1231b from moving relative to fuselage 1100 or foot rest 1230, and then foot rest 1230 is made stably to be folded in machine
The bottom of body 1100.
In the present embodiment, when operating personnel are needed using unmanned vehicle, foot rest 1230 is first opened, and passes through clip
1231b compresses foot rest 1230；Then battery 1310 is inserted into compartment 1110 by the second opening 1112, meanwhile, by battery
1310 push head 1220 makes head 1220 move down and stretch out compartment 1110 by the first opening.
Further, at the bottom of fuselage 1100, two foot rests 1230 can be with nesting to being stacked in one for 1230 doubling of foot rest
Rise, to reduce the thickness of the unmanned vehicle after folding, further reduce the volume of unmanned vehicle.
For example：Open up fluted on one of foot rest 1230, in groove, be provided with holding section；Another foot rest 1230 is contained in
In the groove, and on the foot rest 1230, offer the connecting hole coordinated with holding section；By holding section and the cooperation of connecting hole, enter
One step ensures that foot rest 1230 can stably be folded in the bottom of fuselage 1100；Wherein, two foot rests 1230 can include：Two
The support bar being parallel to each other and the connecting rod of connection support bar；Foot rest 1230 is provided with the connecting rod for another foot rest 1230 and passes through
Avoidance mouth 1233.Or, a wherein foot rest 1230 is enclosed on the outside of another foot rest 1230, and a wherein foot rest 1230 and opens
It is provided with the avoidance mouth 1233 passed through for the connecting rod of another foot rest 1230.
Finally it should be noted that：Various embodiments above is only illustrating the technical solution of the utility model, rather than which is limited
System；Although being described in detail to the utility model with reference to foregoing embodiments, one of ordinary skill in the art should
Understand：Which still can be modified to the technical scheme described in foregoing embodiments, or to which part or whole
Technical characteristic carries out equivalent；And these modifications or replacement, do not make the essence of appropriate technical solution depart from this practicality new
The scope of each embodiment technical scheme of type.
Claims (31)
1. a kind of frame of unmanned vehicle, it is characterised in that include：
Fuselage, the fuselage are provided with least one compartment；And
The compartment has at least one opening, for optionally receiving the multiple different types of of the unmanned vehicle
The part of one or more types in part.
2. the frame of unmanned vehicle according to claim 1, it is characterised in that the compartment is with the first opening, institute
The first opening is stated for receiving first kind part.
3. the frame of unmanned vehicle according to claim 2, it is characterised in that the first kind part includes as follows
It is at least one：Load, the carrier for supporting load, the horn of propulsion plant for supporting unmanned vehicle, foot rest.
4. the frame of unmanned vehicle according to claim 3, it is characterised in that the carrier is head or bracing frame；
And/or, the load is including following at least one：Imageing sensor, sonic sensor, electromagnetic sensor.
5. the frame of unmanned vehicle according to claim 2, it is characterised in that described first is opened in the machine
The bottom or side of body.
6. the frame of unmanned vehicle according to claim 1, it is characterised in that the compartment is with the second opening, institute
The second opening is stated for receiving Second Type part.
7. the frame of unmanned vehicle according to claim 6, it is characterised in that the Second Type part includes as follows
It is at least one：Battery, flight controller；
And/or, described second is opened in the top or side of the fuselage.
8. the frame of unmanned vehicle according to claim 1, it is characterised in that the unmanned vehicle have it is multiple not
With the mode of operation of state, select the member storage of respective type in the compartment, produce the behaviour of different conditions
Make state.
9. the frame of unmanned vehicle according to claim 8, it is characterised in that the part is being inserted or is being retracted in institute
When stating in compartment, change the mode of operation.
10. the frame of unmanned vehicle according to claim 9, it is characterised in that first kind part is inserted or retracted
When in the compartment, the unmanned vehicle is in off-mode or inactive state.
The frame of 11. unmanned vehicles according to claim 10, it is characterised in that the first kind part include as
Lower at least one：Load, the carrier for supporting load, the horn of propulsion plant for supporting unmanned vehicle, foot rest.
The frame of 12. unmanned vehicles according to claim 9, it is characterised in that Second Type part is inserted or retracted
When in the compartment, the unmanned vehicle is in open state or motion state.
The frame of 13. unmanned vehicles according to claim 12, it is characterised in that the Second Type part include as
Lower at least one：Battery, flight controller.
The frame of 14. unmanned vehicles according to claim 8, it is characterised in that the part is taken from the compartment
When going out or stretching out, change the mode of operation.
The frame of 15. unmanned vehicles according to claim 1, it is characterised in that the compartment at any time can only
Receive a type of part.
The frame of 16. unmanned vehicles according to claim 15, it is characterised in that Second Type part is inserted or retracted
During the compartment, triggering first kind part is stretched out from the compartment.
The frame of 17. unmanned vehicles according to claim 16, it is characterised in that the first kind part is driven by one
Moving part drives and stretches out；
Or, the first kind part is pushed and stretched out by Second Type part.
The frame of 18. unmanned vehicles according to claim 15, it is characterised in that Second Type part is from the compartment
When stretching out or taking out, triggering first kind part is retracted in the compartment.
The frame of 19. unmanned vehicles according to claim 18, it is characterised in that the first kind part is driven by one
Moving part drives and retracts；
Or, the first kind part is pulled and retracted by Second Type part.
The frame of 20. unmanned vehicles according to claim 1, it is characterised in that the compartment receives multiple institutes simultaneously
State part.
The frame of 21. unmanned vehicles according to claim 20, it is characterised in that the compartment receives inhomogeneity simultaneously
The part of type.
The frame of 22. unmanned vehicles according to claim 1, it is characterised in that the part is with complete function
Functional part.
The frame of 23. unmanned vehicles according to claim 1, it is characterised in that the part is multiple, including first
Type components and Second Type part, the bottom of the fuselage offer the first opening, offer at the top of the fuselage
Two openings, first opening and second opening are connected with the compartment, and the first kind part is from described first
, into the compartment, the Second Type part is from the described second opening into the compartment for opening.
The frame of 24. unmanned vehicles according to claim 23, it is characterised in that the first kind part includes cloud
Platform and the head mounting seat for installing the head, the head mounting seat is connected by bindiny mechanism with fuselage, and institute
State head mounting seat to move with respect to fuselage, so that the head is received to the compartment by the described first opening.
The frame of 25. unmanned vehicles according to claim 24, it is characterised in that the bindiny mechanism is telescopic machine
Structure, the head mounting seat are down in the compartment by the telescoping mechanism liter；
Or, the bindiny mechanism is switching mechanism, and the head mounting seat overturn to the compartment by the switching mechanism
It is interior.
The frame of 26. unmanned vehicles according to claim 23, it is characterised in that the Second Type part includes electricity
Pond, when the battery inserts the compartment, the first kind part is ejected from the compartment.
The frame of 27. unmanned vehicles according to claim 26, it is characterised in that the battery inserts the compartment
During bottom, the connector that the battery is carried is electrically connected with the connector in the compartment.
The frame of 28. unmanned vehicles according to claim 1, it is characterised in that also including two foot rests, the foot rest
Can doubling in the bottom of the fuselage.
The frame of 29. unmanned vehicles according to claim 28, it is characterised in that each described foot rest is U-shaped machine
Structure, when two foot rests are folded in the bottom of the fuselage, an opening around the compartment is arranged.
The frame of 30. unmanned vehicles according to claim 28, it is characterised in that the foot rest is provided with elastic reset
Mechanism, the flexible restoring organ are used for providing an elastic-restoring force to the foot rest, so that the foot rest is stably folded
In the bottom of the fuselage；
And/or, two foot rests can be to stacking, to reduce the thickness of the unmanned vehicle after folding.
31. a kind of unmanned vehicles, it is characterised in that include：
The frame of the unmanned vehicle described in any one of claim 1-30；And
One or more propulsion plants, in the frame, for providing thrust to the unmanned vehicle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620740089.XU CN206031745U (en) | 2016-07-13 | 2016-07-13 | Unmanned vehicles's frame and unmanned vehicles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620740089.XU CN206031745U (en) | 2016-07-13 | 2016-07-13 | Unmanned vehicles's frame and unmanned vehicles |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206031745U true CN206031745U (en) | 2017-03-22 |
Family
ID=58310931
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620740089.XU Expired - Fee Related CN206031745U (en) | 2016-07-13 | 2016-07-13 | Unmanned vehicles's frame and unmanned vehicles |
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| CN (1) | CN206031745U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107487432A (en) * | 2017-09-22 | 2017-12-19 | 贵州信鸽科技有限公司 | Unmanned vehicle and flight instruments |
| CN108482658A (en) * | 2018-03-09 | 2018-09-04 | 芜湖翼讯飞行智能装备有限公司 | A kind of camera shooting unmanned plane |
| CN110356568A (en) * | 2019-07-02 | 2019-10-22 | 深圳市律远汇智科技有限公司 | A kind of good solar energy unmanned flight's device of protection effect convenient for storage |
| CN110884645A (en) * | 2019-12-09 | 2020-03-17 | 湖南浩天翼航空技术有限公司 | Unmanned aerial vehicle that can cushion and easily receive and release falls to ground supporting mechanism |
| CN110979681A (en) * | 2019-12-30 | 2020-04-10 | 南京航空航天大学 | Long-endurance rotor unmanned aerial vehicle for monitoring and managing farming activities |
-
2016
- 2016-07-13 CN CN201620740089.XU patent/CN206031745U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107487432A (en) * | 2017-09-22 | 2017-12-19 | 贵州信鸽科技有限公司 | Unmanned vehicle and flight instruments |
| CN108482658A (en) * | 2018-03-09 | 2018-09-04 | 芜湖翼讯飞行智能装备有限公司 | A kind of camera shooting unmanned plane |
| CN108482658B (en) * | 2018-03-09 | 2020-05-08 | 芜湖翼讯飞行智能装备有限公司 | Unmanned aerial vehicle makes a video recording |
| CN110356568A (en) * | 2019-07-02 | 2019-10-22 | 深圳市律远汇智科技有限公司 | A kind of good solar energy unmanned flight's device of protection effect convenient for storage |
| CN110884645A (en) * | 2019-12-09 | 2020-03-17 | 湖南浩天翼航空技术有限公司 | Unmanned aerial vehicle that can cushion and easily receive and release falls to ground supporting mechanism |
| CN110979681A (en) * | 2019-12-30 | 2020-04-10 | 南京航空航天大学 | Long-endurance rotor unmanned aerial vehicle for monitoring and managing farming activities |
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