CN207658058U - Separation type flight formula mobile terminal and its flying power unit - Google Patents
Separation type flight formula mobile terminal and its flying power unit Download PDFInfo
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- CN207658058U CN207658058U CN201721648240.8U CN201721648240U CN207658058U CN 207658058 U CN207658058 U CN 207658058U CN 201721648240 U CN201721648240 U CN 201721648240U CN 207658058 U CN207658058 U CN 207658058U
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Abstract
The utility model discloses separation type flight formula mobile terminal and its flying power units, are related to intelligent mobile terminal technical field.A kind of separation type flight formula mobile terminal, including matrix and flying power unit, described matrix is separate structure with flying power unit, it is provided with installation interconnecting piece on the flying power unit, it is provided in described matrix and the matched power connection of interconnecting piece is installed, flying power unit is removably installed on matrix by installing interconnecting piece and power connection.The flight formula mobile terminal of the utility model is designed using seperated, and flying power unit is removably installed on matrix so that mobile terminal can be used as common mobile terminal use, also can be used as unmanned plane use, meets different application scene.
Description
Technical field
The utility model is related to intelligent mobile terminal technical fields.
Background technology
UAV abbreviation " unmanned plane " is one kind by radio robot and/or itself presetting apparatus
The unmanned vehicle of operation, comes across the 1940s earliest.Unmanned plane is widely used, at low cost, and efficiency-cost ratio is good, no
Only there is extremely important effect in modern war, more holds out broad prospects in civil field.Currently, unmanned plane is transported extensively
Use the fields such as guard, city management, agricultural, geology, meteorology, electric power, rescue and relief work, video capture.In the prior art, some
The unmanned plane of fixed-wing may only have a piece of rotor, and the unmanned plane of some helicopter classes may have two panels or two panels or more
Rotor；By the mechanical property of rotor it is found that every rotor makes the air-flow of surrounding generate variation by rotation, risen to be formed
Power, therefore, every rotor are required to corresponding certain separate space, create conditions to form lift for it.More rotors nobody
Machine usually all can realize rotor by the way of symmetrical, and by controlling the difference active force that different direction rotor generates
The control of unmanned plane.However, its body of the unmanned plane of more rotor structures occupies large area space, fiber crops are brought to transport and storage
It is tired.
Currently, also there is folding unmanned plane, so as to unmanned plane when not in use can folding, to improve unmanned plane
Portability.Such as Chinese patent CN201520580644.2, a kind of entitled folding unmanned plane of utility model provide
A kind of rotor of loose-leaf system folds solution, the line centered on body, and the rotor of both sides is constituted a pair two-by-two, and by with
Connecting pin on body constitutes loose-leaf structure.But which still has insufficient place：Due to rotor two-by-two constitute one
Piece loose-leaf, therefore the connecting pin in main body is one kind to be made for a long time by the fixed mode of upper and lower two gears completion
With the abnormal rolling of loose-leaf when may occur causing work since two gear wear degree up and down on a piece of loose-leaf are different
It is dynamic.
Meanwhile with the development of electronics technology, the performance of the intelligent mobile terminals such as mobile phone is higher and higher, it is increasingly intelligent,
The design and use of cell phone software also enhanced convenience.The function of how combining unmanned plane and intelligent mobile terminal, provides more intelligence
Can, easy to carry and intelligent terminal easy to use, be a problem to be solved.
Invention content
The purpose of this utility model is that：It is whole a kind of separation type flight formula movement has been overcome the deficiencies of the prior art and provide
The flight formula mobile terminal of end and its flying power unit, the utility model is designed using seperated, and flying power unit is detachable
Ground is installed on matrix so that mobile terminal can be used as ordinary terminal use and (also can be used as unmanned plane use, meet different application
Scene.
To realize that above-mentioned target, the utility model provide following technical solution：
A kind of separation type flight formula mobile terminal, including matrix and flying power unit, described matrix and flying power list
Member is separate structure, and installation interconnecting piece is provided on the flying power unit, is provided in described matrix and installation interconnecting piece
Flying power unit is removably installed in matrix by matched power connection by installing interconnecting piece and power connection
On.
The mobile terminal is mobile phone, tablet computer, wearable smart machine or laptop, and described matrix includes electricity
Processor, memory, communication module, display screen, power supply and the camera settings of connection.
Further, described matrix further includes navigator fix structure, flight controller and the gyroscope of communication connection；
The navigator fix structure includes camera probe, ultrasonic probe, barometer, inertia survey meter, geomagnetic sensor
With it is one or more in height sonar meter；
The flight controller is transmitted with gyroscope, navigator fix structure into row information, according to gyroscope and navigator fix
The information of structural transmission controls flying power unit.
Further, the installation interconnecting piece is the groove or cavity being arranged on flying power unit, utilizes base end
As power connection, the inside dimension of the groove or cavity is matched with the appearance and size of base end so that described matrix
End nested can be mounted in the groove or cavity.
Further, after the power connection connect with installation interconnecting piece, can realize matrix and flying power unit it
Between electric power and signal transmission.
Preferably, the power connection be Micro) USB port, the installation interconnecting piece be and Micro) USB port
Matched plug.
Further, the power connection, which is arranged, is arranged in the upper side and lower side of matrix and/or power connection in matrix
Left and right side.
Further, the flying power unit includes shell, at least one rotor module, and receiving is provided on the shell
At least one flight cavity of the rotor module.
Preferably, the shell is rectangular body case, and the flight cavity is circular cylindrical cavity, is set in each flight cavity
Set a rotor module.
Protective shell is provided on the flight cavity, the protective shell is the shell of hollow out, and the rotor module setting exists
In protective shell.
Further, it is provided with flight accumulator on the flying power unit, to provide electricity to flying power unit
Power.
The invention also discloses a kind of flying power units, it is characterised in that：It is arranged on the flying power unit
There is installation interconnecting piece, flying power unit can be removably installed in by intelligent mobile terminal by the installation interconnecting piece
On.
Further, it after the flying power unit is installed on intelligent mobile terminal, is carried out by the installation interconnecting piece
Electric power between intelligent mobile terminal and flying power unit and signal transmission.
Further, the installation interconnecting piece is the groove or cavity being arranged on flying power unit, the groove or sky
The inside dimension of chamber is matched with the appearance and size of intelligent mobile terminal end so that the intelligent mobile terminal end can be nested
In the groove or cavity.
Further, the installation interconnecting piece be and Micro) the matched plug of USB port, the installation interconnecting piece can insert
Enter the Micro on intelligent mobile terminal) in USB port, to which flying power unit is mounted on intelligent mobile terminal.
Further, the flying power unit includes shell, at least one rotor module, and receiving is provided on the shell
At least one flight cavity of the rotor module, in the side of shell setting installation interconnecting piece.
The utility model due to using the technology described above, compared with prior art, as an example, has the following advantages that
And good effect：The flight formula mobile terminal of the utility model, flying power unit are removably installed on matrix, dismounting spirit
It is living so that mobile terminal can be used as ordinary terminal using also can be used as unmanned plane use, eliminate fixed flying power unit
Influence to user's normal use mobile terminal.By taking flight formula mobile phone as an example, as mobile phone in use, remove flying power list
Member is convenient for user's communication, online and camera shooting；When needing as unmanned plane, on mobile phone install flying power unit, it can be achieved that
It flies, take photo by plane and monitoring function.
Description of the drawings
Fig. 1 is the structural schematic diagram one under the separation type flight formula mobile phone disassembled form that the utility model embodiment provides.
Fig. 2 is the structural schematic diagram under the separation type flight formula cellular phone combination state in Fig. 1.
Fig. 3 is the structural schematic diagram two under the separation type flight formula mobile phone disassembled form that the utility model embodiment provides.
Fig. 4 is the structural schematic diagram under the separation type flight formula cellular phone combination state in Fig. 3.
Fig. 5 is that the structure for the flight formula mobile phone that the upper and lower sides that the utility model embodiment provides install flying power unit is shown
It is intended to.
Fig. 6 is that the structure for the flight formula mobile phone that the left and right sides that the utility model embodiment provides installs flying power unit is shown
It is intended to.
Fig. 7 is the structural schematic diagram for the protective shell that the utility model embodiment provides.
Fig. 8 is the scheme of installation for the protective shell that the utility model embodiment provides.
Fig. 9 is the structural schematic diagram for the flying power unit that the utility model embodiment provides.
Reference sign：
Flight formula mobile phone 100；
Shell 110 installs interconnecting piece 111, extension and contraction control button 111a；
Matrix 120, power connection 121, electric connection contacts 122；
Rotor module 130, flight cavity 140, protective shell 150.
Specific implementation mode
To separation type flight formula mobile terminal disclosed by the utility model and its fly below in conjunction with the drawings and specific embodiments
Action edge unit is described in further detail.It should be noted that the technical characteristic or technology described in following embodiments are special
The combination of sign is not construed as isolated, they can be combined with each other to reach superior technique effect.Following
In the attached drawing of embodiment, the identical label that each attached drawing occurs represents identical feature or component, can be applied to different implementations
In example.Therefore, once being defined in a certain Xiang Yi attached drawing, then it need not further be begged in subsequent attached drawing
By.
It should be noted that structure, ratio, size etc. depicted in this specification institute attached drawing, only coordinating explanation
The revealed content of book is not limited to the enforceable limit of utility model so that those skilled in the art understands and reads
Fixed condition, the modification of any structure, the change of proportionate relationship or the adjustment of size, in the work(that does not influence utility model and can be generated
Under effect and the purpose that can reach, it should all fall in the range of the revealed technology contents of utility model can be covered.This practicality
The range of novel preferred embodiment includes other realization, wherein described or discussion the sequence, including root can not be pressed
According to involved function by it is basic simultaneously in the way of or in the opposite order, to execute function, this should be by the reality of the utility model
A person of ordinary skill in the field is applied to be understood.
Technology, method and apparatus known to person of ordinary skill in the relevant may be not discussed in detail, but suitable
In the case of, the technology, method and apparatus should be considered as authorizing part of specification.Institute that is shown here and discussing
Have in example, any occurrence should be construed as merely illustrative, not as limitation.Therefore, exemplary embodiment
Other examples can have different values.
Embodiment
A kind of separation type flight formula mobile terminal, including matrix and flying power unit, described matrix and flying power list
Member is separate structure, and installation interconnecting piece is provided on the flying power unit, is provided in described matrix and installation interconnecting piece
Flying power unit is removably installed in matrix by matched power connection by installing interconnecting piece and power connection
On.
The mobile terminal can be mobile phone, tablet computer, wearable smart machine or laptop.For aforementioned shifting
The type of dynamic terminal, is arranged in correspondence with described matrix, described matrix includes that can realize the basic knot of above-mentioned mobile terminal function
Structure.Preferably, described matrix may include processor, memory, communication module, display screen, power supply and the camera shooting of electrical connection
Structure.Certainly, described matrix can also be as needed, setting earphone jack, power key, volume adjustment key, flash lamp, receiver,
The structures such as loud speaker, USB interface are to realize that corresponding function, the setting of above-mentioned each structure can refer to various intelligence in the prior art
The conventional arrangement of mobile terminal, details are not described herein.
It is described by taking separation type flight formula mobile phone as an example in the present embodiment.
Shown in Figure 1, flight formula mobile phone 100 includes shell 110, matrix 120 and flying power unit.Corresponding to described
Flight formula mobile phone, described matrix 120 are specially mobile module.The mobile module is separate structure, institute with flying power unit
It states and is provided with installation interconnecting piece 111 on flying power unit, be provided on the mobile module matched with installation interconnecting piece 111
Flying power unit is removably installed in hand by power connection 121 by installing interconnecting piece 111 and power connection 121
In machine module (i.e. matrix 120).
The upside in matrix 130, downside, left side and/or right side can be arranged in the power connection 121.Preferably, institute
Flying power unit is stated to be symmetrical arranged on matrix 120, it is corresponding, the power connection be arranged in the upside of matrix 120 and
Downside, and/or the left and right side in matrix 120 is set.
In the present embodiment, after the power connection is connect with installation interconnecting piece, the connection can be based on and realize matrix 120
Electric power between flying power unit and signal transmission.Preferably, shown in Figure 1, the power connection 121 is setting
Micro on mobile module) USB port, the installation interconnecting piece 111 is to be arranged in flying power unit and Micro) USB
The plug of port match.
When needing to realize flight function, flying power unit can be plugged on matrix by user by installing interconnecting piece 111
Micro on 120) on USB port, it is shown in Figure 2 to form flight formula mobile phone 100.Based on the Micro) ends USB
Mouthful, electric power and signal transmission can be carried out between described matrix 120 and flying power unit.Specifically, such as passing through matrix 120
On power supply to flying power unit power, for another example pass through matrix 120 control flying power unit flight parameter.
When controlling the flight parameter of flying power unit by matrix 120, specifically, described matrix is also correspondingly arranged on
Navigator fix structure, flight controller and gyroscope, navigator fix structure, flight controller and gyroscope three communication connection.
The communication connection can be wire communication connection, can also be wireless communication connection.The navigator fix structure includes camera shooting
It is one or more in probe, ultrasonic probe, barometer, inertia survey meter, geomagnetic sensor and height sonar meter.It is described to fly
Line control unit can be transmitted with gyroscope, navigator fix structure into row information, and according to gyroscope and navigator fix structural transmission
Information flying power unit is controlled.
It should be noted that after the power connection is connect with installation interconnecting piece, the connection can be based on and realize matrix
Electric power and signal transmission between flying power unit are preferred modes, and described matrix is being connect with flying power unit
Afterwards, can also be simply to combine, and without electric power and signal transmission.By way of example and not limitation, such as it is described
Flying power unit electric power and signal control can be realized based on power source special and nonshared control unit.Specifically, can fly
On action edge unit be arranged flight accumulator, flight accumulator to flying power unit provide electric power.And special control
Device processed, for example can be unmanned controller in the prior art.Certainly, those skilled in the art will be appreciated that, matrix and flight
Realize that electric power and signal transmission are preferably modes after power unit connection, advantage by way of example and not limitation, such as
Pass through existing matrix --- mobile module --- in user and checks flight parameter etc..
It is shown in Figure 3, to install another setting structure of interconnecting piece.Specifically, the installation interconnecting piece 111 is to set
Set groove or cavity on flying power unit, using base end as power connection, the groove or cavity it is interior
Portion's size is matched with the appearance and size of base end so that described matrix end nested can be mounted on the groove or cavity
It is interior.In this way, matrix and flying power unit can be attached by nested mode by nested mounting means.Relative to
Micro) USB port and Micro) USB plug connection type, without have mobile module on corresponding Micro is set)
USB port reduces influence of the installation flying power unit to 120 hardware of matrix.
Preferably, the end sides of matrix 120 are provided with electric connection contacts 122, groove or cavity inside be provided with
The 122 matched electric connecting sheet (not shown) of electric connection contacts.It is shown in Figure 4, when 120 end of matrix be inserted into groove or
When in cavity, the electric connection contacts 122 are contacted with electric connecting sheet, may be implemented between matrix 120 and flying power unit
Electric power and signal transmission.
In the present embodiment, the flying power unit includes shell 110, at least one rotor module 130, the shell
At least one flight cavity 140 for accommodating the rotor module 130 is provided on 110.The rotor module 130 is fixedly installed in
In the flight cavity 140, the flight cavity 140 can accommodate the rotor module 130 completely.
Preferably, the shell 110 is rectangular body case, and the flight cavity 140 is circular cylindrical cavity, each flight cavity
One rotor module 130 is set in body 140.
The rotor module 130 may include flying wing and flight dynamic devices.The flying wing can be used two rotors,
Three pieces rotor or four or more rotor.Piston type, electrodynamic type, vortex-spraying type, turbofan, whirlpool paddle can be used in the flight dynamic devices
Formula, punching type or jet-propelled, in the present embodiment, flight dynamic devices use electrodynamic type engine.It is preferred to be less than using height
Power plant of the brushless motor of 15mm as flying wing.The brushless motor is electrically connected with flight with accumulator, the electric power storage
Special power supply source of the pond as electro-motor.
It is also provided with switch button on the shell 110, switch button is controlling aforementioned brushless motor and battery
Unicom and disconnection.User can be started or closed to flying power unit by trigger switch button.
It by way of example and not limitation, can be by flying power list when user needs flight formula mobile phone to realize unmanned plane function
Member is mounted on mobile module (i.e. matrix), and the switch button then triggered on flying power unit is opened, and switch button is opened
When, the circuit communication of battery and brushless motor, brushless motor is started to work, and flying wing rotation, flying power unit is driven to drive
Mobile module takes off；When the task of flight formula mobile phone terminates or when not enough power supply, flight formula mobile phone is based on the spy in mobile module
Geodesic structure, can intelligently find user or default carrying structure, and land in user on hand or the carrying of default carrying structure
On platform, switch button that can also be on automatic trigger flying power unit after landing is closed, the circuit of battery and brushless motor
It disconnects.Certainly, in addition to aforesaid way, user can also start flight formula mobile phone by separately setting remote control, take off, fly
Row and landing control, aforementioned control mode should not be used as the limitation of the present embodiment.
Shown in Figure 5, in the present embodiment, each matrix 120 is collocated with 2 flying power units, each flying power
Unit includes shell 110, and 2 flight cavitys 140, and side setting and the matrix 120 of shell 110 are provided on shell 110
The installation interconnecting piece (not shown) of connection.
The flight cavity 140 includes the first cavity, the second cavity, and the first rotation is respectively arranged in the first, second cavity
Wing module and the second rotor module.In Fig. 5,2 flying power units are symmetricly set on the upper side and lower side of matrix 120.
Obviously, according to user's needs, 2 flying power units can also be symmetricly set on the left and right side of matrix 120, referring to
Shown in Fig. 6.
Described in Fig. 7, protective shell 150 is also provided on the flight cavity 140.The protective shell 150 is to engrave
Empty shell, the rotor module 130 are arranged in protective shell 150.Such structure can protect rotor module 130
Shield also avoids touching rotor when user is hand-held.Fig. 8 is the structural schematic diagram after protective shell 150 is installed on shell 110,
Rotor module 130 is protected in protective shell 150.
It should be pointed out that in the present embodiment, the quantity of each included rotor of rotor module can be the same or different,
The particular number of rotor can be that odd number may be even number, can need specifically to be arranged according to using.It is appreciated that
It is that when the identical setting of each rotor module, such structure is conducive to improve the stability during unmanned plane during flying；Meanwhile
The rotor module and rotor module of both sides setting can be symmetrical arranged about matrix, and the two forms symmetrical structure, and then can also carry
It soars line mobile phone flight stability.
It is illustrated so that Rotary-Wing Department includes four rotor modules as an example in embodiment, still, those skilled in the art answer
The understanding, the unmanned plane of the utility model are not limited to the structure of quadrotor module, and the number and arrangement form of rotor can roots
It is a kind of concrete form of the utility model, the structure for illustrating the utility model is not answered according to needing to be configured
It is construed as a limitation of the present invention.
Another embodiment of the utility model also discloses a kind of flying power unit.
Shown in Figure 9, the flying power unit includes shell 110, at least one rotor module 130, the shell
It is provided at least one flight cavity 140 for accommodating the rotor module 130 on 110, and is set in the side of the shell 110
Set installation interconnecting piece 111.It is additionally provided with protective shell 150 on the flight cavity 140.The protective shell 150 is the shell of hollow out,
The rotor module 130 is arranged in protective shell 150.Such structure can protect rotor module 130, also avoid
User touches rotor when hand-held.
By the installation interconnecting piece 111, flying power unit can be removably installed on intelligent mobile terminal.
In the present embodiment, after the flying power unit is installed on intelligent mobile terminal, pass through the installation interconnecting piece
Connection, the electric power between intelligent mobile terminal and flying power unit and signal transmission can be carried out.
Preferably, the installation interconnecting piece be and Micro) the matched plug of USB port, the installation interconnecting piece can insert
Enter the Micro on intelligent mobile terminal) in USB port, to which flying power unit is mounted on intelligent mobile terminal.It needs
When realizing flight function, flying power unit can be plugged on intelligent mobile terminal by user by installing interconnecting piece 111
Micro) on USB port, to form flight formula intelligent mobile terminal.Based on the Micro) USB port, the intelligent mobile
Electric power and signal transmission can be carried out between terminal and flying power unit.Specifically, such as by intelligent mobile terminal
Power supply is powered to flying power unit, and the flight parameter of flying power unit is for another example controlled by intelligent mobile terminal.
The intelligent mobile terminal can be mobile phone, tablet computer, wearable smart machine or laptop.
In addition to above structure, the installation interconnecting piece 111 can also be such as lower structure.Specifically, the installation interconnecting piece
For the groove or cavity on flying power unit, the inside dimension and intelligent mobile terminal end of the groove or cavity is arranged
Appearance and size matching so that the intelligent mobile terminal end nested can be mounted in the groove or cavity.In this way, can
By nested mounting means, intelligent mobile terminal and flying power unit to be attached by nested mode.Relative to
Micro) USB port and Micro) USB plug connection type, without on having intelligent mobile terminal setting it is corresponding
Micro) USB port reduces influence of the installation flying power unit to intelligent mobile terminal hardware.
Preferably, the end sides of intelligent mobile terminal are provided with electric connection contacts, are arranged in groove or cavity inside
Have and the matched electric connecting sheet of the electric connection contacts.It is described to be electrically connected when intelligent mobile terminal end is inserted into groove or cavity
Contact point is contacted with electric connecting sheet, and the electric power between intelligent mobile terminal and flying power unit and signal transmission may be implemented.
When needing further to control the flight parameter of flying power unit by intelligent mobile terminal, the intelligent mobile
Terminal is also correspondingly arranged on navigator fix structure, flight controller and gyroscope, navigator fix structure, flight controller and gyro
Instrument three communicates to connect.The communication connection can be wire communication connection, can also be wireless communication connection.
The navigator fix structure includes camera probe, ultrasonic probe, barometer, inertia survey meter, geomagnetic sensor
With it is one or more in height sonar meter.The flight controller can be passed with gyroscope, navigator fix structure into row information
It is defeated, and flying power unit is controlled according to the information of gyroscope and navigator fix structural transmission.
It should be noted that after the power connection is connect with installation interconnecting piece, the connection can be based on and realize matrix
Electric power and signal transmission between flying power unit are preferred modes, and described matrix is being connect with flying power unit
Afterwards, can also be simply to combine, and without electric power and signal transmission.By way of example and not limitation, such as it is described
Flying power unit electric power and signal control can be realized based on power source special and nonshared control unit.Specifically, can fly
On action edge unit be arranged flight accumulator, flight accumulator to flying power unit provide electric power.And special control
Device processed, for example can be unmanned controller in the prior art.Certainly, those skilled in the art will be appreciated that, matrix and flight
Realize that electric power and signal transmission are preferably modes after power unit connection.
Shown in Fig. 9, it is contemplated that installing the protection of interconnecting piece 111 and carrying the convenient of flying power unit
Property is additionally provided with extension and contraction control button 111a on the flying power unit, can be controlled by the extension and contraction control button 111a
System installation interconnecting piece 111 shrinks or stretches out relative to shell 110.
In the present embodiment, external camera settings are also provided on the shell 110.Preferably, the shell 110
Two external camera settings of forward and backward each setting, so may be implemented the pan-shot of front and back position.Further, described external to take the photograph
As structure may include left camera settings and right camera settings, left camera settings and right camera settings can coordinated operation it is real
Existing 3D shootings.The external camera settings can be installed by holder on shell.Can be directed to each camera settings when setting
A holder is respectively set to be controlled, can also be that same holder is arranged for multiple camera settings to be controlled.As act
Example and it is unrestricted, for example left camera settings are mounted on shell left by Zuoyun platform, and right camera settings are mounted on by right holder
Shell right.When shooting, by the Collaborative Control of left and right holder, left camera settings and right camera settings being capable of coordinated behaviour
Make, to realize that 3D is shot, to be similar to Prosthetic Hand and shoot structure.
In the above description, within the scope of the protection of goal of the utility model disclosure, each component can be with arbitrary
Number merges selectively and operatively, and each of these components part itself can also be implemented as hardware.In addition,
As the term of " comprising ", " including " and " having " should give tacit consent to it is being interpreted as including property or open, rather than it is exclusive
Property or closure, unless it is explicitly defined as opposite meaning.All technologies, science and technology or otherwise term all meet
Meaning understood by one of ordinary skill in the art, unless it is defined as opposite meaning.The public term found in dictionary is answered
It is not idealized very much or is impractically explained very much when under the background in the relevant technologies document, unless present disclosure is clearly limited
Determine at such.
Although describing the exemplary aspect of present disclosure for purposes of illustration, those skilled in the art should
, it is realized that foregoing description is only the description to the utility model preferred embodiment, not to any limit of the scope of the utility model
Fixed, the ranges of preferred embodiments of the present invention includes other realization, wherein the appearance or discussion can not be pressed
Sequence executes function.Any change, the modification that the those of ordinary skill in the utility model field does according to the disclosure above content,
Belong to the protection domain of claims.
Claims (11)
1. a kind of separation type flight formula mobile terminal, including matrix and flying power unit, it is characterised in that：Described matrix with fly
Action edge unit is separate structure, is provided with installation interconnecting piece on the flying power unit, is provided with and pacifies in described matrix
Flying power unit is removably installed by the matched power connection of load socket part by installing interconnecting piece and power connection
In on matrix.
2. flight formula mobile terminal according to claim 1, it is characterised in that：The mobile terminal is mobile phone, tablet electricity
Brain, wearable smart machine or laptop, described matrix include the processor being electrically connected, memory, communication module, display
Screen, power supply and camera settings.
3. separation type flight formula mobile terminal according to claim 1 or 2, it is characterised in that：Described matrix further includes leading to
Believe navigator fix structure, flight controller and the gyroscope of connection；
The navigator fix structure includes camera probe, ultrasonic probe, barometer, inertia survey meter, geomagnetic sensor and height
It spends one or more in sonar meter；
The flight controller is transmitted with gyroscope, navigator fix structure into row information, according to gyroscope and navigator fix structure
The information of transmission controls flying power unit.
4. separation type flight formula mobile terminal according to claim 1 or 2, it is characterised in that：The installation interconnecting piece is
The groove or cavity being arranged on flying power unit, using base end as power connection, the groove or cavity
Inside dimension is matched with the appearance and size of base end so that described matrix end nested can be mounted on the groove or cavity
It is interior.
5. separation type flight formula mobile terminal according to claim 1, it is characterised in that：The flying power unit includes
Shell, at least one rotor module are provided at least one flight cavity for accommodating the rotor module on the shell.
6. separation type flight formula mobile terminal according to claim 5, it is characterised in that：The shell is outside cuboid
Shell, the flight cavity are circular cylindrical cavity, and a rotor module is arranged in each flight cavity.
7. separation type flight formula mobile terminal according to claim 5, it is characterised in that：It is provided on the flight cavity
Protective shell, the protective shell are the shell of hollow out, and the rotor module is arranged in protective shell.
8. a kind of flying power unit, it is characterised in that：It is provided with installation interconnecting piece on the flying power unit, by described
Flying power unit can be removably installed on intelligent mobile terminal by installation interconnecting piece.
9. flying power unit according to claim 8, it is characterised in that：The flying power unit is installed on intelligent sliding
After in dynamic terminal, the electric power between intelligent mobile terminal and flying power unit and signal biography are carried out by the installation interconnecting piece
It is defeated.
10. flying power unit according to claim 8, it is characterised in that：The installation interconnecting piece is and Micro-USB
The plug of port match, the installation interconnecting piece are inserted into the ports Micro-USB on intelligent mobile terminal, to fly
Action edge unit is mounted on intelligent mobile terminal.
11. flying power unit according to claim 8, it is characterised in that：The flying power unit includes shell, extremely
Lack a rotor module, at least one flight cavity for accommodating the rotor module is provided on the shell, in the shell
Side setting installation interconnecting piece.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721648240.8U CN207658058U (en) | 2017-11-30 | 2017-11-30 | Separation type flight formula mobile terminal and its flying power unit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721648240.8U CN207658058U (en) | 2017-11-30 | 2017-11-30 | Separation type flight formula mobile terminal and its flying power unit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207658058U true CN207658058U (en) | 2018-07-27 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721648240.8U Active CN207658058U (en) | 2017-11-30 | 2017-11-30 | Separation type flight formula mobile terminal and its flying power unit |
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|---|---|
| CN (1) | CN207658058U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110191219A (en) * | 2019-04-26 | 2019-08-30 | 南京邮电大学 | Mobile phone shell |
-
2017
- 2017-11-30 CN CN201721648240.8U patent/CN207658058U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110191219A (en) * | 2019-04-26 | 2019-08-30 | 南京邮电大学 | Mobile phone shell |
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