CN107117316B - A kind of detachable unmanned plane assisting in flying device - Google Patents
A kind of detachable unmanned plane assisting in flying device Download PDFInfo
- Publication number
- CN107117316B CN107117316B CN201710286088.1A CN201710286088A CN107117316B CN 107117316 B CN107117316 B CN 107117316B CN 201710286088 A CN201710286088 A CN 201710286088A CN 107117316 B CN107117316 B CN 107117316B
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- unmanned plane
- assembly
- quadrotor
- airborne platform
- detachable
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- 239000007787 solid Substances 0.000 claims description 37
- 230000008901 benefit Effects 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 3
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000005194 fractionation Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000004807 localization Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000002360 preparation method Methods 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D5/00—Aircraft transported by aircraft, e.g. for release or reberthing during flight
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
- B64U10/13—Flying platforms
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U80/00—Transport or storage specially adapted for UAVs
- B64U80/80—Transport or storage specially adapted for UAVs by vehicles
- B64U80/82—Airborne vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Transportation (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Accessories Of Cameras (AREA)
- Studio Devices (AREA)
Abstract
The present invention relates to a kind of detachable unmanned plane assisting in flying devices, the detachable unmanned plane assisting in flying device includes remote controler and quadrotor assembly, detachable unmanned plane assisting in flying device further includes detachable connector, airborne platform assembly and PTZ camera, airborne platform assembly connects quadrotor assembly by detachable connector, and PTZ camera is installed on quadrotor assembly bottom；Quadrotor assembly is used separately as unmanned plane or is integrally used as unmanned plane assisting in flying device after connecting with airborne platform assembly, when unmanned plane breaks down, is taken back ground as a kind of unmanned plane rescuing machine.Compared with prior art, the present invention have many advantages, such as it is detachable design, can not only be used for unmanned plane using also can be used as unmanned plane rescuing machine use, rescue it is highly-safe.
Description
Technical field
The present invention relates to a kind of rotor crafts, more particularly, to a kind of detachable unmanned plane assisting in flying device.
Background technique
Development of UAV is rapid, and various unmanned plane emerges one after another, but unmanned plane structure on market today, has a single function,
And lack a kind of unmanned vehicle can providing miscellaneous function for unmanned plane, serving unmanned plane.Existing unmanned plane there is also
Many technical problems, are listed below partial technical problems:
1, unmanned plane functional structure is single now.Existing unmanned plane structure, function are often relatively simple, mostly use integral type
Machine body assembly, design inflexible convenience.
2, unmanned plane cruising ability is insufficient now.Existing unmanned plane is due to the limitation of battery capacity, and cruising ability is often
It is unable to satisfy the requirement of most of user.
3, unmanned plane voyage is small now.Since cruising ability is insufficient or the limitation of remote signal reception and transmission range, so that existing
The voyage of modern unmanned plane is smaller.
4, unmanned plane is easy to happen air crash now.Because battery capacity is not enough to return the environment that can land, or because unmanned plane is sent out
Raw failure, can often cause aviation accident, even if existing part unmanned plane is equipped with the self-help apparatus such as parachute of saving oneself, but it is this
The mode of hard landing still can cause machine centainly to damage.
5, unmanned plane in some environments can not landing now.Existing unmanned plane is special in the water surface, muddy ground or no-fly zone
Under different environment, it can not freely take off, land, which greatly limits the application ranges of unmanned plane now.
Summary of the invention
It is an object of the present invention to overcome the above-mentioned drawbacks of the prior art and provide it is a kind of it is detachable nobody
Machine assisting in flying device.The aircraft takes detachable design, and complete function, flying quality is good, and cruising ability is strong, has filled up city
The vacancy of unmanned plane assisting in flying device on field.
The purpose of the present invention can be achieved through the following technical solutions:
A kind of detachable unmanned plane assisting in flying device, which includes remote controler and four
Rotor craft assembly, the detachable unmanned plane assisting in flying device further include that detachable connector, airborne platform are total
At and PTZ camera, the airborne platform assembly by detachable connector connect quadrotor assembly, it is described
PTZ camera be installed on quadrotor assembly bottom；
The quadrotor assembly uses separately as unmanned plane or integrally makees after connecting with airborne platform assembly
For the use of unmanned plane assisting in flying device, when unmanned plane breaks down, ground is taken back as a kind of unmanned plane rescuing machine.
The airborne platform assembly includes airborne platform rack, airborne platform lamp and solid mechanical arm module, described
Airborne platform rack is in the form of annular discs, and the airborne platform lamp is installed on airborne platform bracket edge, the solid mechanical arm
Module is installed on airborne platform upper rack.
The solid mechanical arm module includes solid mechanical arm and solid mechanical arm accumulator tank, the solid mechanical arm
In solid mechanical arm accumulator tank, the solid mechanical arm roots two sides are respectively equipped with shifting roller, the fixation machine
Tool arm accumulator tank both sides are respectively equipped with sliding slot, and the shifting roller is embedded in sliding slot.
The solid mechanical arm is translated in sliding slot by the shifting roller of its root and/or is carried out around its root
Rotation within the scope of 180 °.
The quadrotor assembly include quadrotor lamp, lifting support foot, brushless motor, propeller and
Quadrotor assembly rack, the lifting support foot are connected to quadrotor assembly bottom of the frame, and described four
The propeller that rotor craft assembly bottom of the frame edge is equipped with brushless motor and connect with brushless motor, four rotations
Rotor aircraft lamp is installed on quadrotor assembly frame edge.
The PTZ camera is installed on quadrotor assembly bottom of the frame.
The airborne platform frame central is equipped with infrared camera.
Power supply device is respectively equipped in the quadrotor assembly and airborne platform assembly, the quadrotor flies
Power supply device in row device assembly connects brushless motor, and the power supply device in the airborne platform assembly is connected and fixed machinery
Arm.
Compared with prior art, the invention has the following advantages that
1, the present invention can carry unmanned plane during flying, increase unmanned plane voyage；
2, the present invention can not be under the particular surroundings of landing, as a kind of mobile landing platform in unmanned plane；
3, the present invention can when unmanned plane not enough power supply is to make a return voyage or break down, as a kind of unmanned plane rescuing machine by its
Ground is taken back, and devises a kind of unique solid mechanical arm module, this specially designed solid mechanical arm module
Most of unmanned planes on market today can be fixed, effectively to guarantee the safety of rescue；
4, after the present invention separates airborne platform, quadrotor assembly can be used separately as unmanned plane of taking photo by plane；
5, the present invention can also carry usual articles, carry out air transport；
6, the present invention takes detachable design, and complete function, flying quality is good, and cruising ability is strong, has filled up in the market
The vacancy of unmanned plane assisting in flying device.
Detailed description of the invention
Fig. 1 is schematic perspective view when the detachable unmanned plane assisting in flying device solid mechanical arm of the present invention is packed up；
Fig. 2 is stereochemical structure signal when the detachable unmanned plane assisting in flying device solid mechanical arm of the present invention is fully deployed
Figure；
Fig. 3 is stereochemical structure signal when the detachable unmanned plane assisting in flying device solid mechanical arm of the present invention shrinks fixed
Figure；
Fig. 4 is the airborne platform assembly of the detachable unmanned plane assisting in flying device of the present invention from quadrotor assembly
Schematic perspective view when separating；
Fig. 5 is when the solid mechanical arm of the airborne platform assembly of the detachable unmanned plane assisting in flying device of the present invention is packed up
Overlooking structure diagram；
Fig. 6 is the overlooking structure diagram of the detachable unmanned plane assisting in flying device quadrotor assembly of the present invention；
Fig. 7 is the schematic perspective view of the detachable unmanned plane assisting in flying device quadrotor assembly of the present invention；
Fig. 8 is the stereochemical structure principle signal of the mechanical arm fixed module of the detachable unmanned plane assisting in flying device of the present invention
Figure；
Fig. 9 is the schematic perspective view of the detachable unmanned plane assisting in flying device remote controler of the present invention；
Figure 10 is the schematic perspective view of the detachable unmanned plane assisting in flying device of the present invention；
Wherein, 1, solid mechanical arm, 2, solid mechanical arm accumulator tank, 3, shifting roller, 4, sliding slot, 5, airborne platform lamp,
6, detachable connector, 7, infrared camera, 8, lifting support foot, 9, PTZ camera, 10, propeller, 11, airborne platform
Assembly, 12, quadrotor lamp, 13, quadrotor assembly, 14, brushless motor, 15, remote controler.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiment is a part of the embodiments of the present invention, rather than whole embodiments.Based on this hair
Embodiment in bright, those of ordinary skill in the art's every other reality obtained without making creative work
Example is applied, all should belong to the scope of protection of the invention.
Embodiment
As shown in Fig. 1-Figure 10, detachable unmanned plane assisting in flying device, including remote controler 15, airborne platform assembly 11,
Quadrotor assembly 13 and detachable connector 6, airborne platform assembly 11 and quadrotor assembly 13 pass through can
Breakaway connector 6 is connected, and airborne platform assembly 11 includes airborne platform rack, airborne platform lamp 5 and solid mechanical arm mould
Block, airborne platform rack is in the form of annular discs, and airborne platform lamp 5 is installed on airborne platform bracket edge, the installation of solid mechanical arm module
In airborne platform upper rack.Solid mechanical arm module includes solid mechanical arm 1, solid mechanical arm accumulator tank 2, sliding slot 4 and moves
Dynamic idler wheel 3, as shown in figure 5, solid mechanical arm 1 is located in solid mechanical arm accumulator tank 2,1 root two sides of solid mechanical arm difference
Equipped with shifting roller 3,2 both sides of solid mechanical arm accumulator tank are respectively equipped with sliding slot 4, and shifting roller 3 is embedded in sliding slot 4.Such as Fig. 7 institute
Show, 13 bottom of quadrotor assembly is equipped with PTZ camera 9.To realize multi-functional requirement and providing auxiliary for unmanned plane
Service, quadrotor assembly 13 include quadrotor lamp 12, lifting support foot 8, brushless motor 14,10 and of propeller
Quadrotor assembly rack, lifting support foot 8 are connected to quadrotor assembly bottom of the frame, and quadrotor is total
Brushless motor 14 and the propeller connecting with brushless motor 10 are installed at bottom of the frame edge, quadrotor lamp 12 is pacified
Loaded on quadrotor assembly frame edge.It, can be only after quadrotor assembly 13 is separated with airborne platform assembly 11
It is vertical to be used as unmanned plane of taking photo by plane.
Remote controler schematic diagram is as shown in figure 9, operator controls quadrotor assembly by remote controler 15 on ground
The revolving speed of brushless motor 14 and propeller 10 in 13 realizes the free flight of rotor craft assembly 13, can on remote controler 15
It shows instant picture captured by PTZ camera 9, realizes aerial photography function.
As shown in Fig. 2, shifting roller 3 rotates 180 °, fixes when a kind of present invention landing platform mobile as unmanned plane
Mechanical arm 1 is in fully unfolded position, provides flat plateau for unmanned plane landing.Mechanical arm is as shown in Figure 3 when shrinking fixed.Such as
Shown in Fig. 4, after airborne platform assembly 11, detachable connector 6 are separated with quadrotor assembly 13, quadrotor flight
Device assembly 13 can be used separately as unmanned plane of taking photo by plane.Airborne platform assembly 11 and quadrotor assembly 13 can be individually
It charges, whole charging is carried out after can also connecting with detachable connector 6.
The expansion degree to solid mechanical arm 1 is realized in movement of the shifting roller 3 in sliding slot 4 in airborne platform assembly 11
With the control of displacement, on airborne platform assembly 11 unmanned plane or other articles be fixed, can be shown on remote controler 15
Instant picture captured by infrared camera 7 sees the environment of 11 top of airborne platform assembly clearly convenient for operator, and the present invention was both
Automatic localization capture can be carried out to UAV targets according to the real time positioning data of UAV targets, it can also be by operator
Member's manual operation, captures other articles, fixed effect is as shown in Figure 3 manually.
As shown in Figure 5 and Figure 6, airborne platform lamp 5 and quadrotor lamp 12 can in the environment of insufficient light, as
Searchlight and highlighting lamp use.
As shown in figure 8, airborne platform frame central is additionally provided with infrared camera 7.
Concrete operating principle:
Detachable unmanned plane assisting in flying device in the present invention, when if desired carrying out emergency relief to certain unmanned plane, benefit
Start aircraft with remote controler 15, arrival need to rescue below unmanned plane, the position of solid mechanical arm 1 be controlled, so that solid mechanical
Arm 1 can block unmanned plane to be rescued lifting support foot or uav bottom to be rescued, so that unmanned plane to be rescued is fixed on
11 top of airborne platform assembly, and aircraft landing is controlled, complete rescue.When airborne platform assembly 11 and quadrotor are total
When at 13 separation, quadrotor assembly 13 carries out solo hop under the control of remote controler 15.
The present invention can provide many miscellaneous functions for unmanned plane now, can carry unmanned plane during flying, increase its voyage；It can be
Unmanned plane can not be under the particular surroundings of landing, the landing platform as a kind of movement；In unmanned plane not enough power supply to make a return voyage or send out
When raw failure, it can be used as a kind of unmanned plane rescuing machine and taken back ground.The present invention can also carry usual articles, be transported in the air
Defeated, the quadrotor assembly after fractionation can also be used separately as unmanned plane of taking photo by plane.The present invention takes detachable design,
It is multiple functional, and filled up the vacancy of unmanned plane assisting in flying device in the market.
The above description is merely a specific embodiment, but scope of protection of the present invention is not limited thereto, any
Those familiar with the art in the technical scope disclosed by the present invention, can readily occur in various equivalent modifications or replace
It changes, these modifications or substitutions should be covered by the protection scope of the present invention.Therefore, protection scope of the present invention should be with right
It is required that protection scope subject to.
Claims (6)
1. a kind of detachable unmanned plane assisting in flying device, the detachable unmanned plane assisting in flying device include remote controler (15) and
Quadrotor assembly (13), which is characterized in that the detachable unmanned plane assisting in flying device further includes detachable
Connector (6), airborne platform assembly (11) and PTZ camera (9), the airborne platform assembly (11) pass through detachable
Connector (6) connects quadrotor assembly (13), and the PTZ camera (9) is installed on quadrotor assembly
(13) bottom；
The quadrotor assembly use separately as unmanned plane or connect with airborne platform assembly after integrally as nothing
Man-machine assisting in flying device uses, and when unmanned plane breaks down, is taken back ground as a kind of unmanned plane rescuing machine；
The airborne platform assembly (11) includes airborne platform rack, airborne platform lamp (5) and solid mechanical arm module, described
Airborne platform rack it is in the form of annular discs, the airborne platform lamp (5) is installed on airborne platform bracket edge, the fixation machine
Tool arm module is installed on airborne platform upper rack；
The solid mechanical arm module includes solid mechanical arm (1) and solid mechanical arm accumulator tank (2), the solid mechanical
Arm (1) is located in solid mechanical arm accumulator tank (2), and described solid mechanical arm (1) the root two sides are respectively equipped with shifting roller
(3), described solid mechanical arm accumulator tank (2) both sides are respectively equipped with sliding slot (4), and the shifting roller (3) is embedded in sliding slot (4)
It is interior.
2. a kind of detachable unmanned plane assisting in flying device according to claim 1, which is characterized in that the fixation machine
Tool arm (1) is translated in sliding slot by the shifting roller of its root and/or carries out the rotation within the scope of 180 ° around its root.
3. a kind of detachable unmanned plane assisting in flying device according to claim 1, which is characterized in that the quadrotor
Aircraft assembly (13) include quadrotor lamp (12), lifting support foot (8), brushless motor (14), propeller (10) and
Quadrotor assembly rack, the lifting support foot (8) is connected to quadrotor assembly bottom of the frame, described
The propeller (10) that quadrotor assembly bottom of the frame edge is equipped with brushless motor (14) and connect with brushless motor,
The quadrotor lamp (12) is installed on quadrotor assembly frame edge.
4. a kind of detachable unmanned plane assisting in flying device according to claim 3, which is characterized in that the holder is taken the photograph
Camera (9) is installed on quadrotor assembly bottom of the frame.
5. a kind of detachable unmanned plane assisting in flying device according to claim 1, which is characterized in that described is airborne flat
Platform frame central is equipped with infrared camera (7).
6. a kind of detachable unmanned plane assisting in flying device according to claim 3, which is characterized in that the quadrotor
Power supply device is respectively equipped in aircraft assembly (13) and airborne platform assembly (11), in the quadrotor assembly
Power supply device connects brushless motor, and the power supply device in the airborne platform assembly is connected and fixed mechanical arm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710286088.1A CN107117316B (en) | 2017-04-27 | 2017-04-27 | A kind of detachable unmanned plane assisting in flying device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710286088.1A CN107117316B (en) | 2017-04-27 | 2017-04-27 | A kind of detachable unmanned plane assisting in flying device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107117316A CN107117316A (en) | 2017-09-01 |
| CN107117316B true CN107117316B (en) | 2019-06-11 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201710286088.1A Active CN107117316B (en) | 2017-04-27 | 2017-04-27 | A kind of detachable unmanned plane assisting in flying device |
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Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108674644B (en) * | 2018-05-21 | 2021-06-29 | 西北工业大学明德学院 | Many rotor crafts with auxiliary aircraft |
| CN108873941A (en) * | 2018-08-29 | 2018-11-23 | 芜湖翼讯飞行智能装备有限公司 | Automatic cover control device and its application method in UAV Formation Flight |
| CN109229351B (en) * | 2018-09-11 | 2021-08-20 | 陕西汇成天云智能科技有限公司 | Utilize four rotor unmanned aerial vehicle of additional rotor heavy sensing self-sustaining weighing apparatus |
| CN110217373A (en) * | 2019-06-20 | 2019-09-10 | 金陵科技学院 | A kind of solar energy floating airplane parking area and mating single blade unmanned plane |
| CN113602495A (en) * | 2021-08-30 | 2021-11-05 | 复旦大学 | Platform device supporting multi-rotor unmanned aerial vehicle to take off and land in air |
| CN116736892B (en) * | 2023-08-15 | 2023-12-08 | 中国兵器装备集团兵器装备研究所 | Method and system for mutual aid return of flight equipment |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5000398A (en) * | 1988-10-25 | 1991-03-19 | Rashev Michael S | Flying multi-purpose aircraft carrier and method of V/STOL assisted flight |
| CN106005400A (en) * | 2016-07-13 | 2016-10-12 | 绵阳空天科技有限公司 | Vertical-takeoff auxiliary system for fixed-wing aircraft |
| CN106043689A (en) * | 2016-07-22 | 2016-10-26 | 绵阳空天科技有限公司 | Vertical take-off auxiliary system for top-mounted fixed-wing aircraft |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8950698B1 (en) * | 2012-10-26 | 2015-02-10 | The Boeing Company | Convertible compounded rotorcraft |
-
2017
- 2017-04-27 CN CN201710286088.1A patent/CN107117316B/en active Active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5000398A (en) * | 1988-10-25 | 1991-03-19 | Rashev Michael S | Flying multi-purpose aircraft carrier and method of V/STOL assisted flight |
| CN106005400A (en) * | 2016-07-13 | 2016-10-12 | 绵阳空天科技有限公司 | Vertical-takeoff auxiliary system for fixed-wing aircraft |
| CN106043689A (en) * | 2016-07-22 | 2016-10-26 | 绵阳空天科技有限公司 | Vertical take-off auxiliary system for top-mounted fixed-wing aircraft |
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| Publication number | Publication date |
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| CN107117316A (en) | 2017-09-01 |
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