CN106364680A - Battery compartment structure of multi-rotor unmanned aerial vehicle - Google Patents
Battery compartment structure of multi-rotor unmanned aerial vehicle Download PDFInfo
- Publication number
- CN106364680A CN106364680A CN201611024215.2A CN201611024215A CN106364680A CN 106364680 A CN106364680 A CN 106364680A CN 201611024215 A CN201611024215 A CN 201611024215A CN 106364680 A CN106364680 A CN 106364680A
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- cabin structure
- battery cabin
- rotor wing
- aerial vehicles
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 230000003014 reinforcing effect Effects 0.000 claims abstract description 7
- 230000002787 reinforcement Effects 0.000 claims description 11
- 230000005611 electricity Effects 0.000 claims description 3
- 210000003205 muscle Anatomy 0.000 claims 1
- 230000007547 defect Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000000630 rising effect Effects 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
- B64D29/00—Power-plant nacelles, fairings, or cowlings
- B64D29/04—Power-plant nacelles, fairings, or cowlings associated with fuselages
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Charge And Discharge Circuits For Batteries Or The Like (AREA)
Abstract
The invention discloses a battery compartment structure of a multi-rotor unmanned aerial vehicle. The battery compartment structure comprises a power plug, a battery compartment sliding groove and reinforcing ribs; the power plug is connected with a vehicle body plug of the multi-rotor unmanned aerial vehicle and used for providing power source power for the multi-rotor unmanned aerial vehicle; the battery compartment sliding groove is transversely arranged at the bottom of the battery compartment structure which is fixed to the battery compartment structure relatively through the battery compartment sliding groove; the reinforcing ribs are arranged on the top of the battery compartment structure and used for reinforcing the internal structure of the battery compartment structure.
Description
Technical field
The present invention relates to a kind of aviation aircraft technical field, the battery cabin structure of particularly a kind of many rotor wing unmanned aerial vehicles.
Background technology
Many rotor wing unmanned aerial vehicles are generally used for aviation target, battle reconnaissance, injure the military missions such as assessment, target guide, with
When can also be used for the non-military task such as flight test, aerial mapping, compared with for fixed-wing, many rotor wing unmanned aerial vehicles have vertical rising
The functions such as fall, hovering, can more flexibly execute task.Because the load of many rotor wing unmanned aerial vehicles is limited, therefore to fuselage
Structure and continuation of the journey have very high requirement, do not require nothing more than light weight, and require cruising time long.
The battery of many rotor wing unmanned aerial vehicles is located at unmanned aerial vehicle body, mainly provides power to aircraft it is ensured that aircraft can be effectively
Complete aerial mission.
Many rotor wing unmanned aerial vehicles battery flat mainly accommodates battery, and many rotor wing unmanned aerial vehicles species currently on the market is various, electricity
The design in pond cabin is very different, and most design all only takes into account fastening and the power supply of battery, and battery flat shape is all generally
Bulk, in flight course, resistance is big, and profile is ugly.And cruising time short it is impossible to complete aerial mission during long boat.Pass
The junction complex structure of the battery flat of system and aircraft is loaded down with trivial details, and changing battery wastes time and energy, and easily makes a slip-up, make in assembling process
Become serious consequence.
Thus, it is desirable to have a kind of battery cabin structure of many rotor wing unmanned aerial vehicles can overcome or at least mitigate the upper of prior art
State defect.
Content of the invention
The technical problem to be solved is to overcome defect present in above-mentioned prior art, and provides one kind many
The battery cabin structure of rotor wing unmanned aerial vehicle.
For solving above-mentioned technical problem, the battery cabin structure of a kind of many rotor wing unmanned aerial vehicles of the present invention, comprising: 1. a kind of many
The battery cabin structure of rotor wing unmanned aerial vehicle is it is characterised in that include: attaching plug, battery flat chute and reinforcement；
Attaching plug, described attaching plug connects the body plug of described many rotor wing unmanned aerial vehicles, for described many rotors
Unmanned plane provides mains power；
Battery flat chute, described battery flat chute is horizontally installed on the bottom of described battery cabin structure, described battery flat knot
Structure is relatively fixed with described many rotor wing unmanned aerial vehicles by described battery flat chute；
Reinforcement, described reinforcement is arranged on the top of described battery cabin structure, for reinforcing described battery cabin structure
Internal structure.
Preferably, the streamlined structure of top surface of described battery cabin structure, described streamlined structure makes described many
Rotor wing unmanned aerial vehicle reduces resistance in flight course.
Preferably, described battery cabin structure also includes: on and off switch and switch placing trough, and described on and off switch is fastened on institute
State in switch placing trough, described switch placing trough is arranged on the inner surface of described battery cabin structure, described on and off switch connects institute
State the battery in battery cabin structure to be used for controlling connection and the power-off of power supply.
The present invention provides a kind of battery cabin structure of many rotor wing unmanned aerial vehicles, and the battery cabin structure of described many rotor wing unmanned aerial vehicles is
Arc line shaped, the battery flat of arc line shaped can effectively reduce air drag during flight, and the battery of high power capacity can improve fly
During the boat of machine, long-time task can be more effectively completed.
Brief description:
Fig. 1 is the front view of the battery cabin structure of many rotor wing unmanned aerial vehicles.
Fig. 2 is the reinforcement schematic diagram of the battery cabin structure of many rotor wing unmanned aerial vehicles.
Fig. 3 is the schematic side view of the battery cabin structure of many rotor wing unmanned aerial vehicles.
Specific embodiment:
For making purpose, technical scheme and advantage that the present invention is implemented clearer, below in conjunction with the embodiment of the present invention
Accompanying drawing, the technical scheme in the embodiment of the present invention is further described in more detail.In the accompanying drawings, identical from start to finish or class
As the label element that represents same or similar element or there is same or like function.Described embodiment is the present invention
A part of embodiment, rather than whole embodiments.Embodiment below with reference to Description of Drawings is exemplary it is intended to use
In the explanation present invention, and it is not considered as limiting the invention.Based on the embodiment in the present invention, ordinary skill people
The every other embodiment that member is obtained under the premise of not making creative work, broadly falls into the scope of protection of the invention.Under
Face combines accompanying drawing and embodiments of the invention is described in detail.
In describing the invention it is to be understood that term " " center ", " longitudinal ", " horizontal ", "front", "rear",
The orientation of instruction such as "left", "right", " vertical ", " level ", " top ", " bottom " " interior ", " outward " or position relationship are based on accompanying drawing institute
The orientation showing or position relationship, are for only for ease of the description present invention and simplify description, rather than the dress of instruction or hint indication
Put or element must have specific orientation, with specific azimuth configuration and operation, therefore it is not intended that protecting to the present invention
The restriction of scope
The battery cabin structure of a kind of many rotor wing unmanned aerial vehicles according to the present invention one broad embodiment includes: attaching plug, electricity
Pond cabin chute and reinforcement；Described attaching plug connects the body plug of described many rotor wing unmanned aerial vehicles, for described many rotors
Unmanned plane provides mains power；Described battery flat chute is horizontally installed on the bottom of described battery cabin structure, described battery flat knot
Structure is relatively fixed with described many rotor wing unmanned aerial vehicles by described battery flat chute；Described reinforcement is arranged on described battery cabin structure
Top, for reinforcing the internal structure of described battery cabin structure.
As Figure 1-3, the battery cabin structure of many rotor wing unmanned aerial vehicles includes: on and off switch 1, attaching plug 3, battery flat are slided
Groove 4, reinforcement 5 and switch placing trough 6.
Described on and off switch 1 is fastened in described switch placing trough 6, and described switch placing trough 6 is arranged on described battery flat
The inner surface of structure, the battery that described on and off switch 1 connects in described battery cabin structure is used for controlling connection and the power-off of power supply.
Described attaching plug 3 connects the body plug of described many rotor wing unmanned aerial vehicles, for carrying to described many rotor wing unmanned aerial vehicles
Power supply driving source.
Described battery flat chute 4 is horizontally installed on the bottom of described battery cabin structure, and described battery cabin structure passes through described
Battery flat chute 4 is relatively fixed with described many rotor wing unmanned aerial vehicles.
Described reinforcement 5 is arranged on the top of described battery cabin structure, for reinforcing the internal junction of described battery cabin structure
Structure.
As Figure 1-3, the streamlined structure of top surface of described battery cabin structure, described streamlined structure makes institute
State many rotor wing unmanned aerial vehicles and reduce resistance in flight course.
3. the many rotor wing unmanned aerial vehicles according to claim 1 battery cabin structure it is characterised in that: described battery flat
Structure also includes: on and off switch and switch placing trough,
Above embodiments of the invention are described in detail, but described content have been only presently preferred embodiments of the present invention,
It is not to be regarded as the practical range for limiting the present invention.All impartial changes made according to the present patent application scope and improvement etc.,
All should still belong within the patent covering scope of the present invention.
Claims (3)
1. a kind of battery cabin structure of many rotor wing unmanned aerial vehicles is it is characterised in that include: attaching plug, battery flat chute and reinforcement
Muscle；
Attaching plug, described attaching plug connects the body plug of described many rotor wing unmanned aerial vehicles, for unmanned to described many rotors
Machine provides mains power；
Battery flat chute, described battery flat chute is horizontally installed on the bottom of described battery cabin structure, and described battery cabin structure leads to
Cross described battery flat chute to be relatively fixed with described many rotor wing unmanned aerial vehicles；
Reinforcement, described reinforcement is arranged on the top of described battery cabin structure, for reinforcing the inside of described battery cabin structure
Structure.
2. the many rotor wing unmanned aerial vehicles according to claim 1 battery cabin structure it is characterised in that: described battery cabin structure
The streamlined structure of top surface, described streamlined structure makes described many rotor wing unmanned aerial vehicles reduce resistance in flight course
Power.
3. the many rotor wing unmanned aerial vehicles according to claim 1 battery cabin structure it is characterised in that: described battery cabin structure
Also include on and off switch and switch placing trough, described on and off switch is fastened in described switch placing trough, described switch placing trough
It is arranged on the inner surface of described battery cabin structure, the battery that described on and off switch connects in described battery cabin structure is used for controlling electricity
The connection in source and power-off.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611024215.2A CN106364680A (en) | 2016-11-18 | 2016-11-18 | Battery compartment structure of multi-rotor unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611024215.2A CN106364680A (en) | 2016-11-18 | 2016-11-18 | Battery compartment structure of multi-rotor unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106364680A true CN106364680A (en) | 2017-02-01 |
Family
ID=57891802
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611024215.2A Pending CN106364680A (en) | 2016-11-18 | 2016-11-18 | Battery compartment structure of multi-rotor unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106364680A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106628105A (en) * | 2017-02-28 | 2017-05-10 | 天峋（常州）智能科技有限公司 | Unmanned aerial vehicle with rod-shaped plug batteries |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204998786U (en) * | 2015-08-06 | 2016-01-27 | 广州极飞电子科技有限公司 | Power module and unmanned aerial vehicle who has this power module |
| EP3040266A1 (en) * | 2014-12-30 | 2016-07-06 | Airbus Operations S.L. | Aircraft rear structure |
| CN205499323U (en) * | 2016-04-07 | 2016-08-24 | 珠海紫燕新科技有限公司 | Unmanned helicopter |
| CN106031318A (en) * | 2015-09-08 | 2016-10-12 | 深圳市大疆创新科技有限公司 | Mobile device, battery module thereof and locking device |
| CN206218240U (en) * | 2016-11-18 | 2017-06-06 | 天峋创新（北京）科技有限公司 | A kind of battery cabin structure of multi-rotor unmanned aerial vehicle |
-
2016
- 2016-11-18 CN CN201611024215.2A patent/CN106364680A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP3040266A1 (en) * | 2014-12-30 | 2016-07-06 | Airbus Operations S.L. | Aircraft rear structure |
| CN204998786U (en) * | 2015-08-06 | 2016-01-27 | 广州极飞电子科技有限公司 | Power module and unmanned aerial vehicle who has this power module |
| CN106031318A (en) * | 2015-09-08 | 2016-10-12 | 深圳市大疆创新科技有限公司 | Mobile device, battery module thereof and locking device |
| CN205499323U (en) * | 2016-04-07 | 2016-08-24 | 珠海紫燕新科技有限公司 | Unmanned helicopter |
| CN206218240U (en) * | 2016-11-18 | 2017-06-06 | 天峋创新（北京）科技有限公司 | A kind of battery cabin structure of multi-rotor unmanned aerial vehicle |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106628105A (en) * | 2017-02-28 | 2017-05-10 | 天峋（常州）智能科技有限公司 | Unmanned aerial vehicle with rod-shaped plug batteries |
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| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170201 |
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| RJ01 | Rejection of invention patent application after publication |