CN204871594U - Set up unmanned vehicles of removable battery in undercarriage - Google Patents
Set up unmanned vehicles of removable battery in undercarriage Download PDFInfo
- Publication number
- CN204871594U CN204871594U CN201520396630.5U CN201520396630U CN204871594U CN 204871594 U CN204871594 U CN 204871594U CN 201520396630 U CN201520396630 U CN 201520396630U CN 204871594 U CN204871594 U CN 204871594U
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- China
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- battery
- battery compartment
- alighting gear
- aircraft body
- unmanned vehicle
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Abstract
The utility model relates to a set up unmanned vehicles of removable battery in undercarriage, have including the aircraft main part, with aircraft main part fixed connection's rotor arm, on locating the rotor arm impeller blade the motor, locate aircraft main part bottom and this aircraft main part fixed connection's undercarriage, a plurality of supports of constitution undercarriage be hollow structure, hollow support in be provided with the battery compartment, but be equipped with in every battery compartment and be used for the connector be connected with rechargeable lithium -ion battery, this connector is inside through cable conductor and the shell of locating the aircraft main part, have the power input electrode who establishes on control circuit's the circuit board and connect, the support as the battery compartment on be equipped with the battery compartment opening that is used for changing the battery, every battery compartment opening to should have the matched with battery cover with the sealed cooperation of battery compartment opening, the utility model discloses an aircraft can not cause the not hard up of main body cover combination department, avoids relative more expensive main body cover to take place to damage, increases the unmanned vehicles flight stability because of reducing simultaneously the focus again.
Description
Technical field
The utility model relates to a kind of rotor unmanned aircraft, particularly relates to that a kind of alighting gear arranges can the unmanned vehicle of quick-replaceable battery.
Background technology
Unmanned vehicle is many rotor unmanned aircrafts particularly, usually be all adopt rechargeable lithium cell to carry out work as the energy driven, although technology and the performance of the chargeable lithium cell of current use are greatly improved, but often the secondary electricity that is full of all needs to expend the more time, the fastest also needs similar 1 hour, therefore when using these unmanned vehicles, the more time is often needed to charge, just need to use polylith lithium cell to change, the lithium cell of current unmanned vehicle is normally arranged in the body housing of unmanned vehicle, the shell opening aircraft body is all needed when each replacing, the combination between the shell of unmanned vehicle and aircraft body is not only easily caused easily to get loose, and be arranged in aircraft body due to battery, the center of gravity of unmanned vehicle can be caused higher, this can cause unmanned vehicle attitude in the process of flight to be difficult to control, in the weather of strong wind, the flight attitude of unmanned vehicle also can be caused to overturn, the unfavorable stability with unmanned vehicle.
Utility model content
The utility model is to solve above-mentioned technical matters, is convenient to dismantle and underslung unmanned plane with unmanned plane in the alighting gear providing a kind of battery to be fixed on unmanned vehicle.
The utility model adopts following technical scheme: the unmanned vehicle arranging replaceable battery in this alighting gear, comprise aircraft body, the rotor arm be fixedly connected with aircraft body, be located at the motor with impeller blade on rotor arm, be located at the alighting gear be fixedly connected with this aircraft body bottom aircraft body, multiple supports of described composition alighting gear are the structure of hollow, battery compartment is provided with in the support of described hollow, the adaptor union for being connected with chargeable lithium cell is provided with in each battery compartment, this adaptor union is by cable and the enclosure being located at aircraft body, connect with power supply input electrode set on the circuit card of control circuit, the described support as battery compartment is provided with the battery compartment opening for changing battery, each battery compartment opening is sealed and matched to having the battery cover that matches and described battery compartment opening.
Arrange in alighting gear of the present utility model in the unmanned vehicle of replaceable battery, the cable of described connection bracket female connector, through the perforate of junction in the internal stent space of hollow and support and aircraft body shell, be connected with aircraft body shell interior circuit board power source input electrode.
Arrange in alighting gear of the present utility model in the unmanned vehicle of replaceable battery, the support of described formation alighting gear, comprise the landing bar of vertical strut bar and level, described battery compartment is located in landing bar.
Arrange in alighting gear of the present utility model in the unmanned vehicle of replaceable battery, described battery cover is sealed and matched by screw and described battery compartment opening.
Arrange in alighting gear of the present utility model in the unmanned vehicle of replaceable battery, the cross sectional shape of the hollow of the support of described formation alighting gear is oval annular.
Useful effect: owing to adopting above-mentioned technical scheme, the unmanned vehicle of replaceable battery is set in alighting gear of the present utility model, when battery changed by needs, the battery cover can opening the battery compartment place on arm is easily changed, relatively there is the shell of the main body opening unmanned vehicle, not only convenient and also can not cause main body cover junction loosen, relatively expensive main body cover is avoided to be damaged, because can lower the center of gravity again simultaneously, formula unmanned vehicle flight attitude is more stable, is convenient to operator and manipulates.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the utility model is described in further detail.
Fig. 1, front view for a kind of embodiment of aircraft of the present utility model;
Fig. 2, lateral plan for a kind of embodiment of aircraft of the present utility model.
Detailed description of the invention
Please refer to shown in Fig. 1 and Fig. 2, for arranging the structural representation of a kind of embodiment of the unmanned vehicle of replaceable battery in alighting gear of the present utility model, the unmanned vehicle of replaceable battery is set in this alighting gear, comprise aircraft body 1, the rotor arm 2 be fixedly connected with aircraft body 1, be located at the motor with impeller blade on rotor arm, be located at the alighting gear be fixedly connected with this aircraft body bottom aircraft body, multiple supports of described composition alighting gear are the structure of hollow, battery compartment is provided with in the support of described hollow, the adaptor union for being connected with chargeable lithium cell 9 is provided with in each battery compartment, this adaptor union is by cable 15 and the enclosure being located at aircraft body, connect with power supply input electrode set on the circuit card of control circuit, the described support as battery compartment is provided with the battery compartment opening for changing battery, each battery compartment opening is sealed and matched with described battery compartment opening to there being the battery cover 15 matched.
Further, the cable of described connection bracket female connector, through the perforate of junction in the internal stent space of hollow and support and aircraft body shell, is connected with aircraft body shell interior circuit board power source input electrode.
Further, the support of described formation alighting gear, comprises vertical strut bar 10 and the landing bar 12 of level, and described battery compartment is located in landing bar.
Further, described battery cover is sealed and matched by screw and described battery compartment opening.
Further, the cross sectional shape of the hollow of the support of described formation alighting gear is oval annular, owing to adopting above-mentioned technical scheme, the unmanned vehicle of replaceable battery is set in alighting gear of the present utility model, when battery changed by needs, the battery compartment place battery cover can opened easily on arm is changed, relatively there is the shell of the main body opening unmanned vehicle, not only convenient and also can not cause main body cover junction loosen, relatively expensive main body cover is avoided to be damaged, because can lower the center of gravity again simultaneously, formula unmanned vehicle flight attitude is more stable, be convenient to operator manipulate.
Claims (5)
1. the unmanned vehicle of replaceable battery is set in alighting gear, comprise aircraft body, the rotor arm be fixedly connected with aircraft body, be located at the motor with impeller blade on rotor arm, be located at the alighting gear be fixedly connected with this aircraft body bottom aircraft body, it is characterized in that: multiple supports of described composition alighting gear are the structure of hollow, battery compartment is provided with in the support of this hollow, the adaptor union for being connected with chargeable lithium cell is provided with in each battery compartment, described adaptor union is connected with power supply input electrode set on the circuit card of control circuit with the enclosure being located at aircraft body by cable, this support as battery compartment is provided with the battery compartment opening for changing battery, each battery compartment opening is sealed and matched to having the battery cover that matches and described battery compartment opening.
2. the unmanned vehicle of replaceable battery is set in alighting gear as claimed in claim 1, it is characterized in that: the cable of described connection bracket female connector, through the perforate of junction in the internal stent space of hollow and support and aircraft body shell, be connected with aircraft body shell interior circuit board power source input electrode.
3. arrange the unmanned vehicle of replaceable battery in alighting gear as claimed in claim 1, it is characterized in that the support of described composition alighting gear includes the landing bar of vertical strut bar and level, described battery compartment is located in landing bar.
4. the unmanned vehicle of replaceable battery is set in alighting gear as claimed in claim 1, it is characterized in that: described battery cover is sealed and matched by screw and described battery compartment opening.
5. the unmanned vehicle of replaceable battery is set in alighting gear as claimed in claim 1, it is characterized in that the cross sectional shape of the hollow of the support of described composition alighting gear is oval annular.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520396630.5U CN204871594U (en) | 2015-06-10 | 2015-06-10 | Set up unmanned vehicles of removable battery in undercarriage |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520396630.5U CN204871594U (en) | 2015-06-10 | 2015-06-10 | Set up unmanned vehicles of removable battery in undercarriage |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204871594U true CN204871594U (en) | 2015-12-16 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520396630.5U Expired - Fee Related CN204871594U (en) | 2015-06-10 | 2015-06-10 | Set up unmanned vehicles of removable battery in undercarriage |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204871594U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108146404A (en) * | 2016-12-02 | 2018-06-12 | 成都天府新区光启未来技术研究院 | The replacement system and method and unmanned plane of unmanned machine battery |
| CN110155312A (en) * | 2019-05-13 | 2019-08-23 | 之江实验室 | A kind of battery compartment of more rotor manned aircraft and manned vehicle comprising the battery compartment |
| CN110475719A (en) * | 2017-04-07 | 2019-11-19 | 马克·H·汉纳 | Distributed battery aircraft and its method of supplying power to |
| CN111204450A (en) * | 2020-04-23 | 2020-05-29 | 北京智芯微电子科技有限公司 | Unmanned aerial vehicle undercarriage and unmanned aerial vehicle |
| US20210323619A1 (en) * | 2020-04-16 | 2021-10-21 | Korea Advanced Institute Of Science And Technology | Wall-climbing drone using auxiliary arm and method for controlling therefor |
-
2015
- 2015-06-10 CN CN201520396630.5U patent/CN204871594U/en not_active Expired - Fee Related
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108146404A (en) * | 2016-12-02 | 2018-06-12 | 成都天府新区光启未来技术研究院 | The replacement system and method and unmanned plane of unmanned machine battery |
| CN108146404B (en) * | 2016-12-02 | 2024-04-02 | 成都天府新区光启未来技术研究院 | Unmanned aerial vehicle battery replacement system and method and unmanned aerial vehicle |
| CN110475719A (en) * | 2017-04-07 | 2019-11-19 | 马克·H·汉纳 | Distributed battery aircraft and its method of supplying power to |
| US11811224B2 (en) | 2017-04-07 | 2023-11-07 | Mark Holbrook Hanna | Distributed-battery aerial vehicle and a powering method therefor |
| CN110155312A (en) * | 2019-05-13 | 2019-08-23 | 之江实验室 | A kind of battery compartment of more rotor manned aircraft and manned vehicle comprising the battery compartment |
| CN110155312B (en) * | 2019-05-13 | 2024-04-09 | 之江实验室 | Battery compartment of multi-rotor manned aircraft and manned aircraft comprising battery compartment |
| US20210323619A1 (en) * | 2020-04-16 | 2021-10-21 | Korea Advanced Institute Of Science And Technology | Wall-climbing drone using auxiliary arm and method for controlling therefor |
| CN111204450A (en) * | 2020-04-23 | 2020-05-29 | 北京智芯微电子科技有限公司 | Unmanned aerial vehicle undercarriage and unmanned aerial vehicle |
| WO2021212633A1 (en) * | 2020-04-23 | 2021-10-28 | 北京智芯微电子科技有限公司 | Unmanned aerial vehicle undercarriage, and unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151216 Termination date: 20170610 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |