CN215622660U - Unmanned aerial vehicle undercarriage for remote sensing measurement - Google Patents
Unmanned aerial vehicle undercarriage for remote sensing measurement Download PDFInfo
- Publication number
- CN215622660U CN215622660U CN202122034925.6U CN202122034925U CN215622660U CN 215622660 U CN215622660 U CN 215622660U CN 202122034925 U CN202122034925 U CN 202122034925U CN 215622660 U CN215622660 U CN 215622660U
- Authority
- CN
- China
- Prior art keywords
- unmanned aerial
- aerial vehicle
- vehicle undercarriage
- cavity
- undercarriage
- 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.)
- Expired - Fee Related
Links
- 238000005259 measurement Methods 0.000 title claims abstract description 9
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 claims description 6
- 229910052744 lithium Inorganic materials 0.000 claims description 6
- 238000009434 installation Methods 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 3
- 238000004134 energy conservation Methods 0.000 abstract description 2
- 230000007613 environmental effect Effects 0.000 abstract description 2
- 238000006243 chemical reaction Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000002035 prolonged effect Effects 0.000 description 3
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Images
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Photovoltaic Devices (AREA)
Abstract
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle undercarriage for remote sensing measurement, which comprises a U-shaped unmanned aerial vehicle undercarriage, wherein two ends of the U-shaped unmanned aerial vehicle undercarriage are symmetrically provided with support rods, a cavity is arranged on the end surface of the U-shaped unmanned aerial vehicle undercarriage, a storage battery is arranged in the cavity, an inverter is arranged at one side of the storage battery and positioned in the cavity, and two groups of mounting brackets are symmetrically arranged on the side wall of the U-shaped unmanned aerial vehicle undercarriage along the length direction of the cavity. Therefore, the long-time endurance can meet the working requirement, and the effects of energy conservation and environmental protection are achieved.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle undercarriage for remote sensing measurement.
Background
The unmanned aircraft is an unmanned aircraft operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer, the existing remote sensing measurement unmanned aircraft landing gear only has the function of supporting the unmanned aircraft, and meanwhile, the unmanned aircraft adopts a charging mode to charge a lithium battery arranged in the unmanned aircraft to provide electric energy for the unmanned aircraft, so that the electric energy stored in the lithium battery in the unmanned aircraft is limited, the endurance capacity of the unmanned aircraft is limited, and the long-time endurance cannot be realized to meet the working requirement.
In conclusion, the unmanned aerial vehicle undercarriage for remote sensing measurement is designed to solve the existing problems.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide an unmanned aerial vehicle undercarriage for remote sensing measurement, which aims to solve the problems in the background technology.
In order to achieve the purpose, the utility model provides the following technical scheme:
the utility model provides an unmanned aerial vehicle undercarriage that remote sensing was measured, includes U type unmanned aerial vehicle undercarriage, the both ends symmetry of U type unmanned aerial vehicle undercarriage is provided with the bracing piece, be provided with the cavity on the terminal surface of U type unmanned aerial vehicle undercarriage, the inside of cavity is provided with the battery, one side of battery is and the inside that is located the cavity is provided with the dc-to-ac converter, the lateral wall of U type unmanned aerial vehicle undercarriage and the length direction symmetry along the cavity are provided with two sets of installing supports, the panel mounting groove has been seted up to the left and right sides lateral wall symmetry of U type unmanned aerial vehicle undercarriage, the internally mounted of panel mounting groove has solar cell panel.
In a preferred embodiment of the present invention, the storage battery is a rechargeable lithium battery, and the storage battery is connected to the inverter through a wire and is electrically connected.
As a preferable aspect of the present invention, the inverter is connected to the solar cell panel by a wire, and the connection mode is an electrical connection.
As the preferable scheme of the utility model, the U-shaped unmanned aerial vehicle undercarriage and the supporting rod are vertically arranged, and the supporting rod is of a hollow structure.
According to the preferable scheme, the U-shaped unmanned aerial vehicle undercarriage and the two groups of mounting brackets are integrally formed, mounting threaded holes are formed in the two groups of mounting brackets, and the storage battery is connected to a main control board of the unmanned aerial vehicle through a lead.
Compared with the prior art, the utility model has the beneficial effects that:
1. according to the unmanned aerial vehicle undercarriage, the two groups of solar panels are arranged on the unmanned aerial vehicle undercarriage, the solar panels absorb solar energy, convert the solar energy into electric energy, convert the converted electric energy into the electric energy through the inverter and store the electric energy into the storage battery, and provide the electric energy for the unmanned aerial vehicle, so that the endurance time of the unmanned aerial vehicle is prolonged, the long-time endurance can be realized, the working requirement can be met, the solar energy is converted into the electric energy, and the effects of energy conservation and environmental protection are achieved.
2. According to the utility model, the supporting rod is designed to be of a hollow structure, so that the weight of the unmanned aircraft is integrally reduced, and the endurance time of the unmanned aircraft is indirectly prolonged.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic view of a portion of the structure of FIG. 1 according to the present invention.
In the figure: 1. a U-shaped unmanned aerial vehicle undercarriage; 2. a support bar; 3. a cavity; 4. a storage battery; 5. an inverter; 6. mounting a bracket; 7. a battery plate mounting groove; 8. a solar cell panel.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, rather than all embodiments, and all other embodiments obtained by a person of ordinary skill in the art without any creative work based on the embodiments of the present invention belong to the protection scope of the present invention.
While several embodiments of the present invention will be described more fully hereinafter with reference to the accompanying drawings, in order to facilitate an understanding of the utility model, the utility model may be embodied in many different forms and should not be construed as limited to the embodiments set forth herein, but rather should be construed to provide a more complete disclosure of the utility model.
It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may also be present, that when an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may also be present, and that the terms "vertical", "horizontal", "left", "right" and the like are used herein for descriptive purposes only.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs, and the terms used herein in the specification of the present invention are for the purpose of describing particular embodiments only and are not intended to limit the present invention, and the term "and/or" as used herein includes any and all combinations of one or more of the associated listed items.
Referring to fig. 1-2, the present invention provides a technical solution:
the utility model provides an unmanned aerial vehicle undercarriage for remote sensing measurement, including U type unmanned aerial vehicle undercarriage 1, the both ends symmetry of U type unmanned aerial vehicle undercarriage 1 is provided with bracing piece 2, be provided with cavity 3 on U type unmanned aerial vehicle undercarriage 1's the terminal surface, the inside of cavity 3 is provided with battery 4, one side of battery 4 is and the inside that is located cavity 3 is provided with dc-to-ac converter 5, U type unmanned aerial vehicle undercarriage 1's lateral wall and be provided with two sets of installing supports 6 along cavity 3's length direction symmetry, panel mounting groove 7 has been seted up to the left and right sides lateral wall symmetry of U type unmanned aerial vehicle undercarriage 1, the internally mounted of panel mounting groove 7 has solar cell panel 8.
As a further preferable mode of the present invention, the storage battery 4 is a rechargeable lithium battery, and the storage battery 4 is connected to the inverter 5 by a wire and is electrically connected.
As a further preferable aspect of the present invention, the inverter 5 is connected to the solar panel 8 by a wire, and the connection method is electrical connection.
As a further preferred scheme of the utility model, the U-shaped unmanned aerial vehicle undercarriage 1 and the support rod 2 are vertically arranged, and the support rod 2 is of a hollow structure.
As a further preferable scheme of the utility model, the U-shaped unmanned aerial vehicle undercarriage 1 and the two sets of mounting brackets 6 are integrally formed, the two sets of mounting brackets 6 are provided with mounting threaded holes, and the storage battery 4 is connected to a main control board of the unmanned aerial vehicle through a wire.
The working process of the utility model is as follows: when the device is used, the U-shaped unmanned aerial vehicle undercarriage 1 and the two sets of mounting brackets 6 are integrally formed, the two sets of mounting brackets 6 are provided with mounting threaded holes, the U-shaped unmanned aerial vehicle undercarriage 1 of the device is mounted on the unmanned aerial vehicle, the storage battery 4 is connected to a main control panel of the unmanned aerial vehicle through a lead, when the unmanned aerial vehicle is used, the storage battery 4 adopts a rechargeable lithium battery, the storage battery 4 is connected to the inverter 5 through a lead in an electrically connecting manner, the inverter 5 is connected to the solar panel 8 through a lead in an electrically connecting manner, the solar panel 8 absorbs solar energy and converts the solar energy into electric energy, the converted electric energy is converted and stored in the storage battery 4 through the inverter 5 to provide the electric energy for the unmanned aerial vehicle, and the endurance time of the unmanned aerial vehicle is prolonged, this process is through being provided with two sets of solar cell panel on U type unmanned aerial vehicle undercarriage 1, solar cell panel 8 absorbs solar energy, and turn into the electric energy with solar energy, and pass through the inside that battery 4 was saved to the inverter 5 conversion with the electric energy of conversion, provide the electric energy for unmanned aerial vehicle, thereby increase unmanned aerial vehicle's time of endurance, consequently, the operational requirement is satisfied in the time of endurance that can be long-time, and utilize solar energy conversion to reach energy-concerving and environment-protective effect.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.
Claims (5)
1. The utility model provides an unmanned aerial vehicle undercarriage of remote sensing measurement, includes U type unmanned aerial vehicle undercarriage (1), its characterized in that: the utility model discloses a solar energy unmanned aerial vehicle undercarriage, including U type unmanned aerial vehicle undercarriage (1), the both ends symmetry of U type unmanned aerial vehicle undercarriage (1) is provided with bracing piece (2), be provided with cavity (3) on the terminal surface of U type unmanned aerial vehicle undercarriage (1), the inside of cavity (3) is provided with battery (4), one side of battery (4) is and the inside that is located cavity (3) is provided with dc-to-ac converter (5), the lateral wall of U type unmanned aerial vehicle undercarriage (1) is and the length direction symmetry along cavity (3) is provided with two sets of installing supports (6), panel mounting groove (7) have been seted up to the left and right sides lateral wall symmetry of U type unmanned aerial vehicle undercarriage (1), the internally mounted of panel mounting groove (7) has solar cell panel (8).
2. The telemetrically measured unmanned aerial vehicle landing gear of claim 1, wherein: the storage battery (4) adopts a rechargeable lithium battery, the storage battery (4) is connected to the inverter (5) through a lead, and the connection mode is electric connection.
3. The telemetrically measured unmanned aerial vehicle landing gear of claim 1, wherein: the inverter (5) is connected to the solar panel (8) through a lead, and the connection mode is electric connection.
4. The telemetrically measured unmanned aerial vehicle landing gear of claim 1, wherein: u type unmanned aerial vehicle undercarriage (1) is perpendicular setting with bracing piece (2), bracing piece (2) are hollow structure.
5. The telemetrically measured unmanned aerial vehicle landing gear of claim 1, wherein: u type unmanned aerial vehicle undercarriage (1) is integrated into one piece, two sets of with two sets of installing support (6) have seted up the installation screw hole on installing support (6), battery (4) pass through the wire and connect on unmanned vehicles's main control board.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122034925.6U CN215622660U (en) | 2021-08-26 | 2021-08-26 | Unmanned aerial vehicle undercarriage for remote sensing measurement |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122034925.6U CN215622660U (en) | 2021-08-26 | 2021-08-26 | Unmanned aerial vehicle undercarriage for remote sensing measurement |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215622660U true CN215622660U (en) | 2022-01-25 |
Family
ID=79902830
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122034925.6U Expired - Fee Related CN215622660U (en) | 2021-08-26 | 2021-08-26 | Unmanned aerial vehicle undercarriage for remote sensing measurement |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215622660U (en) |
-
2021
- 2021-08-26 CN CN202122034925.6U patent/CN215622660U/en not_active Expired - Fee Related
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106058112A (en) | Cylindrical battery module | |
| CN215622660U (en) | Unmanned aerial vehicle undercarriage for remote sensing measurement | |
| CN103850485A (en) | Parking shed with charging function | |
| CN210224136U (en) | Lightweight aluminium alloy box structure | |
| CN205615349U (en) | Charging pile shell | |
| CN206870870U (en) | A kind of fixed support of individual layer arrangement ultracapacitor | |
| CN210724632U (en) | Roof photovoltaic power generation energy memory | |
| CN215072235U (en) | Solar panel support | |
| CN214480369U (en) | Portable wind-solar hybrid power generation and energy storage device | |
| CN207705255U (en) | A kind of household energy-storage battery module support assembly | |
| CN203103457U (en) | Large-volume large-capacity energy storage battery module structure | |
| CN203032356U (en) | Fixing structure for power battery modules used for automobile | |
| CN207339663U (en) | A kind of flow battery AC-DC power module box structures | |
| CN219316207U (en) | Integrated roof | |
| CN209345084U (en) | A kind of solar photovoltaic assembly convenient for monitoring | |
| CN214101239U (en) | Photovoltaic board is used on roof of high-efficient light harvesting | |
| CN202384796U (en) | Solar energy charging station for electric bicycle | |
| CN211151873U (en) | A location structure for fixing a position photovoltaic module | |
| CN217282779U (en) | Outdoor solar energy storage power supply | |
| CN211063547U (en) | Solar power generation device for building | |
| CN216075345U (en) | Novel solar photovoltaic pump station | |
| CN215498158U (en) | Bus tapping structure with bus connection function | |
| CN210530410U (en) | Sentry box on duty with move function | |
| CN210292074U (en) | Remove sunshine room air conditioning equipment with environmental protection | |
| CN214090347U (en) | Mobile shelter PCR laboratory with solar power supply system |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20220125 |