CN112896541A - Portable unmanned aerial vehicle electric oil pump - Google Patents

Portable unmanned aerial vehicle electric oil pump Download PDF

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Publication number
CN112896541A
CN112896541A CN202110193169.3A CN202110193169A CN112896541A CN 112896541 A CN112896541 A CN 112896541A CN 202110193169 A CN202110193169 A CN 202110193169A CN 112896541 A CN112896541 A CN 112896541A
Authority
CN
China
Prior art keywords
oil
oil pump
unmanned aerial
aerial vehicle
circuit module
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
Application number
CN202110193169.3A
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Chinese (zh)
Inventor
钟伟
张亚辉
程浩
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Guangdong Haiwei Dieng Space Information Technology Co ltd
Original Assignee
Guangdong Haiwei Dieng Space Information Technology Co ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Guangdong Haiwei Dieng Space Information Technology Co ltd filed Critical Guangdong Haiwei Dieng Space Information Technology Co ltd
Priority to CN202110193169.3A priority Critical patent/CN112896541A/en
Publication of CN112896541A publication Critical patent/CN112896541A/en
Pending legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00Ground or aircraft-carrier-deck installations
    • B64F1/28Liquid-handling installations specially adapted for fuelling stationary aircraft
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00Propulsion; Power supply
    • B64U50/10Propulsion
    • B64U50/11Propulsion using internal combustion piston engines

Abstract

The invention relates to the technical field of refueling of unmanned aerial vehicles, in particular to a portable unmanned aerial vehicle electric oil pump. The oil pump box comprises an oil pump box body, and comprises a front plate, a back plate, a left side plate, a right side plate, a cover plate and a bottom plate, wherein a touch screen display is arranged on the cover plate, the front plate is provided with a switch of a storage battery, an oil circuit module arranged in the oil pump box body comprises an oil filter, a magnetic oil pump and an oil guide pipe, the circuit module arranged in the oil pump box body comprises a battery box, the storage battery arranged in the battery box and a circuit controller electrically connected with the storage battery, the oil circuit module is close to the bottom plate, the circuit module is close to the cover plate, and the circuit module and the oil circuit module are isolated by the battery box. This electric oil pump reasonable design, it is small, and digital demonstration guarantees the meticulous process of refueling, and then improves unmanned aerial vehicle and refuels efficiency.

Description

Portable unmanned aerial vehicle electric oil pump
Technical Field
The invention relates to the technical field of refueling of unmanned aerial vehicles, in particular to a portable unmanned aerial vehicle electric oil pump.
Background
An unmanned plane is an unmanned plane which is operated by a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by a vehicle-mounted computer, and is classified into military use and civil use according to application fields. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + industry is applied, and is really just needed by the unmanned aerial vehicle.
The disadvantages are that: traditional fuel unmanned aerial vehicle refueling mode generally pours or uses the hand formula of machinery fuel filler pump filling for ground, and this kind of mode of filling efficiency is lower, degree of automation is low, the precision is low, and is not adapted to and uses for large-scale unmanned aerial vehicle large capacity refueling to the unmanned aerial vehicle filling device in existing market does not effectually separates circuit and oil circuit and comes, has the operation risk at the in-process for the unmanned aerial vehicle oiling.
Disclosure of Invention
In order to solve the problems, the invention aims to provide a portable unmanned aerial vehicle electric oil pump which is safe to operate, is reasonable in design, small in size and capable of displaying digitally, ensures a fine refueling process and further improves the refueling efficiency of an unmanned aerial vehicle.
The technical purpose of the invention is realized by the following technical scheme: a portable unmanned aerial vehicle electric oil pump comprises,
the oil pump box body comprises a front plate, a back plate, a left side plate, a right side plate, a cover plate and a bottom plate, wherein an oil inlet and an oil outlet are arranged on the left side plate, an oil outlet and an oil outlet are arranged on the right side plate, a touch screen display is arranged on the cover plate and used for displaying the electric quantity of a storage battery and the pressure in the oil guide pipe and adjusting the pressure of the oil guide pipe, a switch of the storage battery is arranged on the front plate,
the oil circuit module arranged in the oil pump box body comprises an oil filter, a magnetic oil pump and the oil guide pipe, the oil guide pipe consists of an oil inlet guide pipe, an oil transition guide pipe and an oil outlet guide pipe, two ends of the oil inlet guide pipe are respectively connected with the oil inlet guide port and the inlet port of the oil filter, two ends of the oil transition guide pipe are respectively connected with the outlet port of the oil filter and the inlet port of the magnetic oil pump, two ends of the oil outlet guide pipe are respectively connected with the outlet port of the magnetic oil pump and the oil outlet guide port,
the circuit module arranged in the oil pump box body comprises a battery box, a storage battery arranged in the battery box and a circuit controller electrically connected with the storage battery,
the oil circuit module is arranged close to the bottom plate, the circuit module is arranged close to the cover plate, and the battery box isolates the circuit module from the oil circuit module.
Preferably, the magnetic oil pump is a plunger pump.
Preferably, the storage battery is a lithium battery, and the rated voltage is 12 v.
Preferably, the magnetic oil pump is horizontally arranged on the oil bottom plate through two same supporting arms, the oil filter is horizontally arranged on the bottom plate, and the battery box is arranged on the base of the box body.
Further preferably, the oil filter and the support arm are detachably connected to the base plate by bolts.
Preferably, the circuit controller is disposed in a space formed by the back plate, the battery box, the cover plate and the box body base, and the box body base is parallel to the bottom plate.
Preferably, the touch screen display is provided with an on-off control key and a pause control key of the magnetic oil pump.
Preferably, the oil inlet and the oil outlet are provided with a buckle device for connecting an outer oil guide pipe.
Preferably, a pair of foldable handles is arranged on the cover plate.
The principle of the invention is as follows: the inside reasonable effectual plan of oil pump is oil circuit module and circuit module to utilize battery box science to keep apart oil circuit module and circuit module, improve unmanned aerial vehicle refuels the security.
In conclusion, the invention has the following beneficial effects:
the plunger type oiling pump has the advantages of high pressure, compact structure, high efficiency and convenient flow regulation, reduces the space required by the oil pump box body on one hand, and can regulate the flow of the oiling pump through the touch screen display at any time on the other hand, thereby realizing the advantages of strong suction force of the oil pump, stable oil supply and the like;
secondly, lithium batteries with different sizes and rated power supply voltage of 12V can be mounted in the unmanned aerial vehicle avionics system, the rated voltage is the same as that of the lithium batteries of the unmanned aerial vehicle avionics system, materials are convenient to obtain, the idle lithium batteries of the unmanned aerial vehicle can be used for supplying power, idle resources are well utilized, and the equipment universality is improved;
thirdly, the circuit controller is arranged in a space formed by the back plate, the battery box, the cover plate and the box body base, and further isolates the circuit module from the oil circuit module;
fourthly, the buckle device is convenient for the electric oil pump and the external oil guide pipe to be connected conveniently;
fifthly, the pair of handles is convenient for the electric oil pump to move, and when the electric oil pump does not need to move, the pair of handles is folded, so that the attractiveness and the practicability of the electric oil pump are guaranteed.
Drawings
FIG. 1 is a disassembled schematic view of the present invention;
FIG. 2 is a perspective view of the present invention;
FIG. 3 is a left side view of the present invention;
FIG. 4 is a cross-sectional view taken along line A-A of FIG. 3 in accordance with the present invention;
FIG. 5 is a cross-sectional view taken along line B-B of FIG. 3 in accordance with the present invention;
in the figure: 1. a front plate; 2. a back plate; 3. a left side plate; 4. a right side plate; 5. a cover plate; 6. a base plate; 7. an oil inlet and outlet; 8. an oil outlet and an oil guide port; 9. a box body base; 10. a touch screen display; 11. an oil filter; 12. a magnetic oil pump; 13. a battery case; 14. a support arm; 15. a circuit controller; 16. a buckle device; 17. a handle.
Detailed Description
The present invention will be described in detail with reference to the accompanying drawings and embodiments, and the oil conduit is not shown in the drawings because the oil conduit shields other equipment components.
In the description of the present invention, it is to be understood that the terms "center", "longitudinal", "lateral", "length", "width", "thickness", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", "clockwise", "counterclockwise", "axial", "radial", "circumferential", etc., indicate orientations and positional relationships based on those shown in the drawings, and are used merely for convenience of description of the present invention, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and therefore, are not to be considered as limiting the present invention.
Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or eliminating relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In the description of the present invention, "a plurality" means at least two unless specifically defined otherwise.
In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," "secured," and the like are to be construed broadly and can, for example, be fixedly connected, detachably connected, or integrally formed; may be mechanically coupled, may be electrically coupled or may be in communication with each other; they may be directly connected or indirectly connected through intervening media, or they may be connected internally or in any other suitable relationship, unless expressly stated otherwise. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.
Specifically, referring to fig. 1-5, a portable unmanned aerial vehicle electric oil pump comprises an oil pump box body, which comprises a front plate 1, a back plate 2, a left side plate 3, a right side plate 4, a cover plate 5 and a bottom plate 6, wherein the left side plate 3 is provided with an oil inlet 7, the right side plate 4 is provided with an oil outlet 8, the cover plate 5 is provided with a touch screen display 10, the touch screen display 10 is used for displaying the electric quantity of a storage battery and the pressure of an oil guide pipe and adjusting the pressure of the oil guide pipe, the front plate 1 is provided with a switch (not labeled) of the storage battery, wherein the oil inlet 7 and the oil outlet 8 are arranged at the same height and are both positioned at the lower part of the side plate, the touch screen display 10 is embedded into the cover plate 5, and,
set up in inside oil circuit module of oil pump box body, including oil filter 11, magnetic oil pump 12 and lead oil pipe, lead oil pipe by advance lead oil pipe, excessively lead oil pipe and go out lead oil pipe and constitute, advance the entrance point that leads oil port 7 and oil filter 11 is connected respectively at oil pipe's both ends, excessively lead oil pipe both ends and connect the exit end of oil filter 11 and the entrance point of magnetic oil pump 12 respectively, go out and lead oil pipe both ends and connect magnetic oil pump 12's exit end respectively and go out and lead oil port 8, wherein, the flow direction of oil in this embodiment oil circuit module is: from the oil inlet and guide port 7 to the oil filter 11 to the magnetic oil pump 12 to the oil outlet and guide port 8,
the circuit module arranged in the oil pump box body comprises a battery box 13, a storage battery arranged in the battery box 13 and a circuit controller 15 electrically connected with the storage battery,
the oil circuit module is arranged close to the bottom plate 6, the circuit module is arranged close to the cover plate 5, and the battery box 13 isolates the circuit module from the oil circuit module.
Through above-mentioned scheme, the inside reasonable effectual plan of oil pump is oil circuit module and circuit module to utilize 13 scientific of battery box to keep apart oil circuit module and circuit module, improve unmanned aerial vehicle refuels the security.
Specifically, the magnetic oil pump 12 is a plunger pump.
Through the scheme, the plunger type oiling pump has the advantages of high pressure, compact structure, high efficiency and convenient flow regulation, reduces the space required by the oil pump box body on one hand, and can regulate the flow of the oiling pump through the touch screen display 10 at any time on the other hand, thereby realizing the advantages of strong suction of the oil pump, stable oil supply and the like.
Specifically, the storage battery is a lithium battery with a rated voltage of 12 v.
Through above-mentioned scheme, the lithium cell of the rated supply voltage 12V of installation unidimensional, rated voltage is the same with unmanned aerial vehicle avionics system lithium cell, not only is convenient for draw materials, can also utilize idle unmanned aerial vehicle lithium cell power supply, fine utilization idle resource, improved the equipment commonality.
Specifically, the magnetic oil pump 12 is horizontally mounted on the oil bottom plate 6 through two identical supporting arms 14, the oil filter 11 is horizontally mounted on the base of the oil filter 11, and the battery case 13 is arranged on the case base 9.
Specifically, the magnetic oil pump 12 and the supporting arm 14 are detachably connected with the base plate 6 through bolts, and the detachable connection facilitates maintenance of the device.
Specifically, the circuit controller 15 is arranged in a space formed by the back plate 2, the battery box 13, the cover plate 5 and the box body base 9, the box body base 9 is parallel to the bottom plate 6, the circuit controller 15 is completely isolated from the oil circuit module, and the safety of the electric oil pump is further ensured;
specifically, the touch screen display 10 is provided with an on-off control key and a pause control key of the magnetic oil pump 12.
Through the scheme, the touch screen display 10 is powered by the storage battery, the control key of the magnetic oil pump 12 is arranged in the touch screen display, and the control key of the pause key is favorable for controlling the oiling process.
Specifically, the oil inlet and outlet ports 7 and 8 are provided with a buckle device 16 for connecting an oil pipe, so that the electric oil pump and the outer oil pipe can be conveniently connected.
Specifically, the cover plate 5 is provided with a pair of foldable handles 17.
Through the scheme, the handles 17 are arranged to facilitate the movement of the electric oil pump, and when the electric oil pump does not need to be moved, the double handles 17 are folded, so that the attractiveness and the practicability of the electric oil pump are guaranteed.
The application method of the implementation comprises the following steps:
step one, a buckle device 16 arranged on a left side plate 3 is connected with an outer oil pipe of which the other end is connected with an oil drum in a buckle mode, and a buckle device 16 arranged on a right side plate 4 is connected with an outer oil pipe of which the other end is connected with an unmanned aerial vehicle oil tank in a buckle mode;
step two, pressing a storage battery switch arranged on the front plate 1;
step three, after the pre-fuel charge is set or the height of the oil level in the oil tank of the unmanned aerial vehicle is set, starting a working switch of the magnetic oil pump 12 through the touch screen display screen 10;
step four, if the oiling needs to be stopped in midway, the oiling can be suspended by pressing a suspension key;
and step five, after oiling is finished, closing a storage battery switch, and detaching and storing two outer oil pipes of the oil pump box body.
The above-mentioned embodiments only express several embodiments of the present invention, and the description thereof is more specific and detailed, but not construed as limiting the scope of the present invention. It should be noted that, for a person skilled in the art, several variations and modifications can be made without departing from the inventive concept, which falls within the scope of the present invention. Therefore, the protection scope of the present patent shall be subject to the appended claims.

Claims (9)

1. A portable unmanned aerial vehicle electric oil pump, which is characterized by comprising
The oil pump box body comprises a front plate, a back plate, a left side plate, a right side plate, a cover plate and a bottom plate, wherein an oil inlet and an oil outlet are arranged on the left side plate, an oil outlet and an oil outlet are arranged on the right side plate, a touch screen display is arranged on the cover plate and used for displaying the electric quantity of the storage battery and the pressure of the oil guide pipe and adjusting the pressure of the oil guide pipe, a switch of the storage battery is arranged on the front plate,
the oil circuit module arranged in the oil pump box body comprises an oil filter, a magnetic oil pump and the oil guide pipe, the oil guide pipe consists of an oil inlet guide pipe, an oil transition guide pipe and an oil outlet guide pipe, two ends of the oil inlet guide pipe are respectively connected with the oil inlet guide port and the inlet port of the oil filter, two ends of the oil transition guide pipe are respectively connected with the outlet port of the oil filter and the inlet port of the magnetic oil pump, two ends of the oil outlet guide pipe are respectively connected with the outlet port of the magnetic oil pump and the oil outlet guide port,
the circuit module arranged in the oil pump box body comprises a battery box, a storage battery arranged in the battery box and a circuit controller electrically connected with the storage battery,
the oil circuit module is arranged close to the bottom plate, the circuit module is arranged close to the cover plate, and the battery box isolates the circuit module from the oil circuit module.
2. The portable unmanned aerial vehicle electric oil pump of claim 1, wherein the magnetic oil pump is a plunger pump.
3. The portable unmanned aerial vehicle electric oil pump of claim 1, characterized in that the battery is a lithium battery with a rated voltage of 12 v.
4. The portable unmanned aerial vehicle electric oil pump of claim 1, wherein the magnetic oil pump is horizontally mounted on the oil pan by two identical support arms, the oil filter is horizontally mounted on the pan, and the battery compartment is disposed on a cartridge base.
5. The portable unmanned aerial vehicle electric oil pump of claim 4, wherein the oil filter and the support arm are removably connected to the base plate by bolts.
6. The unmanned aerial vehicle electric oil pump of claim 4, characterized in that the circuit controller is arranged in a space formed by the back plate, the battery box, the cover plate and the box body base, and the box body base is parallel to the bottom plate.
7. The portable unmanned aerial vehicle electric oil pump of claim 1, characterized in that the touch screen display is provided with an on-off control key and a pause control key of the magnetic oil pump.
8. The portable unmanned aerial vehicle electric oil pump of claim 1, characterized in that the oil inlet and the oil outlet are provided with a snap device for connecting an outer oil conduit.
9. The portable unmanned aerial vehicle electric oil pump of claim 1, wherein a pair of foldable handles are provided on the cover plate.
CN202110193169.3A 2021-02-20 2021-02-20 Portable unmanned aerial vehicle electric oil pump Pending CN112896541A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202110193169.3A CN112896541A (en) 2021-02-20 2021-02-20 Portable unmanned aerial vehicle electric oil pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202110193169.3A CN112896541A (en) 2021-02-20 2021-02-20 Portable unmanned aerial vehicle electric oil pump

Publications (1)

Publication Number Publication Date
CN112896541A true CN112896541A (en) 2021-06-04

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CN202110193169.3A Pending CN112896541A (en) 2021-02-20 2021-02-20 Portable unmanned aerial vehicle electric oil pump

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CN (1) CN112896541A (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN202808333U (en) * 2012-09-04 2013-03-20 中国航天科工集团第三研究院第八三五七研究所 Portable oiling device for unmanned aerial vehicle
CN105174188A (en) * 2015-05-28 2015-12-23 河南翱翔航空科技有限公司 Portable electric rapid oiling machine
CN207374698U (en) * 2017-11-09 2018-05-18 山东滨奥飞机制造有限公司 A kind of movable small aircraft refuelling device
US20190077521A1 (en) * 2015-10-30 2019-03-14 Intelligent Energy Limited Fueling Station
CN110723711A (en) * 2019-09-29 2020-01-24 沈阳航空航天大学 Portable unmanned aerial vehicle tanker aircraft
CN210149586U (en) * 2019-07-12 2020-03-17 四川飞达源通能源装备制造有限公司 General airport mobile aviation filling equipment

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN202808333U (en) * 2012-09-04 2013-03-20 中国航天科工集团第三研究院第八三五七研究所 Portable oiling device for unmanned aerial vehicle
CN105174188A (en) * 2015-05-28 2015-12-23 河南翱翔航空科技有限公司 Portable electric rapid oiling machine
US20190077521A1 (en) * 2015-10-30 2019-03-14 Intelligent Energy Limited Fueling Station
CN207374698U (en) * 2017-11-09 2018-05-18 山东滨奥飞机制造有限公司 A kind of movable small aircraft refuelling device
CN210149586U (en) * 2019-07-12 2020-03-17 四川飞达源通能源装备制造有限公司 General airport mobile aviation filling equipment
CN110723711A (en) * 2019-09-29 2020-01-24 沈阳航空航天大学 Portable unmanned aerial vehicle tanker aircraft

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Application publication date: 20210604