CN109573072B - Unmanned aerial vehicle oil storage system that inclination was rocked is prevented - Google Patents
Unmanned aerial vehicle oil storage system that inclination was rocked is prevented Download PDFInfo
- Publication number
- CN109573072B CN109573072B CN201811562049.0A CN201811562049A CN109573072B CN 109573072 B CN109573072 B CN 109573072B CN 201811562049 A CN201811562049 A CN 201811562049A CN 109573072 B CN109573072 B CN 109573072B
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- CN
- China
- Prior art keywords
- oil
- oil tank
- unmanned aerial
- aerial vehicle
- storage system
- 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.)
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- 239000003921 oil Substances 0.000 claims abstract description 201
- 230000001817 pituitary effect Effects 0.000 claims abstract description 19
- 239000010705 motor oil Substances 0.000 claims abstract description 8
- 239000002923 metal particle Substances 0.000 claims abstract description 4
- 229910001369 Brass Inorganic materials 0.000 claims description 19
- 239000010951 brass Substances 0.000 claims description 19
- 239000002245 particle Substances 0.000 claims description 18
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims description 14
- 229910052802 copper Inorganic materials 0.000 claims description 14
- 239000010949 copper Substances 0.000 claims description 14
- 239000000463 material Substances 0.000 claims description 7
- 230000000694 effects Effects 0.000 claims description 4
- 229920005989 resin Polymers 0.000 claims description 4
- 239000011347 resin Substances 0.000 claims description 4
- 239000000945 filler Substances 0.000 claims 1
- 239000000295 fuel oil Substances 0.000 abstract description 7
- 238000000034 method Methods 0.000 abstract description 2
- 239000000446 fuel Substances 0.000 description 15
- 206010062767 Hypophysitis Diseases 0.000 description 5
- 239000007788 liquid Substances 0.000 description 5
- 230000007797 corrosion Effects 0.000 description 4
- 238000005260 corrosion Methods 0.000 description 4
- 230000002349 favourable effect Effects 0.000 description 4
- 230000005484 gravity Effects 0.000 description 4
- 239000003822 epoxy resin Substances 0.000 description 3
- 239000012535 impurity Substances 0.000 description 3
- 229920000647 polyepoxide Polymers 0.000 description 3
- 239000002699 waste material Substances 0.000 description 2
- 241000227287 Elliottia pyroliflora Species 0.000 description 1
- 238000010521 absorption reaction Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000002542 deteriorative effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000001914 filtration Methods 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 230000002265 prevention Effects 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 239000012798 spherical particle Substances 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
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
- B64D37/04—Arrangement thereof in or on aircraft
-
- 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
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
- B64D37/06—Constructional adaptations thereof
-
- 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
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/34—Conditioning fuel, e.g. heating
-
- 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
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
- Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
Abstract
The invention discloses an unmanned aerial vehicle oil storage system capable of preventing tilting and shaking, which comprises an oil tank and an oil hammer arranged in the oil tank, wherein the oil hammer is connected to an engine oil supply port outside the oil tank through an oil supply pipe, and an oil return pipe connected with an engine carburetor is also arranged in the oil tank; the oil tank is a semicircular oil tank; the oil hammer comprises an oil nozzle, the lower end of the oil nozzle is fixedly connected with a connecting disc, and the lower side surface of the connecting disc is connected with a lower pituitary body formed by bonding a plurality of metal particles; the oil supply pipe and the oil return pipe are rubber hoses, and the oil supply pipe extends into the bottom of the oil tank and is connected to the oil nozzle. The fuel oil is absorbed from the oil hammer, conveyed to the oil way and then conveyed to the fuel oil storage volume, so that the problem that the engine is damaged due to the fact that fuel oil is not supplied in the flight process of the aircraft can be solved under the condition that the weight of the aircraft is reduced as much as possible, meanwhile, the dead oil quantity of the aircraft is reduced, and the volume of effective fuel oil is increased to the greatest extent.
Description
Technical Field
The invention belongs to the technical field of unmanned aerial vehicles, relates to an unmanned aerial vehicle fuel system, and particularly relates to an unmanned aerial vehicle oil storage system capable of preventing inclination and shaking.
Background
In the prior art, there are many kinds of modes of oil storage of an oil-electricity hybrid power system of an unmanned aerial vehicle with oil-electricity hybrid power, but certain problems exist: when the aircraft flies, due to the inclination of the flying gesture, the oil hammer cannot be always kept below the liquid level, so that an engine oil inlet pipe can enter bubbles or cut off oil when absorbing oil, a light person can damage a crankshaft and a combustion chamber in the engine, and a heavy person can cause the engine to pull a cylinder or stall, so that the aircraft falls down.
Excessive structural members can cause the weight of the aircraft to increase, thereby affecting the endurance time and performance of the aircraft and reducing the safety coefficient of the aircraft.
For the engine oil tank, the gasoline cannot be completely used for landing, a certain amount of oil can be remained all the time to ensure that the engine can normally operate, the residual amount of fuel is called dead oil, the amount of the dead oil depends on the design of an oil storage system of an airplane, and the excessive dead oil can waste the duration of the airplane, reduce the actual consumption of the fuel amount and waste the oil storage space.
Disclosure of Invention
The invention aims to overcome the defects of the prior art, and provides an unmanned aerial vehicle oil storage system capable of preventing tilting and shaking, which is capable of absorbing oil from an oil hammer, conveying the oil to an oil way and storing the shape of the volume of the oil, solving the problem that an engine is damaged due to the fact that the oil is not supplied in the flight process of an aircraft under the condition of ensuring that the weight of the aircraft is reduced as much as possible, reducing the dead oil amount of the aircraft and increasing the volume of effective oil to the maximum extent.
The aim of the invention is realized by the following technical scheme:
the unmanned aerial vehicle oil storage system capable of preventing tilting and shaking comprises an oil tank and an oil hammer arranged in the oil tank, wherein the oil hammer is connected to an engine oil supply port outside the oil tank through an oil supply pipe, and an oil return pipe connected with an engine carburetor is further arranged in the oil tank; the oil tank is a semicircular oil tank; the oil hammer comprises an oil nozzle, the lower end of the oil nozzle is fixedly connected with a connector, and the lower surface of the connector is connected with a lower pituitary body formed by bonding a plurality of metal particles; the oil supply pipe and the oil return pipe are rubber hoses, and the oil supply pipe extends into the bottom of the oil tank and is connected to the oil nozzle.
Further, the connector is a circular connecting disc, and the upper end of the lower pituitary is connected to the lower side surface of the circular connecting disc.
Further, the hypophysis is bonded into a truncated cone structure by brass particles, and each brass particle forms a sponge effect after bonding.
Further, the connector is a conical copper sleeve shell, the upper part of the conical sleeve shell is conical, and the lower part of the conical sleeve shell is a barrel; the upper part of the lower pituitary body extends into the conical copper sleeve body.
Further, the upper part of the conical copper sleeve shell is conical, and the lower part of the conical copper sleeve shell is cylindrical; the pituitary is bonded by brass particles into a bullet-type structure.
Further, the diameter of the brass particles wrapped in the conical copper casing is one half of the diameter of the brass particles with the lower half of the hypophysis exposed.
Further, the oil tank is a semicircular high-density resin oil tank with a hemispherical lower part, and an oil filling port of the oil tank is arranged on the side of the upper end face of the oil tank.
Further, a groove is formed in the bottom of the oil tank.
Further, the upper end face of the oil tank is a plane, and an oil tank fixing bracket for connecting an aircraft is arranged on the periphery of the oil tank.
The invention has the following beneficial effects:
the invention has the characteristics of light weight, simple structure, high strength and reliability on the unmanned engine oil-electricity hybrid power system.
Furthermore, when the aircraft is disassembled, only four oil tank fixing brackets are required to be disassembled, so that the working efficiency is improved, the space utilization rate of the oil tank is improved due to the hemispherical shape, the overall weight of the aircraft is reduced, and the duration of the aircraft is prolonged. The possibility that the engine is extinguished due to bubbles is eliminated, and the stability of the aircraft is improved. The high-density epoxy resin material effectively has the characteristics of falling resistance, corrosion resistance and permeation resistance.
Drawings
Fig. 1 is a schematic view of a single structure of the present invention, in which: (a) a granular brass material oil hammer in one embodiment, (b) a rubber hose, and (c) a semicircular high-density resin oil tank;
FIG. 2 is a schematic diagram of the overall structure of the present invention for achieving its function;
fig. 3 is a schematic view of a particulate brass material oil hammer in accordance with another embodiment of the present invention.
Wherein: 1 is an oil tank; 2 is an oil hammer; 3 is an oil supply pipe; and 4 is an oil return pipe.
Detailed Description
The invention is described in further detail below with reference to the attached drawing figures:
see fig. 1 and 2: the unmanned aerial vehicle oil storage system capable of preventing tilting and shaking comprises an oil tank 1 and an oil hammer 2 arranged in the oil tank 1, wherein the oil hammer 2 is connected to an engine oil supply port outside the oil tank 1 through an oil supply pipe 3, and an oil return pipe 4 connected with an engine carburetor is also arranged in the oil tank 1; the oil tank 1 is a semicircular oil tank; the oil hammer 2 comprises an oil nozzle 2.3, the lower end of the oil nozzle 2.3 is fixedly connected with a connecting disc, and the lower side surface of the connecting disc is connected with a lower pituitary body 2.1 formed by bonding a plurality of metal particles; the oil supply pipe 3 and the oil return pipe 4 are rubber hoses, and the oil supply pipe 3 extends into the bottom of the oil tank 1 and is connected to the oil nozzle 2.3.
As shown in fig. 1 (c): the oil tank 1 is a semicircular high-density resin oil tank with a hemispherical lower part, and an oil filling port of the oil tank 1 is arranged on the side of the upper end face of the oil tank 1. The bottom of the oil tank 1 is provided with a groove. The upper end face of the oil tank 1 is a plane, and an oil tank fixing bracket 1.1 for connecting an aircraft is arranged on the periphery of the oil tank 1. The oil tank 1 of the invention adopts high-density epoxy resin material, thus effectively preventing the permeation and corrosion of gasoline. The shape adopts the hemisphere, is more favorable to fuel and the oil hammer to rock along with the aircraft gesture slope and change the position, and the hemisphere can increase the space utilization, reaches the volume maximize in the oil tank of same weight level. The oil tank oil inlet is arranged on the upper surface, so that fuel can be prevented from being splashed out when the aircraft shakes, and meanwhile, the convenient and fast oiling function is improved. The bottom of the oil tank is in a groove shape, so that dead oil quantity is reduced to the greatest extent.
As in fig. 1 (b): the oil pipe (the oil supply pipe and the oil return pipe) adopts the rubber hose, when the airplane tilts and shakes, the oil pipe can ensure that the oil hammer slides back and forth without external force, and because the liquid can receive the gravity factor and change the position along with the change of the tilting posture of the airplane, the oil hammer also slides along with the change of the tilting posture of the airplane, so that the oil hammer can be always contacted with the liquid. As shown in the figure, two hoses are provided, one hose is an engine oil supply pipe, and the other hose is an engine oil return pipe. The hose is made of epoxy resin material, so that the hose is oil-resistant and corrosion-resistant. The hose can ensure that the oil hammer is not influenced by external force when sliding back and forth in the oil tank along with the change of the aircraft posture. The fuel oil is effectively contacted all the time under the influence of gravity. Preventing the engine from flameout due to no oil sucking.
The lower pituitary body 2.1 of the inventive oil hammer 2 is formed by a plurality of brass particles sticking. In one embodiment of the present invention, as shown in fig. 1 (a): the connector is a round connecting disc 2.2.1, and the upper end of the lower pituitary body 2.1 is connected with the lower side surface of the round connecting disc 2.2.1. The hypophysis 2.1 is adhered to form a truncated cone structure by brass particles, and each brass particle is adhered to form a sponge effect on the hypophysis 2.1. The lower lobe 2.1 reduces the friction of the hammer from the shape and surface finish, allowing the hammer to roll freely within the tank.
In another embodiment of the present invention, as shown in fig. 3, the connector is a conical copper sleeve shell 2.2.2, the upper part of the conical sleeve shell 2.2.2 is conical, and the lower part is a barrel; the upper part of the lower pituitary body 2.1 extends into the conical copper sleeve shell 2.2.2. The upper part of the conical copper bush shell 2.2.2 is conical, and the lower part is cylindrical; the pituitary 2.1 is bonded to a bullet-type structure from brass particles. The diameter of the brass particles wrapped in the conical copper sleeve shell 2.2.2 is half of the diameter of the brass particles of which the lower half part of the hypophysis 2.1 is exposed. The lower half part of the pituitary body 2.1 in the embodiment has large gaps, the upper half part has small gaps, the lower half part is favorable for fuel absorption, the upper half part is favorable for bubble removal and fine impurity filtration. The lower pituitary body 2.2 cone-shaped shell structure has the advantages that the lower half part of the shell is a barrel, particles are effectively prevented from falling off, the upper half part is conical, and residual bubbles and impurities are effectively discharged through the smaller and smaller cross section. The oil nozzle 2.3 of the oil hammer 2 and the connector are integrated, the conical shell structure of the connector is characterized in that the lower half part of the shell is a barrel, particles are effectively prevented from falling off, the upper half part is conical, and residual bubbles and impurities are effectively discharged through the smaller and smaller section. The oil nozzle 2.3 adopts a barb shape, thereby effectively facilitating the insertion and the falling prevention of the oil pipe.
The oil hammer 2 of the invention adopts brass material, which effectively prevents the corrosion and oxidation of gasoline. The oil hammer 2 is formed by bonding spherical particles, is similar to foam, plays a sponge effect, can play a role in absorbing oil, even if the oil hammer is not completely invaded below the liquid level, the oil hammer can ensure that no bubbles exist in an oil pipe as long as the oil hammer contacts with the liquid, and effectively prevents the engine from flameout due to the fact that the engine cannot absorb oil. The oil hammer 2 adopts the oil tank 1 of the invention to be connected to the lower part of an airplane in a hanging way, so as to prevent fuel from deteriorating and volatilizing. The hemispherical shape of the lower part of the oil tank is favorable for the fuel and the oil hammer to slide along with the inclination of the attitude of the airplane, so that the oil hammer always keeps on moving with the fuel at the same time, and the oil hammer is effectively prevented from being separated from the fuel to cause bubbles to enter the oil pipe. The hemispherical design effectively reduces the dead oil quantity of the engine, improves the fuel utilization rate as much as possible, improves the endurance time of the aircraft, and increases the power-weight ratio.
See fig. 2: the installation mode of the invention is as follows:
mounting position: the outermost is the hemisphere oil tank, and the oil tank is inside to be equipped with the oil hammer, and oil pipe connects oil hammer and external engine.
The connection mode is as follows: the engine is arranged at the uppermost end of the engine body, the oil tank is arranged at the lower end of the central plate of the engine body, the oil hammer is connected with the carburetor of the engine through an oil pipe, and the oil hammer is arranged at the bottommost end of the inside of the oil tank;
description of the overall working principle of the invention:
A. when the engine runs, the carburetor can automatically generate negative pressure, the oil hammer always contacts fuel, the negative pressure of the carburetor can absorb the fuel contacted by the oil hammer through the oil pipe, and redundant fuel can return to the oil tank from the oil return pipe of the carburetor;
B. when the aircraft flies, the gesture can swing back and forth, and the fuel can receive gravity influence this moment, and the back and forth movement is kept in the oil tank minimum position all the time in the oil tank. The oil hammer can swing along with the fuel oil due to the influence of gravity and always contacts the fuel oil, so that the continuous oil supply in the oil pipe is ensured.
Claims (9)
1. The unmanned aerial vehicle oil storage system capable of preventing tilting and shaking is characterized by comprising an oil tank (1) and an oil hammer (2) arranged in the oil tank (1), wherein the oil hammer (2) is connected to an engine oil supply port outside the oil tank (1) through an oil supply pipe (3), and an oil return pipe (4) connected with an engine carburetor is further arranged in the oil tank (1); the oil tank (1) is an oil tank with a plane upper end surface and a hemispherical lower part; the oil hammer (2) comprises an oil nozzle (2.3), the lower end of the oil nozzle (2.3) is fixedly connected with a connector, and the lower surface of the connector is connected with a lower pituitary (2.1) formed by bonding a plurality of metal particles; the oil supply pipe (3) and the oil return pipe (4) are rubber hoses, and the oil supply pipe (3) stretches into the bottom of the oil tank (1) and is connected to the oil nozzle (2.3).
2. The unmanned aerial vehicle oil storage system of claim 1, wherein the connector is a circular connecting disc (2.2.1), and the upper end of the lower pituitary (2.1) is connected to the lower side of the circular connecting disc (2.2.1).
3. The unmanned aerial vehicle oil storage system for preventing tilting and shaking according to claim 2, wherein the pituitary (2.1) is bonded into a truncated cone structure by brass particles, and each brass particle bonds to form the pituitary (2.1) into a sponge effect.
4. The unmanned aerial vehicle oil storage system for preventing tilting and shaking according to claim 1, wherein the connector is a conical copper sleeve shell (2.2.2), the upper part of the conical copper sleeve shell (2.2.2) is conical, and the lower part of the conical copper sleeve shell is a barrel; the upper part of the lower pituitary (2.1) extends into the conical copper sleeve shell (2.2.2).
5. The unmanned aerial vehicle oil storage system for preventing tilt and sloshing according to claim 4, wherein the upper part of the conical copper sleeve shell (2.2.2) is conical, and the lower part is cylindrical; the pituitary (2.1) is bonded to a bullet-type structure from brass particles.
6. The unmanned aerial vehicle oil storage system of claim 5, wherein the diameter of the brass particles wrapped in the conical copper sleeve shell (2.2.2) is half of the diameter of the brass particles with the lower half of the pituitary (2.1) exposed.
7. The unmanned aerial vehicle oil storage system capable of preventing tilting and shaking according to claim 1, wherein the hemispherical material of the lower part of the oil tank (1) is high-density resin, and the oil filler of the oil tank (1) is arranged on the side of the upper end face of the oil tank (1).
8. The unmanned aerial vehicle oil storage system against tilting and shaking according to claim 7, wherein the bottom of the oil tank (1) is provided with a groove.
9. The unmanned aerial vehicle oil storage system against tilting and shaking according to claim 7, wherein an oil tank fixing bracket (1.1) for connecting with an aircraft is provided at the circumferential side of the oil tank (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811562049.0A CN109573072B (en) | 2018-12-20 | 2018-12-20 | Unmanned aerial vehicle oil storage system that inclination was rocked is prevented |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811562049.0A CN109573072B (en) | 2018-12-20 | 2018-12-20 | Unmanned aerial vehicle oil storage system that inclination was rocked is prevented |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109573072A CN109573072A (en) | 2019-04-05 |
| CN109573072B true CN109573072B (en) | 2023-12-22 |
Family
ID=65930202
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811562049.0A Active CN109573072B (en) | 2018-12-20 | 2018-12-20 | Unmanned aerial vehicle oil storage system that inclination was rocked is prevented |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109573072B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110239725B (en) * | 2019-05-29 | 2023-04-14 | 陕西飞机工业（集团）有限公司 | Detachable constant-temperature anti-shaking and anti-vibrating lubricating oil tank for airplane |
| CN113525698A (en) * | 2020-04-15 | 2021-10-22 | 北京京东乾石科技有限公司 | Oil tank for aircraft |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB836923A (en) * | 1957-05-30 | 1960-06-09 | Walter Philip Williams | Liquid storage tank for use in aircraft |
| CN201086827Y (en) * | 2007-08-03 | 2008-07-16 | 西安大地测绘工程有限责任公司 | Anti-bubble fuel tank |
| CN202429061U (en) * | 2011-12-28 | 2012-09-12 | 连云港通元机械有限公司 | Fuel tank |
| CN204910771U (en) * | 2015-06-24 | 2015-12-30 | 珠海市德天航模有限公司 | Oil tank of model aeroplane and model ship |
| WO2016131088A1 (en) * | 2015-02-19 | 2016-08-25 | Orbital Australia Pty Ltd | Uav fuel and lubrication system |
| CN209321257U (en) * | 2018-12-20 | 2019-08-30 | 西安达纳森物联科技有限公司 | A kind of unmanned plane oil storage system that Anti-inclining shakes |
-
2018
- 2018-12-20 CN CN201811562049.0A patent/CN109573072B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB836923A (en) * | 1957-05-30 | 1960-06-09 | Walter Philip Williams | Liquid storage tank for use in aircraft |
| CN201086827Y (en) * | 2007-08-03 | 2008-07-16 | 西安大地测绘工程有限责任公司 | Anti-bubble fuel tank |
| CN202429061U (en) * | 2011-12-28 | 2012-09-12 | 连云港通元机械有限公司 | Fuel tank |
| WO2016131088A1 (en) * | 2015-02-19 | 2016-08-25 | Orbital Australia Pty Ltd | Uav fuel and lubrication system |
| CN204910771U (en) * | 2015-06-24 | 2015-12-30 | 珠海市德天航模有限公司 | Oil tank of model aeroplane and model ship |
| CN209321257U (en) * | 2018-12-20 | 2019-08-30 | 西安达纳森物联科技有限公司 | A kind of unmanned plane oil storage system that Anti-inclining shakes |
Also Published As
| Publication number | Publication date |
|---|---|
| CN109573072A (en) | 2019-04-05 |
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