CN110562462A - Throwing type unmanned vehicles and a protection section of thick bamboo thereof - Google Patents
Throwing type unmanned vehicles and a protection section of thick bamboo thereof Download PDFInfo
- Publication number
- CN110562462A CN110562462A CN201910955221.7A CN201910955221A CN110562462A CN 110562462 A CN110562462 A CN 110562462A CN 201910955221 A CN201910955221 A CN 201910955221A CN 110562462 A CN110562462 A CN 110562462A
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- China
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- glass fiber
- fiber reinforced
- reinforced plastic
- wall
- protection cylinder
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- 235000017166 Bambusa arundinacea Nutrition 0.000 title claims abstract description 15
- 235000017491 Bambusa tulda Nutrition 0.000 title claims abstract description 15
- 241001330002 Bambuseae Species 0.000 title claims abstract description 15
- 235000015334 Phyllostachys viridis Nutrition 0.000 title claims abstract description 15
- 239000011425 bamboo Substances 0.000 title claims abstract description 15
- 239000011152 fibreglass Substances 0.000 claims abstract description 76
- 238000009413 insulation Methods 0.000 claims abstract description 32
- 230000001681 protective effect Effects 0.000 claims abstract description 28
- 238000010438 heat treatment Methods 0.000 claims abstract description 15
- 229920005830 Polyurethane Foam Polymers 0.000 claims description 6
- 238000005266 casting Methods 0.000 claims description 6
- 239000011496 polyurethane foam Substances 0.000 claims description 6
- 210000001503 joint Anatomy 0.000 claims description 4
- 238000002360 preparation method Methods 0.000 abstract description 4
- 229910000838 Al alloy Inorganic materials 0.000 description 10
- 238000005485 electric heating Methods 0.000 description 9
- 229920000742 Cotton Polymers 0.000 description 6
- 238000004321 preservation Methods 0.000 description 5
- 238000003466 welding Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 4
- 238000001723 curing Methods 0.000 description 3
- 239000012528 membrane Substances 0.000 description 3
- 238000001514 detection method Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 229920001187 thermosetting polymer Polymers 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000005056 compaction Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 238000013007 heat curing Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 239000011810 insulating material Substances 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 238000004806 packaging method and process Methods 0.000 description 1
- 239000005011 phenolic resin Substances 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 229920001721 polyimide Polymers 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 238000007493 shaping process Methods 0.000 description 1
- 238000003892 spreading Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 229920006305 unsaturated polyester Polymers 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D5/00—Aircraft transported by aircraft, e.g. for release or reberthing during flight
Abstract
The application relates to unmanned air vehicle technical field, especially relates to a type of jettisoning unmanned vehicles and a protection section of thick bamboo thereof, and wherein, the type of jettisoning unmanned vehicles protection section of thick bamboo includes: the heating layer is covered on the inner surface of the protection cylinder body; the protective cylinder body sequentially comprises a glass fiber reinforced plastic inner wall, a heat insulation layer and a glass fiber reinforced plastic outer wall from inside to outside, the glass fiber reinforced plastic inner wall and the glass fiber reinforced plastic outer wall are clamped on the heat insulation layer, and the glass fiber reinforced plastic inner wall, the heat insulation layer and the glass fiber reinforced plastic outer wall are integrally formed. The application provides a type of jettisoning unmanned vehicles protective barrel and type of jettisoning unmanned vehicles, when having reduced the preparation degree of difficulty of the protective barrel of type of jettisoning unmanned vehicles, improved the thermal insulation performance of a protective barrel.
Description
Technical Field
The application relates to the technical field of unmanned aerial vehicles, in particular to a throwing type unmanned aerial vehicle and a protection cylinder thereof.
Background
With the gradual development of national science and technology and economic strength, the unmanned aerial vehicle is widely applied to various fields, such as military detection, forest fire detection, power industry inspection, geological survey, aerial photography and the like. The throwing type unmanned aerial vehicle is used, the throwing type unmanned aerial vehicle is taken as a submachine to be hung on a mother machine (such as a medium-sized or large-sized unmanned aerial vehicle or a manned machine), the mother machine throws the submachine when a task is executed, and the submachine and the mother machine are separated to independently fly.
However, the sub-machine flies at high altitude and low temperature for a long time after being carried by the main machine, and key components of the sub-machine, such as a battery, control system electronic components and the like, are easy to be damaged in a low-temperature environment, so that after the sub-machine is put in, the key components of the sub-machine cannot be started, and the sub-machine is damaged.
In the prior art, the shell of the protection cylinder of the tossing type unmanned aerial vehicle is an aluminum alloy shell, specifically, the shell is a cylinder made of an aluminum alloy sheet through welding or sealed riveting, and the aluminum alloy shell of the protection cylinder of the tossing type unmanned aerial vehicle can ensure the required rigidity and strength; in addition, the heat preservation cotton and the heating wires are adhered to the inside of the aluminum alloy shell and used for heating and preserving heat in the aluminum alloy shell in a low-temperature environment, so that key parts of the submachine arranged in the protection cylinder are kept at a proper working temperature.
However, since the protection cylinder of the tossing type unmanned aerial vehicle is in a slender shape, the protection cylinder of the tossing type unmanned aerial vehicle is manufactured by adopting an aluminum alloy sheet through a welding or riveting process in the prior art, and if the protection cylinder is manufactured by adopting the welding process, the deformation is easy to occur, and the profile quality and the butt seam quality are difficult to ensure; if the protective cylinder is manufactured by sealing riveting, the workload is very large. And because the protection cylinder is in a slender shape, when the heat insulation cotton and the heating wire are laid in the aluminum alloy shell of the protection cylinder, the operation space is small, the operation difficulty is high, the heat insulation cotton is easy to glue or curl, and the bonding quality of the heat insulation cotton is difficult to control.
In addition, the shell of the protection cylinder is made of aluminum alloy, and due to the high heat conductivity coefficient and the quick heat conduction of the aluminum alloy, the heat insulation performance of the protection cylinder is almost completely provided by the internal heat insulation cotton, so that the heat insulation performance of the existing protection cylinder is lower; and because other functional components such as a guide rail, a clamping groove, an electric heating wire and the like need to be installed in the protection cylinder, an opening must be formed in the heat insulation cotton at the position of the guide rail, the clamping groove, the electric heating wire and other components, the inner wall of the aluminum alloy shell cannot be completely covered, a heat leakage channel is formed, and the heat insulation performance is further reduced.
Therefore, how to reduce the manufacturing difficulty of the protection cylinder of the tossing type unmanned aerial vehicle and improve the heat insulation performance of the protection cylinder is a technical problem which needs to be solved urgently by technical personnel in the field.
Disclosure of Invention
The application provides a throwing type unmanned vehicles protection section of thick bamboo and throwing type unmanned vehicles to when reducing the preparation degree of difficulty of throwing type unmanned vehicles's a protection section of thick bamboo, improve the thermal insulation performance of a protection section of thick bamboo.
In order to solve the technical problem, the application provides the following technical scheme:
A tossing-type UAV protective canister comprising: the heating layer is covered on the inner surface of the protection cylinder body; the protective cylinder body sequentially comprises a glass fiber reinforced plastic inner wall, a heat insulation layer and a glass fiber reinforced plastic outer wall from inside to outside, the glass fiber reinforced plastic inner wall and the glass fiber reinforced plastic outer wall are clamped on the heat insulation layer, and the glass fiber reinforced plastic inner wall, the heat insulation layer and the glass fiber reinforced plastic outer wall are integrally formed.
The tossing-type unmanned aerial vehicle protective cylinder as described above, wherein preferably, the heat insulating layer is a polyurethane foam layer.
The tossing type unmanned aerial vehicle protection cylinder as described above, wherein preferably, the heating layer is a PI electric heating film layer.
The tossing type unmanned aerial vehicle protection cylinder is characterized in that the thickness ratio of the glass fiber reinforced plastic inner wall, the insulating layer and the glass fiber reinforced plastic outer wall is 1:3: 1.
In the tossing-type unmanned aerial vehicle protection cylinder described above, preferably, a guide groove or a guide protrusion is mounted on an inner surface of the inner glass fiber reinforced plastic wall, and the guide groove or the guide protrusion faces a guide rail in an axial direction of the protection cylinder body, and an extending direction of the guide rail is the same as the axial direction of the protection cylinder body.
The tossing type unmanned aerial vehicle protection cylinder as described above, wherein preferably, the heat insulation layer completely covers between the inner wall of the glass fiber reinforced plastic and the outer wall of the glass fiber reinforced plastic, and at the cylinder mouth position of the protection cylinder body, the heat insulation layer is chamfered so as to directly bond the inner wall of the glass fiber reinforced plastic and the outer wall of the glass fiber reinforced plastic at the cylinder mouth position of the protection cylinder body, thereby forming a complete sandwich structure of the heat insulation layer of the glass fiber reinforced plastic.
In the tossing-type unmanned aerial vehicle protection cylinder as described above, preferably, a through hole is provided at a cylinder opening position of the protection cylinder, and a bolt is inserted through the through hole of the flange and the through hole of the protection cylinder to fixedly connect the protection cylinder body and the flange.
A tossing-type unmanned aerial vehicle comprising: the primary machine, the secondary machine and the throwing type unmanned aerial vehicle protection barrel; a cylinder opening of the casting type unmanned aerial vehicle protection cylinder is in butt joint with the submachine, and a preset part of the submachine is arranged in the casting type unmanned aerial vehicle protection cylinder; the lifting lug fixed on the outer surface of the protection cylinder is fixedly connected with the master machine so as to mount the sub machine on the master machine.
Compared with the background art, the throwing type unmanned aerial vehicle protection cylinder and the throwing type unmanned aerial vehicle provided by the invention have the advantages that the inner wall and the outer wall of the protection cylinder body are both made of glass fiber reinforced plastics, so that the thermal conductivity is low, and the thermal insulation performance of the protection cylinder is ensured; the protection cylinder body is integrally formed in a paving and heat curing mode, so that the protection cylinder body is manufactured without operations such as welding, riveting and the like, and the defects of large manufacturing workload and high working difficulty are avoided; in addition, the heat-insulating layer avoids the guide rail clamping grooves, so that the outer surface of the inner wall of the glass fiber reinforced plastic can be completely covered, a heat leakage channel does not exist, and higher heat-insulating performance can be further ensured.
Drawings
in order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments described in the present invention, and other drawings can be obtained by those skilled in the art according to the drawings.
FIG. 1 is a schematic structural diagram of a tossing-type unmanned aerial vehicle protection barrel provided by an embodiment of the application;
3 FIG. 3 2 3 is 3 a 3 sectional 3 view 3 taken 3 along 3 line 3 A 3- 3 A 3 of 3 FIG. 3 1 3; 3
Fig. 3 is an enlarged view of a nozzle position of a casting type unmanned aerial vehicle protection barrel provided by an embodiment of the application.
Detailed Description
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the drawings are illustrative only and should not be construed as limiting the invention.
Referring to fig. 1, fig. 1 is a schematic structural diagram of a tossing type unmanned aerial vehicle protection cylinder provided in an embodiment of the present application.
The application provides a type of jettisoning unmanned vehicles protection section of thick bamboo includes: a protective cylinder body 1 and a heating layer (not shown in the figure) covering the inner surface of the protective cylinder body 1; the structure of the protective cylinder body 1 is a sandwich structure of glass fiber reinforced plastics and an insulating layer (such as a polyurethane foam layer); the heating layer can be heating wires, electrothermal films and other parts capable of generating heat, and the heating layer is preferably an electrothermal film in the application.
3 referring 3 to 3 fig. 3 2 3, 3 fig. 3 2 3 is 3 a 3 cross 3- 3 sectional 3 view 3 taken 3 along 3 line 3 a 3- 3 a 3 of 3 fig. 3 1 3. 3 Specifically, the protective cylinder body 1 sequentially comprises a glass fiber reinforced plastic inner wall 101, an insulating layer 102 and a glass fiber reinforced plastic outer wall 103 from inside to outside, that is, the glass fiber reinforced plastic inner wall 101 and the glass fiber reinforced plastic outer wall 103 clamp the insulating layer 102 together, and the glass fiber reinforced plastic inner wall 101, the insulating layer 102 and the glass fiber reinforced plastic outer wall 103 are integrally formed to form an integral protective cylinder body 1 without a connecting seam. In order to ensure the heat preservation effect, the thickness ratio of the glass fiber reinforced plastic inner wall 101, the heat preservation layer 102 and the glass fiber reinforced plastic outer wall 103 is preferably 1:3:1, and other thickness ratios can be adopted according to the actual heat preservation requirement, specifically, the thicknesses of the glass fiber reinforced plastic inner wall 101, the heat preservation layer 102 and the glass fiber reinforced plastic outer wall 103 are respectively 2mm, 6mm and 2 mm.
Specifically, the heating layer is preferably a PI electric heating film layer in the application, and the PI electric heating film is also called a high-heat electric heating film, is a transparent metal flexible electric heating film, and is thin in thickness and small in occupied volume. After the protective cylinder is adhered to the inner surface of the protective cylinder body 1, the thickness of the protective cylinder is thin, and the occupied volume is small, so that the internal space of the protective cylinder body 1 can be saved, and the occupied space of sensitive components of a submachine is increased; the PI electric heating film has high integration degree, so that the speed of pasting the PI electric heating film on the inner surface of the protective cylinder body 1 is high, and the operation of pasting the heating layer is convenient and simple; in addition, because the insulating layer of PI electric heat membrane is the polyimide film, it has good dielectric strength, excellent dielectric strength, higher heat-conduction efficiency to the heat-generating body of PI electric heat membrane has superstrong stability, consequently the type of jettisoninging unmanned vehicles protection section of thick bamboo of this application can provide good heating performance.
On the basis, the glass fiber reinforced plastic inner wall 101 and the glass fiber reinforced plastic outer wall 103 of the protection cylinder body 1 are both the inner wall and the outer wall of the protection cylinder body 1 formed by paving, thermally curing and laminating multiple layers of glass fiber reinforced plastic prepreg.
specifically, a glass fiber reinforced plastic prepreg is formed by reinforcing a resin matrix such as an unsaturated polyester, an epoxy resin, or a phenol resin matrix with glass fibers. Cutting the glass fiber reinforced plastic prepreg into a preset shape, and paving the cut glass fiber reinforced plastic prepreg on a protective cylinder mould, wherein the prefabricated protective cylinder body 1 is in a long and thin cylindrical shape, and the protective cylinder mould is also in a long and thin cylindrical shape. Pre-compaction is needed after the first layer of glass fiber reinforced plastic prepreg is paved, 3-4 layers of glass fiber reinforced plastic prepreg can be paved in the subsequent process, and then the glass fiber reinforced plastic inner wall 101 is formed by pre-compacting the plurality of layers of glass fiber reinforced plastic prepreg.
Then, the outer surface of the glass fiber reinforced plastic inner wall 101 is covered with an insulating layer 102, specifically, a polyurethane foam layer, or other insulating materials may be used. Wherein, polyurethane foam's thermal conductivity is lower, can guarantee higher thermal insulation performance to because polyurethane foam layer can be at the circumference of glass steel inner wall 101 complete cover surface, do not have the heat leak channel, higher thermal insulation performance of assurance that can be further.
After the outer surface of the glass fiber reinforced plastic inner wall 101 is covered with the insulating layer 102, glass fiber reinforced plastic prepreg is continuously paved and pre-compacted on the outer surface of the insulating layer 102, and the glass fiber reinforced plastic outer wall 103 is formed by pre-compacting multiple layers of glass fiber reinforced plastic prepreg. After the glass fiber reinforced plastic outer wall 103 is formed, the protection cylinder body 1 is packaged by a vacuum bag and is sent into an oven to be integrally cured and formed.
Preferably, referring to fig. 3, the insulating layer 102 is completely covered between the inner glass fiber reinforced plastic wall 101 and the outer glass fiber reinforced plastic wall 103, and the insulating layer 102 is chamfered at the opening of the protective cylinder body 1, so that the inner glass fiber reinforced plastic wall 101 and the outer glass fiber reinforced plastic wall 103 are directly bonded at the opening of the protective cylinder body 1 to form a complete sandwich structure of the insulating layer. Because the glass fiber reinforced plastic inner wall 101 and the glass fiber reinforced plastic outer wall 103 are directly bonded at the opening of the protection cylinder body 1, the edge folding effect is achieved at the opening of the protection cylinder body 1, and the strength of the opening of the protection cylinder body 1 is ensured.
On the basis, in order to ensure the flatness of the outer surface of the protection cylinder body 1, that is, the flatness of the outer surface of the outer glass fiber reinforced plastic wall 103, a pressure equalizing plate can be placed on the outer surface of the outer glass fiber reinforced plastic wall 103 when the protection cylinder body 1 is manufactured. The pressure equalizing plate is a metal plate with a smooth surface, is manufactured according to the outer surface of the protective cylinder, and is arranged on the outer surface of the glass fiber reinforced plastic prepreg paving layer before packaging and curing so as to ensure that the temperature and the pressure are uniformly transmitted in the curing process and the outer surface of the cured protective cylinder body 1 is smooth.
Because the inner wall and the outer wall of the protection cylinder body 1 are both made of glass fiber reinforced plastics, the thermal conductivity of the protection cylinder body is lower, and the thermal insulation performance of the protection cylinder is further ensured. And the protection section of thick bamboo body 1 of this application is through spreading the mode integrated into one piece of subsides, thermosetting, consequently the operation such as a preparation protection section of thick bamboo body 1 need not welding, riveting, has consequently just avoided the shortcoming that the preparation work load is big, the work degree of difficulty is high.
In addition, still because protection section of thick bamboo body 1 is spread on the protection section of thick bamboo mould and is pasted, thermosetting and the shaping, consequently fashioned internal surface of protection section of thick bamboo body 1 is comparatively smooth, and surface quality is higher, easily pastes PI electric heat membrane to functional subassembly such as guide rail draw-in groove is still easily installed.
On the basis of the above, the guide rail 2 having the guide groove or the guide protrusion facing the axial direction of the protection cylinder body 1 is further installed on the inner surface of the protection cylinder body 1 (i.e., the inner surface of the glass fiber reinforced plastic inner wall 101), and the extending direction of the guide rail 2 is the same as the axial direction of the protection cylinder body 1. If the guide rail 2 has a guide groove, the rail engaged with the guide groove and connected to the slave machine is a protrusion, and if the guide rail 2 has a guide protrusion, the rail engaged with the guide protrusion and connected to the slave machine is a groove. When the submachine flies, the rail of the submachine slides to the cylinder opening of the protection cylinder body 1 relative to the guide rail 2, so that the submachine flies.
Since the sub-machine is generally separated from the protection cylinder in advance when the sub-machine is separated from the protection cylinder, referring to fig. 1, when the inner diameter of the section of the cylinder body 11 of the protection cylinder body 1 facing the cylinder opening is larger than the inner diameter of the section of the cylinder body 12 of the protection cylinder body 1 facing the cylinder bottom (for example, the inner diameter of the cylinder body 11 is larger than the inner diameter of the cylinder body 12 by the thickness of the heat insulation layer 2), the guide rail 2 extends from the direction of the cylinder bottom of the protection cylinder body 1 to the position where the inner diameter of the cylinder opening of the protection cylinder body 1 is larger, so as to reduce the risk of the guide rail sliding and.
In addition, in order to fixedly connect the protection cylinder with the sub-machine, that is, to fix the protection cylinder body 1 with the sub-machine, please continue to refer to fig. 3, the edge of the cylinder opening of the protection cylinder body 1 may be connected with the flange 3, and the protection cylinder body 1 is connected to the sub-machine through the flange 3, so as to realize the butt joint of the protection cylinder and the sub-machine. Specifically, a through hole is provided at a position where the inner diameter of the cylinder opening of the protective cylinder body is increased, that is, at a position where the outer surface of the inner glass fiber reinforced plastic wall 101 and the inner surface of the outer glass fiber reinforced plastic wall 103 are bonded to each other, so that a bolt is inserted through the through hole and the through hole of the flange to fixedly connect the protective cylinder body 1 and the flange 3. In addition, a lifting lug is fixed on the outer surface of the protection cylinder body 1, so that the protection cylinder is fixed with the main machine through the lifting lug.
The application also provides a type of jettisoning unmanned vehicles, include: the primary machine, the secondary machine and the throwing type unmanned aerial vehicle protection barrel provided by the embodiment; the mouth of the throwing type unmanned aerial vehicle protection barrel is in butt joint with the submachine, and a preset part of the submachine is arranged in the throwing type unmanned aerial vehicle protection barrel; the lifting lug on the outer surface of the protection cylinder is fixedly connected with the master machine so as to hang the slave machine on the master machine.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential attributes thereof. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.
Claims (8)
1. A jettisoning type unmanned vehicles protection section of thick bamboo which characterized in that includes: the heating layer is covered on the inner surface of the protection cylinder body; the protective cylinder body sequentially comprises a glass fiber reinforced plastic inner wall, a heat insulation layer and a glass fiber reinforced plastic outer wall from inside to outside, the glass fiber reinforced plastic inner wall and the glass fiber reinforced plastic outer wall are clamped on the heat insulation layer, and the glass fiber reinforced plastic inner wall, the heat insulation layer and the glass fiber reinforced plastic outer wall are integrally formed.
2. The tossing-type unmanned aerial vehicle protection cylinder according to claim 1, wherein the heat insulation layer is a polyurethane foam layer.
3. The tossing-type unmanned aerial vehicle protection cartridge of claim 1, wherein the heating layer is a PI electrothermal film layer.
4. The tossing-type unmanned aerial vehicle protection cylinder according to any one of claims 1 to 3, wherein the thickness ratio of the glass fiber reinforced plastic inner wall, the insulating layer and the glass fiber reinforced plastic outer wall is 1:3: 1.
5. The tossing-type unmanned aerial vehicle protection cylinder according to any one of claims 1 to 3, wherein a guide groove or a guide protrusion is installed on the inner surface of the glass fiber reinforced plastic inner wall and faces to a guide rail of the protection cylinder body in the axial direction, and the extension direction of the guide rail is the same as the axial direction of the protection cylinder body.
6. The tossing-type unmanned aerial vehicle protection cylinder according to any one of claims 1 to 3, wherein the insulation layer is completely covered between the inner glass fiber reinforced plastic wall and the outer glass fiber reinforced plastic wall, and the insulation layer is chamfered at the cylinder opening position of the protection cylinder body, so that the inner glass fiber reinforced plastic wall and the outer glass fiber reinforced plastic wall are directly bonded at the cylinder opening position of the protection cylinder body to form a complete sandwich structure of the insulation layer made of glass fiber reinforced plastic.
7. The tossing-type unmanned aerial vehicle protection cylinder according to any one of claims 1 to 3, wherein a through hole is formed in a cylinder opening position of the protection cylinder, and a bolt is inserted through the through hole and the through hole of the flange to fixedly connect the protection cylinder body and the flange.
8. A tossing-type unmanned aerial vehicle, comprising: a mother machine, a son machine and the casting type unmanned aerial vehicle protection barrel of any one of claims 1 to 7; a cylinder opening of the casting type unmanned aerial vehicle protection cylinder is in butt joint with the submachine, and a preset part of the submachine is arranged in the casting type unmanned aerial vehicle protection cylinder; the lifting lug fixed on the outer surface of the protection cylinder is fixedly connected with the master machine so as to mount the sub machine on the master machine.
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CN201910955221.7A CN110562462A (en) | 2019-10-09 | 2019-10-09 | Throwing type unmanned vehicles and a protection section of thick bamboo thereof |
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Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
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CN2533371Y (en) * | 2001-07-25 | 2003-01-29 | 四川中嘉玻璃钢有限公司 | Heat insulation layer assembly for composite heat insulation pipe |
AU2011101594A4 (en) * | 2011-12-05 | 2012-01-12 | Zhifu Xie | A kind of innovative glass fiber reinforced plastic multi-layer heat insulating and preserving compound pipe |
CN202927295U (en) * | 2012-11-05 | 2013-05-08 | 西安天嘉蓝环保科技有限责任公司 | Warm-keeping and corrosion-resistant glass steel tube |
CN108100287A (en) * | 2017-11-23 | 2018-06-01 | 北京航空航天大学 | A kind of unmanned plane space base emitter |
CN210618478U (en) * | 2019-10-09 | 2020-05-26 | 北京中航智科技有限公司 | Throwing type unmanned vehicles and a protection section of thick bamboo thereof |
-
2019
- 2019-10-09 CN CN201910955221.7A patent/CN110562462A/en active Pending
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN2533371Y (en) * | 2001-07-25 | 2003-01-29 | 四川中嘉玻璃钢有限公司 | Heat insulation layer assembly for composite heat insulation pipe |
AU2011101594A4 (en) * | 2011-12-05 | 2012-01-12 | Zhifu Xie | A kind of innovative glass fiber reinforced plastic multi-layer heat insulating and preserving compound pipe |
CN202927295U (en) * | 2012-11-05 | 2013-05-08 | 西安天嘉蓝环保科技有限责任公司 | Warm-keeping and corrosion-resistant glass steel tube |
CN108100287A (en) * | 2017-11-23 | 2018-06-01 | 北京航空航天大学 | A kind of unmanned plane space base emitter |
CN210618478U (en) * | 2019-10-09 | 2020-05-26 | 北京中航智科技有限公司 | Throwing type unmanned vehicles and a protection section of thick bamboo thereof |
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