CN108569410B - Rotor unmanned aerial vehicle power generation facility mount pad - Google Patents
Rotor unmanned aerial vehicle power generation facility mount pad Download PDFInfo
- Publication number
- CN108569410B CN108569410B CN201810247488.6A CN201810247488A CN108569410B CN 108569410 B CN108569410 B CN 108569410B CN 201810247488 A CN201810247488 A CN 201810247488A CN 108569410 B CN108569410 B CN 108569410B
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- Prior art keywords
- hole
- motor
- power generation
- connecting body
- generation device
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- 238000010248 power generation Methods 0.000 title claims abstract description 26
- 239000000758 substrate Substances 0.000 claims abstract description 48
- 238000009434 installation Methods 0.000 claims abstract description 45
- 230000007704 transition Effects 0.000 claims description 18
- 230000005540 biological transmission Effects 0.000 claims description 13
- 239000000446 fuel Substances 0.000 description 15
- 239000007858 starting material Substances 0.000 description 4
- 208000016261 weight loss Diseases 0.000 description 4
- 239000013585 weight reducing agent Substances 0.000 description 4
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 238000009423 ventilation Methods 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000011900 installation process Methods 0.000 description 1
- 239000000126 substance 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Abstract
The invention discloses a rotor unmanned aerial vehicle power generation device mounting seat, which comprises a connecting substrate, a connecting body and a motor mounting seat; a power shaft through hole and a first positioning piece are arranged on the connecting substrate; the connecting body is of a hollow columnar structure, and a second positioning piece is arranged on the connecting body; the motor mounting seat is of a hollow columnar structure; the first positioning piece is used for determining the installation position of the connecting body on the connecting substrate, so that the central axis of the power shaft through hole and the central axis of the connecting body are on the same straight line; the second locating piece is used for determining the installation position of the connecting body on the motor installation seat, so that the central axis of the connecting body and the central axis of the motor installation seat are on the same straight line. The coaxial precision between each part of the power generation device is guaranteed, and the coaxial precision is good, the strength is good, the weight is light, and the like.
Description
Technical Field
The invention relates to the technical field of rotor unmanned aerial vehicles, in particular to a rotor unmanned aerial vehicle power generation device mounting seat.
Background
The oil-electricity hybrid power rotor unmanned aerial vehicle gradually becomes an important development direction of the industrial rotor unmanned aerial vehicle because of the advantages of large carrying capacity, long endurance time and the like. The power generation system adopts a generator driven by a fuel engine, and the generator generates power to provide power for the power system. In order to ensure that the fuel generator can stably operate when the clutch drives the generator to generate electricity, the coaxial between the clutch of the fuel engine and the generator is required to be well ensured. In order to achieve the above objective and to ensure that the installation process is as simple, convenient and rapid as possible, research into the installation seat of the rotary wing unmanned aerial vehicle power generation device is required.
Disclosure of Invention
The technical problem to be solved by the invention is as follows: aiming at the technical problems in the prior art, the invention provides the rotor unmanned aerial vehicle power generation device mounting seat which has the advantages of simple and reasonable structure, convenience in mounting, good strength and light weight, and can well ensure the coaxial precision among all parts of the power generation device.
In order to solve the technical problems, the technical scheme provided by the invention is as follows: a rotor unmanned aerial vehicle power generation device mounting seat comprises a connecting substrate, a connecting body and a motor mounting seat;
the connecting substrate is provided with a power shaft through hole and a first positioning piece;
the connecting body is of a hollow columnar structure, and a second positioning piece is arranged on the connecting body;
the motor mounting seat is of a hollow columnar structure;
the first positioning piece is used for determining the installation position of the connecting body on the connecting substrate, so that the central axis of the power shaft through hole and the central axis of the connecting body are in the same straight line;
the second positioning piece is used for determining the installation position of the connecting body on the motor installation seat, so that the central axis of the connecting body and the central axis of the motor installation seat are on the same straight line.
Further, a power shaft limiting hole is further formed in the connecting substrate and used for positioning and mounting the connecting substrate.
Further, the starting motor installation position is further arranged on the connecting substrate, and the starting motor installation position comprises a motor shaft through hole and a motor fixing screw hole.
Further, a transmission gear hole is further formed in the connecting substrate, and the transmission gear hole is located between the power shaft through hole and the motor shaft through hole.
Further, the connection base plate is circular with a protruding portion, and the starting motor mounting position is located on the protruding portion.
Further, a first opening is formed in the connecting portion of the connecting body and the starting motor installation position on the side wall of the connecting end of the connecting body and the connecting substrate.
Further, a plurality of first weight-reducing windows are formed in the side wall of the connector, and the first weight-reducing windows are uniformly distributed on the side wall.
Further, the thickness of the side walls at the two ends of the connecting body is larger than that of the side walls of the middle part; and a mounting hole is formed in one end connected with the motor mounting seat.
Further, the motor mounting seat is of a columnar structure with one end open, and a third positioning piece is arranged on the inner side of the end face.
Further, a plurality of second weight reduction windows are arranged on the side wall of the motor mounting seat, and the second weight reduction windows are uniformly distributed on the side wall.
Further, the device also comprises a transition connecting plate, wherein a first mounting hole and a second mounting hole are formed in the transition connecting plate, the first mounting hole is used for fixedly mounting the connecting substrate, and the second mounting hole is used for positioning and mounting the transition connecting plate; and a notch is formed in the transition connecting plate.
Compared with the prior art, the invention has the advantages that:
1. the invention adopts the installation mode of combining the connecting substrate, the connecting body and the motor installation seat, can conveniently realize the installation of all parts of the power generation device, and simultaneously realizes the positioning connection among all parts by the positioning piece, thereby being capable of well ensuring the coaxiality among all parts of the power generation device and having good coaxiality precision.
2. The connecting substrate is provided with the starting motor installation position, so that the electric starting of the power generation device can be conveniently realized, and the restarting of the rotor unmanned aerial vehicle during the air parking is realized.
3. According to the connecting substrate, the connecting body and the motor mounting seat, the weight-reducing window is formed in the connecting substrate, the connecting body and the motor mounting seat, and the connecting substrate is made of aluminum alloy, so that the connecting strength is ensured, and meanwhile, the weight is reduced.
Drawings
Fig. 1 is a perspective view of a structure of an embodiment of the present invention.
Fig. 2 is a side view of the structure of an embodiment of the present invention.
Fig. 3 is a cross-sectional view of an embodiment of the present invention.
Fig. 4 is a schematic structural diagram of a connection substrate according to an embodiment of the invention.
FIG. 5 is a schematic view of a connector structure according to an embodiment of the present invention.
Fig. 6 is a schematic view of a motor mounting base according to an embodiment of the present invention.
Fig. 7 is a schematic view of a motor mount for a single cylinder engine according to an embodiment of the present invention.
FIG. 8 is a schematic diagram of a motor mount for a dual cylinder engine in accordance with an embodiment of the present invention.
Legend description: 1. a connection substrate; 101. a power shaft via hole; 102. a first positioning member; 103. a power shaft limiting hole; 104. a motor shaft via hole; 105. a motor fixing screw hole; 106. a drive gear hole; 2. a connecting body; 201. a second positioning member; 202. a first opening; 203. 103 th weight-reduction window; 204. a mounting hole; 3. a motor mounting seat; 301. a third positioning member; 302. a second weight-reduction window; 4. a transition connecting plate; 401. a first mounting hole; 402. and a second mounting hole.
Detailed Description
The invention is further described below in connection with the drawings and the specific preferred embodiments, but the scope of protection of the invention is not limited thereby.
The rotor unmanned aerial vehicle power generation device mounting seat comprises a connecting substrate 1, a connecting body 2 and a motor mounting seat 3; a power shaft through hole 101 and a first positioning piece 102 are arranged on the connecting substrate 1; the connecting body 2 is of a hollow columnar structure, and a second positioning piece 201 is arranged on the connecting body 2; the motor mounting seat 3 is of a hollow columnar structure; the first positioning piece 102 is used for determining the installation position of the connector 2 on the connection substrate 1, so that the central axis of the power shaft via hole 101 and the central axis of the connector 2 are on the same straight line; the second positioning member 201 is used to determine the mounting position of the connection body 2 on the motor mount 3 such that the central axis of the connection body 2 and the central axis of the motor mount 3 are on the same straight line. The connecting substrate 1 is also provided with a power shaft limiting hole 103, and the power shaft limiting hole 103 is used for positioning and mounting the connecting substrate 1. The connection base plate 1 is mounted to the engine or to the transition connection plate 4. It should be noted that, the first positioning member 201 and the second positioning member 202 are used to achieve positioning and installation between two components, and various specific implementation manners may be adopted, such as a protrusion or recess structure matched between two components connected to each other, a positioning hole, etc. As shown in fig. 4, the first positioning member 102 in this embodiment is a positioning hole, and the positioning hole also has the fixing function of the connecting body 2 and the connecting substrate 1.
Fig. 1, 2 and 3 are schematic views of the installation base of the rotor unmanned aerial vehicle power generation device according to the present embodiment from different angles of view in the installed state. Fig. 4 is a schematic structural view of the connection substrate 1. In the installed state, the fixed installation connection substrate 1 is installed on one side of the power output shaft of the fuel engine, and the central axis of the power shaft through hole 101 and the axis of the power output shaft of the fuel engine are on the same straight line through the installation position determined by the power shaft limiting hole 103. In the installation state, the power output shaft of the fuel engine is arranged in the connecting body 2, the generator is arranged in the motor installation seat 3, and the clutch realizes the connection between the power output shaft of the fuel engine and the generator shaft. The transmission shafts of the fuel engine, the clutch and the generator are positioned on the same straight line through the connecting base plate 1, the connecting body 2 and the motor mounting seat 3.
As shown in fig. 4, in the present embodiment, a starter motor mounting position is further provided on the connection substrate 1, and the starter motor mounting position includes a motor shaft via hole 104 and a motor fixing screw hole 105. The connection substrate 1 is further provided with a transmission gear hole 106, and the transmission gear hole 106 is located between the power shaft through hole 101 and the motor shaft through hole 104. The connection substrate 1 is circular with a protruding portion where the starter motor mounting position is located. Under the installation state, an electric starting gear is arranged on a power output shaft of the fuel engine, a starting motor is arranged at a motor installation position of the connecting substrate 1, a gear is also arranged on an output shaft of the starting motor, and the gear of the starting motor is directly or indirectly meshed with a starting gear on the fuel engine to transmit the power of the starting motor to the fuel engine, so that the electric starting of the fuel engine is realized. The starting motor is arranged on the connecting substrate 1, so that the stability of the installation position of the starting motor can be ensured, and the stability of an electric starting system can be improved. The transmission gear hole 106 is arranged on the connecting substrate 1, and a transmission gear can be arranged between a gear of the starting motor and a starting gear of the fuel engine to adjust the transmission ratio of the starting motor, so that the starting motors with different power can be flexibly selected to realize electric starting. The transmission gear is a unidirectional transmission gear.
In this embodiment, a first opening 202 is provided at a connection portion of the connection body 2 and the starting motor mounting position on a side wall of the connection end of the connection body 2 and the connection substrate 1. Installation of the starter motor to the transmission of the fuel engine is thereby facilitated by the first opening 202. A plurality of first weight-reducing windows 203 are formed in the side wall of the connector 2, and the first weight-reducing windows 203 are uniformly distributed on the side wall. The connecting body 2 is preferably of cylindrical configuration. The thickness of the side walls at the two ends of the connector 2 is larger than that of the side wall of the middle part; a mounting hole 204 is provided at one end connected to the motor mount 3. The cylindrical structure is adopted, and the first weight-reducing window 203 is arranged, so that on one hand, the strength of the connector can be ensured, and the connector 2 can not deform; on the other hand, the weight of the connector 2 can be reduced, so that the requirement of the rotor unmanned aerial vehicle on the load can be met.
In this embodiment, the second positioning member 201 on the connector 2 is used to define the mounting position of the motor mount 3, and may take various forms. As shown in the sectional view of fig. 3, the second positioning member 201 is a protrusion that mates with the motor mount 3, by which the mounting position of the motor mount 3 is determined. Alternatively, as shown in fig. 5, the second positioning member 201 is a bolt hole through which the mounting position of the motor mount 3 is determined, and the bolt hole is also used to fix the motor mount 3 to the connection body 2 by a bolt.
In this embodiment, as shown in fig. 6, the motor mount 3 has a columnar structure with one end open, and a third positioning member 301 is disposed inside the end surface. The mounting position of the generator in the motor mount 3 can be defined by the third positioning member 301, so that coaxiality among the fuel engine, the clutch and the generator is ensured. A plurality of second weight-reducing windows 302 are arranged on the side wall of the motor mounting seat 3, and the second weight-reducing windows 302 are uniformly distributed on the side wall. The open end of the motor mounting seat 3 is connected with the connector 2, and a plurality of ventilation holes are formed in the end face of the other end of the motor mounting seat so as to facilitate ventilation and heat dissipation of the motor in the motor mounting seat 3. The second weight-reducing windows 302 are uniformly distributed on the side wall of the motor mounting seat 3, and the axial upright posts and the radial connecting ribs are formed on the side wall, so that the weight of the motor mounting seat 3 is reduced, and meanwhile, the strength of the motor mounting seat 3 is ensured.
In the present embodiment, as shown in fig. 7, when a single-cylinder engine is used, the connection substrate 1 may be directly fixedly mounted on the engine. The connecting base plate 1, the connecting body 2 and the motor mounting seat 3 are sequentially connected. The coaxial installation of the engine, the clutch and the generator is realized.
As shown in fig. 8, in the case of adopting a two-cylinder engine, limited by the installation position of the engine, for more convenient installation of equipment, in this embodiment, the device further comprises a transition connection board 4, wherein a first installation hole 401 and a second installation hole 402 are arranged on the transition connection board 4, the first installation hole 401 is used for fixedly installing the connection substrate 1, and the second installation hole 402 is used for positioning and installing the transition connection board 4; the transition connecting plate 4 is provided with a notch. The transition connection plate 4 is firstly installed on the double-cylinder engine, then the connection base plate 1 is installed on the transition connection plate 4, and the base plate 1 is installed on the double-cylinder engine through the transition connection plate 4. In the installation state, the notch on the transition connecting plate 4 is matched with the installation phase of the starting motor on the connecting substrate 1, so that the installation of the starting motor is convenient.
In this embodiment, the connection substrate 1, the connection body 2 and the motor mount 3 are all made of aluminum alloy, in particular, aviation aluminum.
The foregoing is merely a preferred embodiment of the present invention and is not intended to limit the present invention in any way. While the invention has been described with reference to preferred embodiments, it is not intended to be limiting. Therefore, any simple modification, equivalent variation and modification of the above embodiments according to the technical substance of the present invention shall fall within the scope of the technical solution of the present invention.
Claims (11)
1. The utility model provides a rotor unmanned aerial vehicle power generation facility mount pad which characterized in that: comprises a connecting substrate (1), a connecting body (2) and a motor mounting seat (3);
a power shaft through hole (101) and a first positioning piece (102) are arranged on the connecting substrate (1);
the connecting body (2) is of a hollow columnar structure, and a second positioning piece (201) is arranged on the connecting body (2);
the motor mounting seat (3) is of a hollow columnar structure;
the first positioning piece (102) is used for determining the installation position of the connecting body (2) on the connecting substrate (1) so that the central axis of the power shaft through hole (101) and the central axis of the connecting body (2) are on the same straight line;
the second positioning piece (201) is used for determining the installation position of the connecting body (2) on the motor installation seat (3) so that the central axis of the connecting body (2) and the central axis of the motor installation seat (3) are on the same straight line;
the first positioning piece (102) and the second positioning piece (201) are used for positioning and mounting between two parts.
2. The rotary-wing unmanned aerial vehicle power generation device mount according to claim 1, wherein: the connecting substrate (1) is further provided with a power shaft limiting hole (103), and the power shaft limiting hole (103) is used for positioning and mounting the connecting substrate (1).
3. The rotary-wing unmanned aerial vehicle power generation device mount according to claim 2, wherein: the connecting substrate (1) is further provided with a starting motor installation position, and the starting motor installation position comprises a motor shaft through hole (104) and a motor fixing screw hole (105).
4. The rotary-wing drone power generation device mount of claim 3, wherein: the connecting substrate (1) is further provided with a transmission gear hole (106), and the transmission gear hole (106) is located between the power shaft through hole (101) and the motor shaft through hole (104).
5. The rotary-wing unmanned aerial vehicle power generation device mount pad of claim 4, wherein: the connecting base plate (1) is circular and provided with a protruding part, and the starting motor installation position is positioned on the protruding part.
6. The rotary-wing unmanned aerial vehicle power generation device mount pad of claim 4, wherein: the connecting body (2) is provided with a first opening (203) on the side wall of one end connected with the connecting substrate (1) and at the joint of the connecting body and the starting motor installation position.
7. The rotary-wing unmanned aerial vehicle power generation device mount according to claim 6, wherein: a plurality of first weight-reducing windows (203) are formed in the side wall of the connecting body (2), and the first weight-reducing windows (203) are uniformly distributed on the side wall.
8. The rotary-wing unmanned aerial vehicle power generation device mount according to claim 7, wherein: the thickness of the side walls at the two ends of the connecting body (2) is larger than that of the side wall of the middle part; and a mounting hole (204) is formed at one end connected with the motor mounting seat (3).
9. The rotary-wing drone power generation device mount of any one of claims 1 to 8, wherein: the motor mounting seat (3) is of a columnar structure with one end open, and a third positioning piece (301) is arranged on the inner side of the end face of the motor mounting seat (3).
10. The rotary-wing drone power generation device mount of claim 9, wherein: the side wall of the motor mounting seat (3) is provided with a plurality of second weight-reducing windows (302), and the second weight-reducing windows (302) are uniformly distributed on the side wall.
11. The rotary-wing drone power generation device mount of any one of claims 1 to 8, wherein: the connecting device comprises a connecting substrate (1), and is characterized by further comprising a transition connecting plate (4), wherein a first mounting hole (401) and a second mounting hole (402) are formed in the transition connecting plate (4), the first mounting hole (401) is used for fixedly mounting the connecting substrate (1), and the second mounting hole (402) is used for positioning and mounting the transition connecting plate (4); and a notch is formed in the transition connecting plate (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810247488.6A CN108569410B (en) | 2018-03-23 | 2018-03-23 | Rotor unmanned aerial vehicle power generation facility mount pad |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810247488.6A CN108569410B (en) | 2018-03-23 | 2018-03-23 | Rotor unmanned aerial vehicle power generation facility mount pad |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108569410A CN108569410A (en) | 2018-09-25 |
| CN108569410B true CN108569410B (en) | 2023-10-27 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201810247488.6A Active CN108569410B (en) | 2018-03-23 | 2018-03-23 | Rotor unmanned aerial vehicle power generation facility mount pad |
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Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN200940642Y (en) * | 2006-06-16 | 2007-08-29 | 泰豪科技股份有限公司 | Coupling pin for connecting generator and diesel engine |
| CN200958422Y (en) * | 2006-09-28 | 2007-10-10 | 科泰电源设备（上海）有限公司 | Nuclear safety diesel-oil generator set |
| CN201355299Y (en) * | 2008-12-18 | 2009-12-02 | 南车洛阳机车有限公司 | Elastic coupling dynamic balancing mandrel for diesel locomotive diesel power generating set |
| CN101826773A (en) * | 2009-03-05 | 2010-09-08 | 中国船舶重工集团公司第七一一研究所 | Pulse load genset |
| CN203859625U (en) * | 2014-03-31 | 2014-10-01 | 北汽大洋电机科技有限公司 | Motor and gearbox integration structure |
| CN104085295A (en) * | 2014-07-03 | 2014-10-08 | 广州电力机车有限公司 | Articulated dump truck power system based on torque transmission device |
| CN104097495A (en) * | 2014-07-03 | 2014-10-15 | 广州电力机车有限公司 | Method and tool for mounting diesel engine and generator of articulated dumper |
| CN104279941A (en) * | 2014-10-28 | 2015-01-14 | 南车戚墅堰机车有限公司 | Diesel generating set coaxiality measuring method |
| CN205135803U (en) * | 2015-11-24 | 2016-04-06 | 白云龙 | Full opposition of level increases journey ware |
| CN206041739U (en) * | 2016-09-21 | 2017-03-22 | 华晨汽车集团控股有限公司 | Increase rotor installation component of form hybrid vehicle generator |
| CN208036629U (en) * | 2018-03-23 | 2018-11-02 | 中科灵动航空科技成都有限公司 | A kind of rotor wing unmanned aerial vehicle power generator mounting base |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US9193451B2 (en) * | 2013-04-22 | 2015-11-24 | Ival O. Salyer | Aircraft using turbo-electric hybrid propulsion system for multi-mode operation |
-
2018
- 2018-03-23 CN CN201810247488.6A patent/CN108569410B/en active Active
Patent Citations (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN200940642Y (en) * | 2006-06-16 | 2007-08-29 | 泰豪科技股份有限公司 | Coupling pin for connecting generator and diesel engine |
| CN200958422Y (en) * | 2006-09-28 | 2007-10-10 | 科泰电源设备（上海）有限公司 | Nuclear safety diesel-oil generator set |
| CN201355299Y (en) * | 2008-12-18 | 2009-12-02 | 南车洛阳机车有限公司 | Elastic coupling dynamic balancing mandrel for diesel locomotive diesel power generating set |
| CN101826773A (en) * | 2009-03-05 | 2010-09-08 | 中国船舶重工集团公司第七一一研究所 | Pulse load genset |
| CN203859625U (en) * | 2014-03-31 | 2014-10-01 | 北汽大洋电机科技有限公司 | Motor and gearbox integration structure |
| CN104085295A (en) * | 2014-07-03 | 2014-10-08 | 广州电力机车有限公司 | Articulated dump truck power system based on torque transmission device |
| CN104097495A (en) * | 2014-07-03 | 2014-10-15 | 广州电力机车有限公司 | Method and tool for mounting diesel engine and generator of articulated dumper |
| CN104279941A (en) * | 2014-10-28 | 2015-01-14 | 南车戚墅堰机车有限公司 | Diesel generating set coaxiality measuring method |
| CN205135803U (en) * | 2015-11-24 | 2016-04-06 | 白云龙 | Full opposition of level increases journey ware |
| CN206041739U (en) * | 2016-09-21 | 2017-03-22 | 华晨汽车集团控股有限公司 | Increase rotor installation component of form hybrid vehicle generator |
| CN208036629U (en) * | 2018-03-23 | 2018-11-02 | 中科灵动航空科技成都有限公司 | A kind of rotor wing unmanned aerial vehicle power generator mounting base |
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| Publication number | Publication date |
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| CN108569410A (en) | 2018-09-25 |
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