CN107097943A - A kind of horn structure for being used to combine gyroplane - Google Patents
A kind of horn structure for being used to combine gyroplane Download PDFInfo
- Publication number
- CN107097943A CN107097943A CN201710354684.9A CN201710354684A CN107097943A CN 107097943 A CN107097943 A CN 107097943A CN 201710354684 A CN201710354684 A CN 201710354684A CN 107097943 A CN107097943 A CN 107097943A
- Authority
- CN
- China
- Prior art keywords
- rotor
- motor
- horn
- undercarriage
- column construction
- 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
Links
- 238000010276 construction Methods 0.000 claims abstract description 23
- 239000003795 chemical substances by application Substances 0.000 claims description 3
- 238000004519 manufacturing process Methods 0.000 abstract description 4
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 238000005194 fractionation Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
- B64C25/12—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like sideways
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
- B64C27/14—Direct drive between power plant and rotor hub
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Abstract
The invention discloses a kind of horn structure for being used to combine gyroplane, it is related to unmanned vehicle field.The horn structure includes：Horn, rotor, rotor carry end and horn connector；One end of the horn sets horn connector, and the other end sets rotor to carry end；The rotor is fixed on the rotor and carried on end；The agent structure that the rotor carries end is column construction；Motor is set in the inner chamber of the column construction, and the motor is connected with the rotor.Structure of the present invention realizes many rotor single-blade horns of different task load and is total to the Rapid Combination of paddle structure up and down, it can be changed into the rotor of three axle six, the rotor of four axle four from the rotor of three axle three and be changed into the rotor of four axle eight, the rotor of six axle six to be changed into the rotor of six axle 12 according to unmanned plane is realized the need for mission payload, aircraft bearing capacity is improved, the production cost of gyroplane is reduced and improves the efficiency of unmanned plane outdoor study task.
Description
Technical field
The present invention relates to unmanned vehicle field, more particularly to a kind of horn structure for being used to combine gyroplane.
Background technology
Unmanned plane have flexible light, lightweight, small volume, rapid-assembling/disassembling, as needed can carry different task set
It is standby, the features such as the manufacturing cycle is short, largely used in military markets and commercial market.
But, with the fast development of unmanned flight's technology, more and more higher is required to unmanned plane.Existing unmanned plane is single-blade machine
Arm and it can not be changed according to the rotor that unmanned plane is realized the need for mission payload.
The content of the invention
It is an object of the invention to provide a kind of horn structure for being used to combine gyroplane, so as to solve to deposit in the prior art
Foregoing problems.
To achieve these goals, the horn structure of the present invention for being used to combine gyroplane, the horn structure includes：
Horn, rotor, rotor carry end and horn connector；One end of the horn sets horn connector, and the other end sets rotor to carry
End；The rotor is fixed on the rotor and carried on end；The agent structure that the rotor carries end is column construction；The column construction
Inner chamber in motor is set, the motor is connected with the rotor.
Preferably, when the quantity of the rotor is 1, the upper bottom surface of the column construction sets rotor anchor tip, institute
Rotor is stated to be fixed on the rotor anchor tip；When the quantity of the rotor is 2, the upper and lower bottom surface of the column construction
On be respectively provided with rotor anchor tip, fix a rotor on each rotor anchor tip.
Preferably, when the quantity of the rotor is 1, the column construction is divided into motor waterproof from top to bottom
Lid, motor cabinet and lower bottom cover；The motor is set between the upper motor waterproof cover and the motor cabinet, and the motor is fixed on
On the motor cabinet；Electron speed regulator is set between the motor cabinet and the lower bottom cover.
Preferably, when the quantity of the rotor is 2, the column construction is divided into motor waterproof from top to bottom
Lid, motor cabinet and lower motor waterproof cover；The motor, the motor are set between the upper motor waterproof cover and the motor cabinet
It is fixed on the motor cabinet；Electron speed regulator is set between the motor cabinet and the lower motor waterproof cover.
Preferably, indicator lamp, the indicator lamp and the motor connection are set on the outer wall of the column construction.
Preferably, the horn structure also includes undercarriage, and by horizontal folding part, the undercarriage connects with the horn
Fitting is detachably connected.
It is highly preferred that the undercarriage includes undercarriage leg, undercarriage base and the undercarriage rubber base being sequentially arranged；
The fixed connector of the horizontal folding part is fixedly connected with the undercarriage leg and the horn connector respectively；The water
Flexible connection head and the horn connector pin connection of flat-folded overlapping piece.
The beneficial effects of the invention are as follows：
Structure of the present invention realizes many rotor single-blade horns of different task load and is total to quick group of paddle structure up and down
Close, can realize that unmanned plane is changed into the rotor of three axle six, the rotor of four axle four from the rotor of three axle three and is changed into according to the need for mission payload
The rotor of four axle eight, the rotor of six axle six are changed into the rotor of six axle 12, improve aircraft bearing capacity, reduce gyroplane production cost and
Improve the efficiency of unmanned plane outdoor study task.
Brief description of the drawings
Fig. 1 is the horn structural representation for being used to combine gyroplane of no undercarriage；
Fig. 2 is the single-blade horn structural representation for being used to combine gyroplane of no undercarriage；
Fig. 3 is the double oar horn structural representations for being used to combine gyroplane of no undercarriage；
Fig. 4 is motor cabinet structural representation；
Fig. 5 is motor waterproof cover structural representation；
Fig. 6 is that the combination of double oar horn structure undercarriages in the deployed state for combining gyroplane for having undercarriage is shown
It is intended to；
Fig. 7 is that the fractionation of double oar horn structure undercarriages in the deployed state for combining gyroplane for having undercarriage is shown
It is intended to；
Fig. 8 is the signal of undercarriage in a folded configuration in the double oar horn structures for combining gyroplane for have undercarriage
Figure；
Fig. 9 is the unmanned plane structural representation of the double oar horn structures of the rotor of three axle six；
Figure 10 is the unmanned plane structural representation of the rotor single-blade horn structure of six axle six.
Embodiment
In order to make the purpose , technical scheme and advantage of the present invention be clearer, below in conjunction with accompanying drawing, the present invention is entered
Row is further described.It should be appreciated that embodiment described herein is not used to only to explain the present invention
Limit the present invention.
Embodiment
Reference picture 1, the horn structure for combining gyroplane is used for described in the present embodiment, and the horn structure includes：Horn 1,
Rotor 2, rotor carry end 3 and horn connector 4；One end of the horn 1 sets horn connector 4, and the other end sets rotor to carry
End 3；The rotor 2 is fixed on the rotor and carried on end 3；The agent structure that the rotor carries end 3 is column construction；The cylindricality
Setting motor 3-4 in the inner chamber of structure, the motor 3-4 are connected with the rotor 2.Horn structure described in the present embodiment is without rising and falling
Frame.
Explanation, which is explained in more detail, is：
(1) single-blade horn structure and double oar horn structures
1st, single-blade horn structure
Reference picture 2, the rotor quantity of single-blade horn structure is 1, and the upper bottom surface of the column construction sets rotor to fix
Joint, the rotor is fixed on the rotor anchor tip；The column construction is divided into motor waterproof from top to bottom
Cover 3-1, motor cabinet 3-2 and lower bottom cover 3-3；The motor is set between the upper motor waterproof cover 3-1 and the motor cabinet 3-2
3-4, the motor 3-4 is fixed on the motor cabinet 3-2；Electronics is set between the motor cabinet 3-2 and the lower bottom cover 3-3
Speed regulator 3-5.
2nd, double oar horn structures
Reference picture 3, the rotor quantity of double oar horn structures is to be respectively provided with rotation on 2, the upper and lower bottom surface of the column construction
A rotor is fixed on wing anchor tip, each rotor anchor tip.The column construction is from top to bottom successively
It is divided into motor waterproof cover 3-1, motor cabinet 3-2 and lower motor waterproof cover 3-6；The upper motor waterproof cover 3-1 and the motor
The motor 3-4, the motor 3-4 is set to be fixed on the motor cabinet 3-2 between seat 3-2；The motor cabinet 3-2 with it is described
Electron speed regulator 3-5 is set between lower motor waterproof cover 3-6.
The structural representation of motor cabinet is as shown in figure 4, set dentalation on the outer wall of the motor cabinet, dentalation is used
In increase motor radiating area, facilitate motor radiating.The structural representation of upper and lower motor waterproof cover is as shown in Figure 5；For motor
With electron speed regulator waterproof.
(2) on the other structures on column construction
Indicator lamp is set on the outer wall of the column construction, and the indicator lamp is connected with the motor 3-4.
Embodiment 2
Reference picture 6, the present embodiment and the difference of embodiment 1 are：Horn structure has undercarriage 5 described in the present embodiment, leads to
Horizontal folding part 6 is crossed, the undercarriage is detachably connected with the horn connector.
Reference picture 7 and 8, the undercarriage 5 includes undercarriage leg 5-1, the undercarriage base 5-2 being sequentially arranged and risen and fallen
Frame rubber base 5-3；The fixed connector of the horizontal folding part 6 is connected with the undercarriage leg 5-1 and the horn respectively
Part 4 is fixedly connected；Flexible connection head and the horn connector pin connection of the horizontal folding part 6.Undercarriage is as needed
Rapid deployment and folding are realized by Quick-release pin.
By using above-mentioned technical proposal disclosed by the invention, following beneficial effect has been obtained：
Structure of the present invention realizes many rotor single-blade horns of different task load and is total to quick group of paddle structure up and down
Close, can realize that unmanned plane is changed into the rotor of three axle six, the rotor of four axle four from the rotor of three axle three and is changed into according to the need for mission payload
The rotor of four axle eight, the rotor of six axle six are changed into the rotor of six axle 12, improve aircraft bearing capacity, reduce gyroplane production cost and
Improve the efficiency of unmanned plane outdoor study task.
Described above is only the preferred embodiment of the present invention, it is noted that for the ordinary skill people of the art
For member, under the premise without departing from the principles of the invention, some improvements and modifications can also be made, these improvements and modifications also should
Depending on protection scope of the present invention.
Claims (7)
1. a kind of horn structure for being used to combine gyroplane, it is characterised in that the horn structure includes：Horn, rotor, rotor
Carry end and horn connector；
One end of the horn sets horn connector, and the other end sets rotor to carry end；The rotor is fixed on the rotor and carried
On end；The agent structure that the rotor carries end is column construction；Motor is set in the inner chamber of the column construction, the motor with
The rotor connection.
2. it is used for the horn structure for combining gyroplane according to claim 1, it is characterised in that
When the quantity of the rotor is 1, the upper bottom surface of the column construction sets rotor anchor tip, and the rotor is fixed on
On the rotor anchor tip；
When the quantity of the rotor is 2, rotor anchor tip, Mei Gesuo are respectively provided with the upper and lower bottom surface of the column construction
State and a rotor is fixed on rotor anchor tip.
3. it is used for the horn structure for combining gyroplane according to claim 1, it is characterised in that the quantity of the rotor is 1
When individual, the column construction is divided into motor waterproof cover, motor cabinet and lower bottom cover from top to bottom；The upper motor waterproof cover
The motor is set between the motor cabinet, and the motor is fixed on the motor cabinet；The motor cabinet and the bottom
Electron speed regulator is set between lid.
4. it is used for the horn structure for combining gyroplane according to claim 1, it is characterised in that the quantity of the rotor is 2
When individual, the column construction is divided into motor waterproof cover, motor cabinet and lower motor waterproof cover from top to bottom；The upper motor
The motor is set between waterproof cover and the motor cabinet, and the motor is fixed on the motor cabinet；The motor cabinet and institute
State and electron speed regulator is set between lower motor waterproof cover.
5. it is used for the horn structure for combining gyroplane according to claim 1, it is characterised in that the outer wall of the column construction
Upper setting indicator lamp, the indicator lamp and the motor connection.
6. it is used for the horn structure for combining gyroplane according to claim 1, it is characterised in that the horn structure also includes
Undercarriage, by horizontal folding part, the undercarriage is detachably connected with the horn connector.
7. it is used for the horn structure for combining gyroplane according to claim 6, it is characterised in that the undercarriage is included sequentially
Undercarriage leg, undercarriage base and the undercarriage rubber base of setting；
The fixed connector of the horizontal folding part is fixedly connected with the undercarriage leg and the horn connector respectively；Institute
State the flexible connection head and the horn connector pin connection of horizontal folding part.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710354684.9A CN107097943A (en) | 2017-05-19 | 2017-05-19 | A kind of horn structure for being used to combine gyroplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710354684.9A CN107097943A (en) | 2017-05-19 | 2017-05-19 | A kind of horn structure for being used to combine gyroplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107097943A true CN107097943A (en) | 2017-08-29 |
Family
ID=59670371
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710354684.9A Pending CN107097943A (en) | 2017-05-19 | 2017-05-19 | A kind of horn structure for being used to combine gyroplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107097943A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107444618A (en) * | 2017-09-20 | 2017-12-08 | 王月娟 | A kind of unmanned plane wing for being easy to fold |
| CN107914877A (en) * | 2017-12-20 | 2018-04-17 | 聊城揽悦创新科技有限公司 | Three axis connecting rod unmanned planes |
| CN108001682A (en) * | 2018-01-03 | 2018-05-08 | 中煤航测遥感集团有限公司 | A kind of detachable unmanned plane |
| CN108715226A (en) * | 2018-08-07 | 2018-10-30 | 濉溪淮匠机械设备有限责任公司 | A kind of more rotor plant protection drones |
| CN108750071A (en) * | 2018-07-17 | 2018-11-06 | 深圳市龙云创新航空科技有限公司 | A kind of more rotor horns and one folding structure of undercarriage |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204231059U (en) * | 2014-12-04 | 2015-03-25 | 北方天途航空技术发展（北京）有限公司 | Motor electricity adjusts integrated support |
| CN204916180U (en) * | 2015-08-12 | 2015-12-30 | 南京钟山苑航空技术有限公司 | Rotor type unmanned vehicles horn folding mechanism |
| CN105460210A (en) * | 2015-12-04 | 2016-04-06 | 上海浦江桥隧大桥管理有限公司 | Portable six-rotor-wing aircraft used for bridge detection |
| US20160280369A1 (en) * | 2013-11-01 | 2016-09-29 | The University Of Queensland | Rotorcraft |
| CN106005443A (en) * | 2016-07-29 | 2016-10-12 | 安翔泰岳（镇江）航空科技有限公司 | Unmanned aerial vehicle |
| CN106379522A (en) * | 2016-10-26 | 2017-02-08 | 辽宁电力建设监理有限公司 | Long-endurance aircraft |
| CN205931257U (en) * | 2016-08-02 | 2017-02-08 | 上海拓攻机器人有限公司 | A motor cabinet for having more rotor unmanned vehicles |
| CN106411090A (en) * | 2016-06-28 | 2017-02-15 | 哈瓦国际航空技术（深圳）有限公司 | Integrated brushless motor for unmanned aerial vehicle |
| CN206782066U (en) * | 2017-05-19 | 2017-12-22 | 北京帝测科技股份有限公司 | A kind of horn structure for being used to combine gyroplane |
-
2017
- 2017-05-19 CN CN201710354684.9A patent/CN107097943A/en active Pending
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20160280369A1 (en) * | 2013-11-01 | 2016-09-29 | The University Of Queensland | Rotorcraft |
| CN204231059U (en) * | 2014-12-04 | 2015-03-25 | 北方天途航空技术发展（北京）有限公司 | Motor electricity adjusts integrated support |
| CN204916180U (en) * | 2015-08-12 | 2015-12-30 | 南京钟山苑航空技术有限公司 | Rotor type unmanned vehicles horn folding mechanism |
| CN105460210A (en) * | 2015-12-04 | 2016-04-06 | 上海浦江桥隧大桥管理有限公司 | Portable six-rotor-wing aircraft used for bridge detection |
| CN106411090A (en) * | 2016-06-28 | 2017-02-15 | 哈瓦国际航空技术（深圳）有限公司 | Integrated brushless motor for unmanned aerial vehicle |
| CN106005443A (en) * | 2016-07-29 | 2016-10-12 | 安翔泰岳（镇江）航空科技有限公司 | Unmanned aerial vehicle |
| CN205931257U (en) * | 2016-08-02 | 2017-02-08 | 上海拓攻机器人有限公司 | A motor cabinet for having more rotor unmanned vehicles |
| CN106379522A (en) * | 2016-10-26 | 2017-02-08 | 辽宁电力建设监理有限公司 | Long-endurance aircraft |
| CN206782066U (en) * | 2017-05-19 | 2017-12-22 | 北京帝测科技股份有限公司 | A kind of horn structure for being used to combine gyroplane |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107444618A (en) * | 2017-09-20 | 2017-12-08 | 王月娟 | A kind of unmanned plane wing for being easy to fold |
| CN107914877A (en) * | 2017-12-20 | 2018-04-17 | 聊城揽悦创新科技有限公司 | Three axis connecting rod unmanned planes |
| CN108001682A (en) * | 2018-01-03 | 2018-05-08 | 中煤航测遥感集团有限公司 | A kind of detachable unmanned plane |
| CN108750071A (en) * | 2018-07-17 | 2018-11-06 | 深圳市龙云创新航空科技有限公司 | A kind of more rotor horns and one folding structure of undercarriage |
| CN108715226A (en) * | 2018-08-07 | 2018-10-30 | 濉溪淮匠机械设备有限责任公司 | A kind of more rotor plant protection drones |
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|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170829 |