CN105799924A - Simple aircraft with water tank - Google Patents
Simple aircraft with water tank Download PDFInfo
- Publication number
- CN105799924A CN105799924A CN201610301512.0A CN201610301512A CN105799924A CN 105799924 A CN105799924 A CN 105799924A CN 201610301512 A CN201610301512 A CN 201610301512A CN 105799924 A CN105799924 A CN 105799924A
- Authority
- CN
- China
- Prior art keywords
- water tank
- annular water
- aircraft
- propeller
- side wall
- 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
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 title claims abstract description 70
- 230000005540 biological transmission Effects 0.000 claims abstract description 3
- 239000007921 spray Substances 0.000 claims description 9
- 239000000463 material Substances 0.000 abstract description 3
- 239000000575 pesticide Substances 0.000 abstract description 3
- 238000005507 spraying Methods 0.000 abstract 3
- 230000000694 effects Effects 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000002917 insecticide Substances 0.000 description 1
- 238000003973 irrigation Methods 0.000 description 1
- 230000002262 irrigation Effects 0.000 description 1
- 238000004519 manufacturing process Methods 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
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/16—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
- B64D1/18—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/20—Rotors; Rotor supports
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Life Sciences & Earth Sciences (AREA)
- Pest Control & Pesticides (AREA)
- Catching Or Destruction (AREA)
Abstract
The invention discloses a simple aircraft with a water tank, belongs to the field of aircrafts, and aims at providing the simple aircraft integrating the water tank and a flight body. The simple aircraft comprises the annular water tank and a spraying system, wherein the annular water tank comprises a top plate, a bottom plate, an inner side wall and an outer side wall; the top plate, the bottom plate, the inner side wall and the outer side wall define a first cavity body; a plurality of connecting rods are evenly distributed along the circumferential direction of the annular water tank; one end of each connecting rod is fixed to the outer side wall of the annular water tank and the other end of each connecting rod extends outwards along the radial direction of the annular water tank; a propeller is arranged on each connecting rod and is located on the same circumference which is concentric with the annular water tank; each propeller comprises a motor which is in transmission connection with the propeller; each motor is arranged on the inner side wall of the annular water tank; and the spraying system is located in the annular water tank and is communicated with the first cavity body of the annular water tank. The simple aircraft with the water tank is used for agriculturally spraying pesticides and water; the structure of the aircraft is simplified; material is saved; and the weight of the aircraft is reduced.
Description
Technical field
The invention belongs to aircraft field, particularly carry the simple and easy aircraft of water tank.
Background technology
Along with the progress of science and technology, spray insecticide on a large scale in farmland and the work such as spray irrigation is progressively done by unmanned vehicle.Existing agricultural aircraft, the flying body of the water tank and aircraft that contain pesticide is usually independent, and flying body plays the effect of delivery water tank, and water tank functions only as the effect containing pesticide.Water tank is relatively independent with the flying body of aircraft, first has to the annexation considering water tank with flying body, adds the complexity of aircraft, moreover, increase the deadweight of aircraft.
Summary of the invention
The technical problem to be solved is to provide the simple and easy aircraft carrying water tank that a kind of water tank is integrated with flying body.
The technical solution used in the present invention is: carry the simple and easy aircraft of water tank, including annular water tank, described annular water tank includes top board, base plate, medial wall and lateral wall, described top board, base plate, medial wall and lateral wall surround the first cavity, the annularly uniform many connecting rods of water tank circumference, the lateral wall of annular water tank is fixed in described connecting rod one end, extending radially outwardly of the other end annularly water tank；Being provided with propeller on every connecting rod, propeller is positioned at on the same circumference of the concyclic heart of annular water tank, and including the motor being connected with propeller drive, described motor is installed on the medial wall of annular water tank；Also including spray system, described spray system is installed on annular water tank and is connected with the first cavity of annular water tank.
Further, also including top closure lid and bottom portion hush panel, described top closure lid is connected with roof movement, and described bottom seal plate is fixing with base plate to be connected, and described top closure lid, bottom seal plate and medial wall surround the second cavity.
Further, described bottom seal plate and base plate are integrated part.
The invention has the beneficial effects as follows: this carries the simple and easy aircraft of water tank, and connecting rod one end is installed on the lateral wall of annular water tank, extending radially outwardly of the other end annularly water tank；Every connecting rod is provided with propeller.Annular water tank not only has water storage function, also doubles as the body of flying body.Body and water tank are integrally combined, simplify the structure of aircraft, save material, alleviate the weight of aircraft.
Accompanying drawing explanation
Fig. 1 is schematic diagram of the present invention.
Fig. 2 is the A-A sectional view of Fig. 1.
In figure, annular water tank 1, top board 11, base plate 12, medial wall 13, lateral wall the 14, first cavity 2, connecting rod 3, propeller 4, motor 5, spray system 6, top closure lid 7, bottom seal plate the 8, second cavity 9.
Detailed description of the invention
Below in conjunction with drawings and Examples, the present invention is described further.
Carry the simple and easy aircraft of water tank, as depicted in figs. 1 and 2, including annular water tank 1, described annular water tank 1 includes top board 11, base plate 12, medial wall 13 and lateral wall 14, described top board 11, base plate 12, medial wall 13 and lateral wall 14 surround the first cavity 2, the annularly uniform many connecting rods 3 of water tank 1 circumference, the lateral wall 14 of annular water tank 1 is fixed in described connecting rod 3 one end, extending radially outwardly of the other end annularly water tank 1；Being provided with propeller 4 on every connecting rod 3, propeller 4 is positioned at on the same circumference of the concyclic heart of annular water tank 1, and including the motor 5 being in transmission connection with propeller 4, described motor 5 is installed on the medial wall 13 of annular water tank 1；Also including spray system 6, described spray system is installed on annular water tank 1 and is connected with the first cavity 2 of annular water tank 1.
This carries the simple and easy aircraft of water tank, and connecting rod 3 one end is installed on the lateral wall 14 of annular water tank 1, extending radially outwardly of the other end annularly water tank 1；Every connecting rod 3 is provided with propeller 4.Annular water tank 1 not only has water storage function, also doubles as the body of flying body.Body and water tank are integrally combined, simplify the structure of aircraft, save material, alleviate the weight of aircraft.
Certainly, the region that annular water tank 1 medial wall 13 surrounds can both ends open, but, owing to motor 5 is installed on annular water tank 1 medial wall 13, lost efficacy in order to avoid motor 5 and medial wall 13 are installed and dropped, injured crowd by a crashing object.Therefore, as preferably, also including top closure lid 7 and bottom seal plate 8, described top closure lid 7 is flexibly connected with top board 11, described bottom seal plate 8 is fixing with base plate 12 to be connected, and described top closure lid 7, bottom seal plate 8 and medial wall 13 surround the second cavity 9.The second cavity 9 closed plays the effect of protection motor 5.Top closure lid 7 is flexibly connected easy access motor 5 with top board 11.
In order to facilitate processing and manufacturing, as preferably, described bottom seal plate 8 is integrated part with base plate 12.Bottom seal plate 8 and base plate 12 are integrated part, have saved operation bottom seal plate 8 and base plate 12 spliced.
Claims (3)
1. carry the simple and easy aircraft of water tank, it is characterized in that: include annular water tank (1), described annular water tank (1) includes top board (11), base plate (12), medial wall (13) and lateral wall (14), described top board (11), base plate (12), medial wall (13) and lateral wall (14) surround the first cavity (2), the annularly uniform many connecting rods (3) of water tank (1) circumference, the lateral wall (14) of annular water tank (1) is fixed in described connecting rod (3) one end, extending radially outwardly of the other end annularly water tank (1)；Every connecting rod (3) is provided with propeller (4), propeller (4) be positioned at on the same circumference of annular water tank (1) the concyclic heart, including the motor (5) being in transmission connection with propeller (4), described motor (5) is installed on the medial wall (13) of annular water tank (1)；Also including spray system (6), described spray system is installed on annular water tank (1) and is connected with first cavity (2) of annular water tank (1).
2. carry the simple and easy aircraft of water tank as claimed in claim 1, it is characterized in that: also include top closure lid (7) and bottom seal plate (8), described top closure lid (7) is flexibly connected with top board (11), described bottom seal plate (8) and base plate (12) are fixing to be connected, and described top closure lid (7), bottom seal plate (8) and medial wall (13) surround the second cavity (9).
3. carry the simple and easy aircraft of water tank as claimed in claim 2, it is characterised in that: described bottom seal plate (8) and base plate (12) are integrated part.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610301512.0A CN105799924A (en) | 2016-05-09 | 2016-05-09 | Simple aircraft with water tank |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610301512.0A CN105799924A (en) | 2016-05-09 | 2016-05-09 | Simple aircraft with water tank |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105799924A true CN105799924A (en) | 2016-07-27 |
Family
ID=56455559
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610301512.0A Pending CN105799924A (en) | 2016-05-09 | 2016-05-09 | Simple aircraft with water tank |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105799924A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018123186A1 (en) * | 2016-12-28 | 2018-07-05 | ヤマハ発動機株式会社 | Multicopter |
| WO2018123187A1 (en) * | 2016-12-28 | 2018-07-05 | ヤマハ発動機株式会社 | Multicopter |
| CN108782528A (en) * | 2018-06-26 | 2018-11-13 | 深圳市安思科电子科技有限公司 | A kind of plant protection drone of efficient adjustable concentration |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104354864A (en) * | 2014-10-29 | 2015-02-18 | 浙江大学 | Rotary wing type unmanned aerial vehicle for spraying pesticides |
| CN104908937A (en) * | 2015-06-30 | 2015-09-16 | 孙建香 | Agricultural sprayer |
| CN104943863A (en) * | 2015-06-26 | 2015-09-30 | 常州展华机器人有限公司 | Pesticide spraying unmanned aerial vehicle |
| WO2015161352A1 (en) * | 2014-04-22 | 2015-10-29 | Da Costa Goerl Eduardo | Unmanned aerial vehicle (uav) used for agricultural activity and the application of pesticides and fertilizers |
| CN205168879U (en) * | 2014-12-03 | 2016-04-20 | 珠海银通农业科技有限公司 | Independently drive plant protection aircraft based on GPS |
-
2016
- 2016-05-09 CN CN201610301512.0A patent/CN105799924A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2015161352A1 (en) * | 2014-04-22 | 2015-10-29 | Da Costa Goerl Eduardo | Unmanned aerial vehicle (uav) used for agricultural activity and the application of pesticides and fertilizers |
| CN104354864A (en) * | 2014-10-29 | 2015-02-18 | 浙江大学 | Rotary wing type unmanned aerial vehicle for spraying pesticides |
| CN205168879U (en) * | 2014-12-03 | 2016-04-20 | 珠海银通农业科技有限公司 | Independently drive plant protection aircraft based on GPS |
| CN104943863A (en) * | 2015-06-26 | 2015-09-30 | 常州展华机器人有限公司 | Pesticide spraying unmanned aerial vehicle |
| CN104908937A (en) * | 2015-06-30 | 2015-09-16 | 孙建香 | Agricultural sprayer |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2018123186A1 (en) * | 2016-12-28 | 2018-07-05 | ヤマハ発動機株式会社 | Multicopter |
| WO2018123187A1 (en) * | 2016-12-28 | 2018-07-05 | ヤマハ発動機株式会社 | Multicopter |
| JP2018108774A (en) * | 2016-12-28 | 2018-07-12 | ヤマハ発動機株式会社 | Multicopter |
| JP2018108775A (en) * | 2016-12-28 | 2018-07-12 | ヤマハ発動機株式会社 | Multicopter |
| CN110114270A (en) * | 2016-12-28 | 2019-08-09 | 雅马哈发动机株式会社 | More gyroplanes |
| CN110139799A (en) * | 2016-12-28 | 2019-08-16 | 雅马哈发动机株式会社 | More gyroplanes |
| CN108782528A (en) * | 2018-06-26 | 2018-11-13 | 深圳市安思科电子科技有限公司 | A kind of plant protection drone of efficient adjustable concentration |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20160727 |