CN207683784U - A kind of foldable course of new aircraft of battle - Google Patents
A kind of foldable course of new aircraft of battle Download PDFInfo
- Publication number
- CN207683784U CN207683784U CN201721928275.7U CN201721928275U CN207683784U CN 207683784 U CN207683784 U CN 207683784U CN 201721928275 U CN201721928275 U CN 201721928275U CN 207683784 U CN207683784 U CN 207683784U
- Authority
- CN
- China
- Prior art keywords
- shaft
- side wall
- aircraft
- aircraft body
- foldable
- 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.)
- Active
Links
Landscapes
- Toys (AREA)
Abstract
The utility model discloses a kind of foldable course of new aircraft of battle,Including aircraft body,There are two support arms disposed in parallel by shaft rotation connection for the side wall of the aircraft body,And two shafts are arranged in diagonal line,The side wall setting of aircraft body is parallel to positioned at the shaft of the aircraft body upper right side,Shaft positioned at aircraft body lower-left end is arranged perpendicular to the side wall of aircraft body,The shaft is hollow structure,The bottom of the shaft is rotatably connected to the first threaded rod by the first rotating member,There are two the second threaded rods being laterally arranged by the rotation connection of the second rotating member for the inner wall of the shaft,The side wall of two second threaded rods (10) is arranged with matched nut (12),The side wall of the nut (12) is equipped with kelly,The side wall of the aircraft body is equipped with and the matched card slot of kelly.The force piece of aircraft can be folded and be packed up by the utility model, easy to carry and protection.
Description
Technical field
The utility model is related to flight equipment technical field more particularly to a kind of foldable course of new aircraft of battle.
Background technology
In the prior art, unmanned plane press application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into scouting
Machine and target drone.Civilian aspect, unmanned plane+sector application, which is unmanned plane, really just have been needed；At present take photo by plane, agricultural, plant protection, from
It claps, express transportation, disaster relief, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, video display
The application in shooting, manufacture romance etc. field, has greatly expanded the purposes of unmanned plane itself, developed country is also actively extending
Sector application and development unmanned air vehicle technique, with progress of the epoch, unmanned plane is also begun to as toy by called optical imaging, such as
Unmanned plane with battle function, however the force piece of existing battle unmanned plane is all fixed setting, is held when not in use
It is easily broken, nor is convenient for carrying, for this purpose, it is proposed that a kind of fighting foldable course of new aircraft to solve above-mentioned ask
Topic.
Utility model content
Purpose of the utility model is to solve in the prior art however it is existing battle unmanned plane force piece be all
Fixed setting, it is easy to be broken when not in use, nor it is convenient for carrying problem, and a kind of battle proposed is foldable new
Type aircraft.
To achieve the goals above, the utility model uses following technical solution：
A kind of foldable course of new aircraft of battle, including aircraft body, the side wall of the aircraft body pass through shaft
There are two support arms disposed in parallel for rotation connection, and two shafts are arranged in diagonal line, are located at the aircraft body upper right side
Shaft be parallel to aircraft body side wall setting, be located at aircraft body lower-left end shaft perpendicular to aircraft sheet
The side wall of body is arranged, and two one end of the support arm far from shaft are equipped with force piece, and the side wall of the aircraft body is also set
It is hollow structure to have battle device and camera, the shaft, and the bottom of the shaft is rotatably connected to by the first rotating member
First threaded rod, there are two the second threaded rods being laterally arranged by the rotation connection of the second rotating member for the inner wall of the shaft, and
Two the second threaded rods are located at the both sides of the first threaded rod, the two described one end of second threaded rod far from the second rotating member
It is equipped with and is arranged with matched spiral shell with the matched helical gear of the first threaded rod, the side wall of two second threaded rods
Mother, the side wall of the nut is equipped with kelly, and kelly is arranged through the side wall of shaft, the side wall of the aircraft body be equipped with
The matched card slot of kelly.
Preferably, the bottom of the aircraft is additionally provided with landing holder.
Preferably, transverse slat is additionally provided in the shaft, and the side wall of transverse slat is equipped with sliding slot, the sliding slot passes through two cunnings
Block is slidably connected with nut respectively.
Preferably, it is enclosed with rubber protecting jacket on first threaded rod.
Preferably, the card slot is vertically arranged.
The utility model is rotated force piece to the side of aircraft body by rotating arm, in order to carry and protect
Shield, and support arm is fixed on horizontal position by the clamping of kelly and card slot, when preventing state of flight, support arm is rotated to folding
Overlapping state.
Description of the drawings
Fig. 1 be the utility model proposes a kind of foldable course of new aircraft of battle overlooking structure diagram；
Fig. 2 be the utility model proposes a kind of foldable course of new aircraft of battle main structure diagram；
Fig. 3 be the utility model proposes a kind of foldable course of new aircraft of battle side main structure diagram；
Fig. 4 is the main structure diagram at A in Fig. 3.
In figure：1 aircraft body, 2 shafts, 3 support arms, 4 force pieces, 5 battle devices, 6 cameras, 7 first rotating members, 8
First threaded rod, 9 second rotating members, 10 second threaded rods, 11 helical gears, 12 nuts, 13 kellies, 14 card slots, 15 transverse slats, 16 are slided
Slot, 17 sliding blocks.
Specific implementation mode
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.
Referring to Fig.1-4, a kind of foldable course of new aircraft of battle, including aircraft body 1, the bottom of aircraft body 1
It is additionally provided with landing holder, is convenient for the landing of unmanned plane, prevents aircraft body 1 when landing from colliding with ground, aircraft sheet
There are two support arm 3 disposed in parallel, transverse slat 15, and transverse slat 15 are additionally provided in shaft 2 by the rotation connection of shaft 2 for the side wall of body 1
Side wall be equipped with sliding slot 16, sliding slot 16 is slidably connected with nut 12 respectively by two sliding blocks 17, since sliding block 17 can only be
Be slidably connected in sliding slot 16, so the nut 12 being connect with sliding block 17 can only also move on the second threaded rod 10, without with
It is rotated with the second threaded rod 10, such nut 12 can be clamped or detach with card slot 14 with kelly 13, and two shafts 2
It is arranged in diagonal line, the side wall setting of aircraft body 1 is parallel to positioned at the shaft 2 of 1 upper right side of aircraft body, is located at flight
The shaft 2 at 1 lower-left end of device ontology is arranged perpendicular to the side wall of aircraft body 1, and two one end of support arm 3 far from shaft 2 are all provided with
The side wall of dynamic part 4, aircraft body 1 is additionally provided with battle device 5 and camera 6, and shaft 2 is hollow structure, the bottom of shaft 2
Portion is rotatably connected to the first threaded rod 8 by the first rotating member 7, is enclosed with rubber protecting jacket on the first threaded rod 8, prevents from rotating
When abrade hand, there are two the second threaded rods 10 being laterally arranged by the rotation connection of the second rotating member 9 for the inner wall of shaft 2, and
Two the second threaded rods 10 are located at the both sides of the first threaded rod 8, two the second threaded rods 10 far from the second rotating member 9 one
End is equipped with to be arranged with matched with 8 matched helical gear 11 of the first threaded rod, the side walls of two the second threaded rods 10
The side wall of nut 12, nut 12 is equipped with kelly 13, and kelly 13 is arranged through the side wall of shaft 2, and the side wall of aircraft body 1 is set
Have and is vertically arranged with 13 matched card slot 14 of kelly, card slot 14, just needs when only support arm 3 is in horizontal position
It is fixed, because at this moment aircraft is in state of flight, support arm 3 water can not be fixed on if card slot 14 is arranged in other positions
Prosposition is set, and aircraft just can not normal flight.
Two rotations of support arms 3 first are waited propping up by the utility model when needing to get up support arm 3 to horizontal position
After arm 3 reaches horizontal position, the first threaded rod 8 is then rotated, the first threaded rod 8 is engaged with two helical gears 11, helical gear 11
The second threaded rod 10 is driven to rotate, for the nut 12 on the second threaded rod 10 because being connect with sliding block 17, nut 12 can be
It is moved on second threaded rod 10, side wall and card slot 14 of the nut 12 with kelly 13 through shaft 2 are clamped, and such shaft 2 is just not
Be rotated further by, be fixed in the horizontal direction without rotating to support arm 3, such aircraft can normal flight, when not making
It when with aircraft, needs to fold up support arm 3, when folding, only needs negative direction to rotate the first threaded rod 8, so that the second screw thread
Nut 12 on bar 10 moves backward, and nut 12 will be detached with card slot 14 with kelly 13, can thus be folded support arm 3
To the side of aircraft body 1, in order to carry and protect force piece 4.
The preferable specific implementation mode of the above, only the utility model, but the scope of protection of the utility model is not
Be confined to this, any one skilled in the art within the technical scope disclosed by the utility model, according to this practicality
Novel technical solution and its utility model design are subject to equivalent substitution or change, should all cover the protection model in the utility model
Within enclosing.
Claims (5)
1. a kind of foldable course of new aircraft of battle, including aircraft body (1), which is characterized in that the aircraft body (1)
Side wall by shaft (2) rotation connection there are two support arm disposed in parallel (3), and two shafts (2) are in diagonal line setting, position
It is parallel to the side wall setting of aircraft body (1) in the shaft (2) of the aircraft body (1) upper right side, is located at the flight
The shaft (2) at device ontology (1) lower-left end is arranged perpendicular to the side wall of aircraft body (1), and two support arms (3) are far from shaft
(2) one end is equipped with force piece (4), and the side wall of the aircraft body (1) is additionally provided with battle device (5) and camera (6),
The shaft (2) is hollow structure, and the bottom of the shaft (2) is rotatably connected to the first threaded rod by the first rotating member (7)
(8), the inner wall of the shaft (2) is rotatablely connected by the second rotating member (9) there are two the second threaded rod (10) being laterally arranged,
And two the second threaded rods (10) are located at the both sides of the first threaded rod (8), two second threaded rods (10) are far from the
One end of two rotating members (9) is equipped with and the first threaded rod (8) matched helical gear (11), two second threaded rods (10)
Side wall be arranged with matched nut (12), the side wall of the nut (12) is equipped with kelly (13), and kelly (13) passes through
The side wall setting of shaft (2) is worn, the side wall of the aircraft body (1) is equipped with and kelly (13) matched card slot (14).
2. a kind of foldable course of new aircraft of battle according to claim 1, which is characterized in that the aircraft body
(1) bottom is additionally provided with landing holder.
3. a kind of foldable course of new aircraft of battle according to claim 1, which is characterized in that in the shaft (2) also
Equipped with transverse slat (15), and the side wall of transverse slat (15) is equipped with sliding slot (16), and the sliding slot (16) passes through two sliding blocks (17) difference
It is slidably connected with nut (12).
4. a kind of foldable course of new aircraft of battle according to claim 1, which is characterized in that first threaded rod
(8) rubber protecting jacket is enclosed on.
5. a kind of foldable course of new aircraft of battle according to claim 1, which is characterized in that the card slot (14) is along perpendicular
Histogram is to setting.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721928275.7U CN207683784U (en) | 2017-12-29 | 2017-12-29 | A kind of foldable course of new aircraft of battle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721928275.7U CN207683784U (en) | 2017-12-29 | 2017-12-29 | A kind of foldable course of new aircraft of battle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207683784U true CN207683784U (en) | 2018-08-03 |
Family
ID=62994104
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721928275.7U Active CN207683784U (en) | 2017-12-29 | 2017-12-29 | A kind of foldable course of new aircraft of battle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207683784U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2020083313A (en) * | 2018-11-30 | 2020-06-04 | エスゼット ディージェイアイ テクノロジー カンパニー リミテッドＳｚ Ｄｊｉ Ｔｅｃｈｎｏｌｏｇｙ Ｃｏ．，Ｌｔｄ | Foldable unmanned aerial vehicle |
| WO2022094944A1 (en) * | 2020-11-06 | 2022-05-12 | 深圳市大疆创新科技有限公司 | Multirotor unmanned aerial vehicle and kit |
-
2017
- 2017-12-29 CN CN201721928275.7U patent/CN207683784U/en active Active
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2020083313A (en) * | 2018-11-30 | 2020-06-04 | エスゼット ディージェイアイ テクノロジー カンパニー リミテッドＳｚ Ｄｊｉ Ｔｅｃｈｎｏｌｏｇｙ Ｃｏ．，Ｌｔｄ | Foldable unmanned aerial vehicle |
| WO2020107457A1 (en) * | 2018-11-30 | 2020-06-04 | SZ DJI Technology Co., Ltd. | Foldable unmanned aerial vehicle |
| CN111655577A (en) * | 2018-11-30 | 2020-09-11 | 深圳市大疆创新科技有限公司 | Foldable unmanned aerial vehicle |
| EP3678935A4 (en) * | 2018-11-30 | 2020-10-14 | SZ DJI Technology Co., Ltd. | Foldable unmanned aerial vehicle |
| CN111655577B (en) * | 2018-11-30 | 2024-01-26 | 深圳市大疆创新科技有限公司 | Foldable unmanned aerial vehicle |
| WO2022094944A1 (en) * | 2020-11-06 | 2022-05-12 | 深圳市大疆创新科技有限公司 | Multirotor unmanned aerial vehicle and kit |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN207683784U (en) | A kind of foldable course of new aircraft of battle | |
| CN106741876B (en) | Unmanned aerial vehicle | |
| CN107215465B (en) | A kind of unmanned plane suitable for taking photo by plane with shatter-resistant function | |
| WO2017097021A1 (en) | Wearable unmanned aerial vehicle | |
| CN105818626A (en) | Universal robot for water, land and air investigation | |
| CN205632000U (en) | Land, water and air investigation all -purpose robot | |
| CN106927042A (en) | A kind of unmanned plane of changeable form | |
| CN208085997U (en) | The unmanned plane that a kind of horn is scalable, folds | |
| CN208021722U (en) | Self-locking undercarriage is turned under one kind | |
| CN206914627U (en) | A kind of collapsible unmanned plane undercarriage | |
| CN107985574B (en) | Buoyancy assisted lifting unmanned aerial vehicle | |
| CN205872485U (en) | On -board unmanned aerial vehicle protection device that gets into danger | |
| CN209410351U (en) | A kind of unmanned plane scouting probe for landform detective | |
| CN207595281U (en) | A kind of unmanned plane full angle image aerial device | |
| CN207748034U (en) | A kind of aerial photography aircraft convenient for rising and falling | |
| CN208602716U (en) | One kind is taken photo by plane unmanned plane filming apparatus | |
| CN205440849U (en) | Folding many rotor unmanned aerial vehicle horn | |
| CN205952290U (en) | Folding portable aircraft | |
| CN207157488U (en) | A kind of unmanned plane of scalable paddle arm and foot stool | |
| CN213768973U (en) | Unmanned aerial vehicle carries on manual and automatically regulated catapult angle's multipurpose catapult | |
| CN109436350A (en) | A kind of novel unmanned plane | |
| CN113716017A (en) | Unmanned aerial vehicle with adjustable wing angle | |
| CN208021720U (en) | A kind of aircraft with support frame structure | |
| CN107600420A (en) | A kind of multi-rotor unmanned aerial vehicle control module | |
| CN109782780A (en) | A kind of winged control examination protective device of multi-rotor unmanned aerial vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |