CN107264789A - A kind of Combined unmanned machine - Google Patents
A kind of Combined unmanned machine Download PDFInfo
- Publication number
- CN107264789A CN107264789A CN201710561382.9A CN201710561382A CN107264789A CN 107264789 A CN107264789 A CN 107264789A CN 201710561382 A CN201710561382 A CN 201710561382A CN 107264789 A CN107264789 A CN 107264789A
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- CN
- China
- Prior art keywords
- connecting rod
- main body
- slide rail
- fixed mount
- fixed
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- 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.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
-
- 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
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Guiding Agricultural Machines (AREA)
Abstract
The invention discloses a kind of Combined unmanned machine, its structure includes main body, retainer ring, connecting rod, support feet, pick-up lens, fixed mount, adjust slide rail, retainer ring is nested on connecting rod inner opposite end outer surface of cupular part, retainer ring links together main body more than connecting rod, connecting rod insertion is connected to body interior, insertion body interior at the top of support feet, support frame pin is by main body below connecting rod, pick-up lens it is fixed by snap with fixed mount on, pick-up lens is interference fit with fixed mount, fixed mount is fixed on main body lower bottom part by nut, adjust built in slide rail and connecting rod inside middle, regulation slide rail is mutually closely connected by nut with connecting rod, connecting rod is provided with limit shaft, rotary shaft, stator, propeller blade, limit shaft is fixed on propeller shaft upper surface, the present invention realizes the unmanned plane in flight operation, can be by the telescopic adjustment of connecting rod, it is more prone to use flight environment of vehicle, strengthen practicality.
Description
Technical field
The present invention is a kind of Combined unmanned machine, belongs to unmanned plane field.
Background technology
Domestic and international unmanned plane correlation technique is developed rapidly, and UAS species is various, the wide distinct characteristics of purposes, causes it
In size, quality, voyage, endurance, flying height, flying speed, task dispatching many-side has larger difference.Due to unmanned plane
Diversity, different sorting techniques are had for different considering：Classify by flying platform configuration, unmanned plane can be divided into fixed-wing
Unmanned plane, rotor wing unmanned aerial vehicle, unmanned airship, umbrella wing unmanned plane, flapping wing unmanned plane etc., classification by use, unmanned plane can be divided into army
With unmanned plane and civilian unmanned plane.Military unmanned air vehicle can be divided into reconnaissance UAV, bait unmanned plane, UAV for electronic countermeasure, logical
Letter relaying unmanned plane, UCAV and target drone etc.；Civilian unmanned plane can be divided into inspection/monitoring unmanned plane, agricultural unmanned plane,
Meteorological unmanned plane, exploration unmanned plane and mapping unmanned plane etc..
Prior art published application number is a kind of CN201620866399.6 unmanned plane, and it includes unmanned plane main body, institute
State and the second screw rod is installed with the inside of connecting rod, second screw rod is connected with the second screw screw thread, second screw rod
Outside be provided with the first screw rod, the outer wall of second screw rod is provided with tumbler, and the top of the tumbler is provided with turning
Moving axis, the outer wall of the rotary shaft is provided with propeller, and the inner chamber of the tumbler is provided with the first screw, first screw
It is connected with the first screw flight.The Combined unmanned machine, is connected by the second screw rod with the second screw screw thread, can be connecting rod
Disassemble, be connected by the first screw rod with the first screw screw thread from unmanned plane main body, can be connecting rod from tumbler
On disassemble, be connected by the 3rd screw rod with the 3rd screw screw thread, secondary unmanned plane main body can be torn open from unmanned plane main body
Unload down, easily unmanned plane main body can be dismounted, but the unmanned plane is flying in use, the bar of connection propeller
Length is fixed, it is impossible to be adjusted according to environment, and especially when entering small space, flight operation is restricted.
The content of the invention
In view of the deficienciess of the prior art, it is an object of the present invention to provide a kind of Combined unmanned machine, to solve can adjust
The problem of connecting pole length.
To achieve these goals, the object of the invention provides a kind of Combined unmanned machine, and its structure includes main body, consolidated
Determine ring, connecting rod, support feet, pick-up lens, fixed mount, regulation slide rail, the retainer ring is nested in connecting rod inner opposite end top
On portion outer surface, the retainer ring links together main body more than connecting rod, and the connecting rod insertion is connected to body interior, institute
Insertion body interior at the top of support feet is stated, support frame as described above pin is by main body below connecting rod, and the pick-up lens passes through
In buckle fixation and fixed mount, the pick-up lens is interference fit with fixed mount, and the fixed mount is fixed on master by nut
Body lower bottom part, the regulation slide rail is built-in with connecting rod inside middle, and the regulation slide rail is mutually tight by nut and connecting rod
Close connection, the connecting rod is provided with limit shaft, rotary shaft, stator, propeller blade, and the limit shaft is fixed on propeller shaft
Surface, the rotary shaft is closely snapped together by axle with stator, and the stator is fixed on outside connecting rod by nut
Side roof part upper surface, the propeller blade is by rotary shaft above connecting rod, and the support feet is provided with support bar, fixation
Bar, the fix bar is through in the middle of support feet, and the fix bar insertion is connected to inside support bar, the fix bar and support
Bar is connected for interference fit, and the regulation slide rail is made up of connecting groove, fixing nut, sliding block, slide rail body, and the connection is recessed
Groove is in integrated formed structure with slide rail body, and the connecting groove is in the middle of slide rail body and runs through, and the fixing nut is led to
Cross connecting hole insertion to be connected on sliding block, the fixing nut is interference fit with sliding block, and the sliding block is on slide rail body
Side and the connection that cooperates.
Further, the support feet is located on the outside of fixed mount by main body.
Further, the connecting rod is provided with 4, and the connecting rod is uniformly distributed in main body outer surface.
Further, the main body is provided with 1, and the main body is the circular configuration between a diameter of 5cm-12cm.
Further, the support feet is provided between 2, the support feet and is parallel to each other.
Further, the fixing nut is provided with 3, and the fixing nut is successively above equidistant arrangement and sliding block.
Further, the slide rail body is one kind in aluminum alloy materials or stainless steel material.
Beneficial effects of the present invention：Regulation slide rail is made up of connecting groove, fixing nut, sliding block, slide rail body, is connected recessed
Groove is in integrated formed structure with slide rail body, and connecting groove is in the middle of slide rail body and runs through, and fixing nut passes through connecting hole
Insertion is connected on sliding block, and fixing nut is interference fit with sliding block, and sliding block is located above slide rail body and the connection that cooperates,
The unmanned plane is realized in flight operation, can be more prone to use flight environment of vehicle by the telescopic adjustment of connecting rod, strengthen
Practicality.
Brief description of the drawings
By reading the detailed description made with reference to the following drawings to non-limiting example, further feature of the invention,
Objects and advantages will become more apparent upon：
Fig. 1 is a kind of Combined unmanned machine structural representation of the invention.
Fig. 2 is the structural representation of support frame of the present invention.
Fig. 3 adjusts the structural representation of slide rail for the present invention.
In figure：Main body -1, retainer ring -2, connecting rod -3, support feet -4, pick-up lens -5, fixed mount -6, regulation slide rail -
7th, limit shaft -30, rotary shaft -31, stator -32, propeller blade -33, support bar -40, fix bar -41, connecting groove -70,
Fixing nut -71, sliding block -72, slide rail body -73.
Embodiment
To be easy to understand the technical means, the inventive features, the objects and the advantages of the present invention, with reference to
Embodiment, is expanded on further the present invention.
Fig. 1-Fig. 3 is referred to, the present invention provides a kind of scheme：Its structure includes main body 1, retainer ring 2, connecting rod 3, branch
Spike 4, pick-up lens 5, fixed mount 6, regulation slide rail 7, the retainer ring 2 are nested in the inner opposite end outer surface of cupular part of connecting rod 3
On, the retainer ring 3 links together the main body 1 of connecting rod more than 3, and the insertion of connecting rod 3 is connected to inside main body 1, described
Inside the top of support feet 4 insertion main body 1, support frame as described above pin 4 is by main body 1 located at the lower section of connecting rod 3, the pick-up lens 5
On fixed by snap and fixed mount 6, the pick-up lens 5 is interference fit with fixed mount 6, and the fixed mount 6 passes through nut
It is fixed on the lower bottom part of main body 1, the regulation slide rail 7 is built-in with the inside middle of connecting rod 3, the regulation slide rail 7 passes through nut
Mutually closely it is connected with connecting rod 3, the connecting rod 3 is provided with limit shaft 30, rotary shaft 31, stator 32, propeller blade 33, described
Limit shaft 30 is fixed on the upper surface of propeller shaft 33, and the rotary shaft 31 is closely snapped together by axle with stator 32, institute
State stator 32 and the outside top upper surface of connecting rod 3 is fixed on by nut, the propeller blade 33 is located at by rotary shaft 31
The top of connecting rod 33, the support feet 4 is provided with support bar 40, fix bar 41, the fix bar 41 through in the middle of support feet 4,
The insertion of fix bar 41 is connected to inside support bar 40, and the fix bar 41 is connected with support bar 40 for interference fit, described
Regulation slide rail 7 is made up of connecting groove 70, fixing nut 71, sliding block 72, slide rail body 73, the connecting groove 70 and slide rail master
Body 73 is in integrated formed structure, and the connecting groove 70 is in the middle of slide rail body 73 and runs through, and the fixing nut 71 passes through
Connecting hole insertion is connected on sliding block 72, and the fixing nut 71 is interference fit with sliding block 72, and the sliding block 72 is located at slide rail
The top of main body 73 and the connection that cooperates, the support feet 4 is by main body 1 located at the outside of fixed mount 6, and the connecting rod 3 is provided with 4
Root, the connecting rod 3 is uniformly distributed in the outer surface of main body 1, and the main body 1 is provided with 1, and the main body 1 is a diameter of 5cm-
Circular configuration between 12cm, the support feet 4 is provided between 2, the support feet 4 and is parallel to each other, the fixing nut 71
Provided with 3, the fixing nut 71 top of equidistant arrangement and sliding block 72 successively, the slide rail body 73 is aluminum alloy materials or not
One kind in rust Steel material.
Regulation slide rail described in this patent, i.e. slide rail, are its bearing knots inside the slide rail that naked eyes can not be seen
Structure, this part is directly connected to its weight capacity.Existing ball guide, roller bearing slide rail, also there is silicon wheel slide rail in the market.
The former, so as to ensure the cleaning of slide rail, will not be entered by the rolling of steel ball, the automatic dust and foul excluded on slide rail because of foul
Enter internal and influence its sliding function.Steel ball can be such that active force is spread to surrounding simultaneously, it is ensured that both horizontally and vertically
Stability.The chip that silicon wheel slide rail is produced in long-term use, friction process is in snowflake shape, and can also be by it by rolling
Band gets up, and does not interfere with equally and slides freely.
When in use, first check for whether each several part is stably connected with, confirm after Plant in good condition, equipment is placed on
Suitable operating position, by adjusting slide rail to reach the purpose of adjustable connecting rod length, in the operation of practical unmanned plane during flying
When, it can be more prone to use flight environment of vehicle, strengthen practicality by the telescopic adjustment of connecting rod.
The main body -1 of the present invention, retainer ring -2, connecting rod -3, support feet -4, pick-up lens -5, fixed mount -6, regulation are slided
Rail -7, limit shaft -30, rotary shaft -31, stator -32, propeller blade -33, support bar -40, fix bar -41, connecting groove -
70th, fixing nut -71, sliding block -72, slide rail body -73, part are the portion that universal standard part or those skilled in the art know
Part, its structure and principle all can be learnt by technical manual or be known by normal experiment method, this hair for this technology personnel
The problem of bright solution is the function that unmanned plane can not possess adjustable connecting rod length, it is impossible to be adjusted according to environment, especially
When entering small space, flight operation is restricted, being mutually combined by above-mentioned part of the invention, realizes the unmanned plane
In flight operation, it can be more prone to use flight environment of vehicle, strengthen practicality, specifically such as by the telescopic adjustment of connecting rod
It is lower described：
The regulation slide rail 7 is made up of connecting groove 70, fixing nut 71, sliding block 72, slide rail body 73, and the connection is recessed
Groove 70 is in integrated formed structure with slide rail body 73, and the connecting groove 70 is in the middle of slide rail body 73 and runs through, described solid
Determine nut 71 to be connected on sliding block 72 by connecting hole insertion, the fixing nut 71 is interference fit, the cunning with sliding block 72
Block 72 is located at the top of slide rail body 73 and the connection that cooperates.
In embodiments of the invention 1, the slide rail body 73 is aluminum alloy materials；
In embodiments of the invention 2, the slide rail body 73 is stainless steel material；
| Embodiment 1 | Embodiment 2 | |
| Material hardness | Typically | Greatly |
| Service life | It is long | It is longer |
| Wear resistance | Typically | It is good |
In summary, when the slide rail body of the present invention is stainless steel material, material hardness of the invention is big, service life
Long, more wear-resistant, using effect reaches most preferably.
The general principle and principal character and advantages of the present invention of the present invention has been shown and described above, for this area skill
For art personnel, it is clear that the invention is not restricted to the details of above-mentioned one exemplary embodiment, and without departing substantially from the present invention spirit or
In the case of essential characteristic, the present invention can be realized in other specific forms.Therefore, all should be by no matter from the point of view of which point
Embodiment regards exemplary as, and be it is nonrestrictive, the scope of the present invention by appended claims rather than on state
It is bright to limit, it is intended that all changes fallen in the implication and scope of the equivalency of claim are included in the present invention
It is interior.Any reference in claim should not be considered as to the claim involved by limitation.
Moreover, it will be appreciated that although the present specification is described in terms of embodiments, not each embodiment is only wrapped
Containing an independent technical scheme, this narrating mode of specification is only that for clarity, those skilled in the art should
Using specification as an entirety, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
It may be appreciated other embodiment.
Claims (5)
1. a kind of Combined unmanned machine, its structure includes main body (1), retainer ring (2), connecting rod (3), support feet (4), camera lens
Head (5), fixed mount (6), regulation slide rail (7), the retainer ring (2) are nested on connecting rod (3) inner opposite end outer surface of cupular part,
The retainer ring (3) links together main body (1) more than connecting rod (3), and connecting rod (3) insertion is connected in main body (1)
Insertion main body (1) is internal at the top of portion, the support feet (4), and support frame as described above pin (4) is located under connecting rod (3) by main body (1)
Side, the pick-up lens (5) it is fixed by snap with fixed mount (6) on, the pick-up lens (5) is interference with fixed mount (6)
Coordinate, the fixed mount (6) is fixed on main body (1) lower bottom part by nut, the regulation slide rail (7) is built-in and connecting rod
(3) inside middle, the regulation slide rail (7) is mutually closely connected by nut with connecting rod (3), it is characterised in that：
The connecting rod (3) is provided with limit shaft (30), rotary shaft (31), stator (32), propeller blade (33), the limit shaft
(30) propeller shaft (33) upper surface is fixed on, the rotary shaft (31) is closely snapped together by axle with stator (32),
The stator (32) is fixed on connecting rod (3) outside top upper surface by nut, and the propeller blade (33) passes through rotation
Axle (31) is above connecting rod (33)；
The support feet (4) is provided with support bar (40), fix bar (41), and the fix bar (41) is middle through support feet (4),
The embedded support bar (40) that is connected to of the fix bar (41) is internal, and the fix bar (41) connects with support bar (40) for interference fit
Connect；
The regulation slide rail (7) is made up of connecting groove (70), fixing nut (71), sliding block (72), slide rail body (73), described
Connecting groove (70) is in integrated formed structure with slide rail body (73), and the connecting groove (70) is in the middle of slide rail body (73)
And run through, the fixing nut (71) is connected on sliding block (72) by connecting hole insertion, the fixing nut (71) and sliding block
(72) it is interference fit, the sliding block (72) is located at slide rail body (73) top and the connection that cooperates.
2. a kind of Combined unmanned machine according to claim 1, it is characterised in that：The support feet (4) passes through main body (1)
On the outside of fixed mount (6).
3. a kind of Combined unmanned machine according to claim 1, it is characterised in that：The connecting rod (3) is provided with 4, institute
State connecting rod (3) and be uniformly distributed in main body (1) outer surface.
4. a kind of Combined unmanned machine according to claim 1, it is characterised in that：The main body (1) is described provided with 1
Main body (1) is the circular configuration between a diameter of 5cm-12cm.
5. a kind of Combined unmanned machine according to claim 1, it is characterised in that：The support feet (4) is provided with 2, institute
State and be parallel to each other between support feet (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710561382.9A CN107264789A (en) | 2017-07-11 | 2017-07-11 | A kind of Combined unmanned machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710561382.9A CN107264789A (en) | 2017-07-11 | 2017-07-11 | A kind of Combined unmanned machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107264789A true CN107264789A (en) | 2017-10-20 |
Family
ID=60072526
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710561382.9A Pending CN107264789A (en) | 2017-07-11 | 2017-07-11 | A kind of Combined unmanned machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107264789A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019154118A1 (en) * | 2018-02-06 | 2019-08-15 | 酷黑科技（北京）有限公司 | Ducted aircraft capable of implementing aerial reconstruction in real time, and docking separation method and system |
-
2017
- 2017-07-11 CN CN201710561382.9A patent/CN107264789A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019154118A1 (en) * | 2018-02-06 | 2019-08-15 | 酷黑科技（北京）有限公司 | Ducted aircraft capable of implementing aerial reconstruction in real time, and docking separation method and system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20171020 |
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| WD01 | Invention patent application deemed withdrawn after publication |