CN108248882A - A kind of unmanned plane optical mirror slip - Google Patents
A kind of unmanned plane optical mirror slip Download PDFInfo
- Publication number
- CN108248882A CN108248882A CN201810054815.6A CN201810054815A CN108248882A CN 108248882 A CN108248882 A CN 108248882A CN 201810054815 A CN201810054815 A CN 201810054815A CN 108248882 A CN108248882 A CN 108248882A
- Authority
- CN
- China
- Prior art keywords
- lens
- unmanned plane
- optical mirror
- mirror slip
- plane optical
- 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
- 230000003287 optical effect Effects 0.000 title claims abstract description 21
- 239000000565 sealant Substances 0.000 claims abstract description 14
- 239000000428 dust Substances 0.000 claims description 6
- 238000007789 sealing Methods 0.000 claims description 2
- 239000012535 impurity Substances 0.000 abstract description 3
- 238000000034 method Methods 0.000 description 10
- 238000010586 diagram Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- FGRBYDKOBBBPOI-UHFFFAOYSA-N 10,10-dioxo-2-[4-(N-phenylanilino)phenyl]thioxanthen-9-one Chemical compound O=C1c2ccccc2S(=O)(=O)c2ccc(cc12)-c1ccc(cc1)N(c1ccccc1)c1ccccc1 FGRBYDKOBBBPOI-UHFFFAOYSA-N 0.000 description 1
- 206010044565 Tremor Diseases 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000006467 substitution reaction Methods 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
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B13/00—Optical objectives specially designed for the purposes specified below
- G02B13/001—Miniaturised objectives for electronic devices, e.g. portable telephones, webcams, PDAs, small digital cameras
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B7/00—Mountings, adjusting means, or light-tight connections, for optical elements
- G02B7/02—Mountings, adjusting means, or light-tight connections, for optical elements for lenses
- G02B7/021—Mountings, adjusting means, or light-tight connections, for optical elements for lenses for more than one lens
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Instruments For Viewing The Inside Of Hollow Bodies (AREA)
Abstract
The invention discloses a kind of unmanned plane optical mirror slips, including body, the organism bottom both sides are arranged with stent, the organism bottom center is equipped with chassis, the stent is equipped with supporting rod, the tray bottom is equipped with Rotational Cylindrical, the Rotational Cylindrical two bottom sides are arranged with baffle, rotating bar is connected between two baffles, the rotating bar is equipped with video camera, sealant is arranged in the camera lens, the first lens are equipped with by the incident direction in foreign minister successively along light in the sealant, second lens, third lens, 4th lens, diaphragm, 5th lens, 6th lens and the 7th lens.The present invention in camera lens by being arranged sealant, the entrance of impurity is avoided, by setting supporting rod, hydraulic stem, spring and universal wheel, reduces the damage caused by eyeglass when unmanned plane falls, by chassis, Rotational Cylindrical and rotating bar, the Multidirectional-moving to camera lens is realized.
Description
Technical field
The present invention relates to unmanned air vehicle technique field more particularly to a kind of unmanned plane optical mirror slips.
Background technology
Along with the promotion of unmanned air vehicle technique, the range of unmanned plane application is more and more wider, will to the quality of unmanned plane
Ask higher and higher, the common picture pick-up device that unmanned plane of taking photo by plane uses mostly uses optical mirror slip in picture pick-up device.Have nobody
Eyeglass is in the presence of being spaced in picture pick-up device in machine, and between eyeglass and extraneous air, the impurity that may result in air enter camera lens
Camera shooting is influenced, eyeglass need to be dismantled and cleared up, if misoperation in dropping process, fuselage slowly declines without vertical, may lead
The overturning of unmanned plane is caused, the eyeglass in picture pick-up device is damaged, and picture pick-up device is to carry out some side by rotating fuselage
The shooting of position, it is complicated for operation.
Invention content
The purpose of the present invention is to solve some problems of the prior art, and a kind of unmanned plane optical frames proposed
Piece.
To achieve these goals, present invention employs following technical solutions：
A kind of unmanned plane optical mirror slip, including body, the organism bottom both sides are arranged with stent, the organism bottom
Center is equipped with chassis, and both sides are arranged with connecting rod at the top of the body, and the body top center is equipped with the machine of flexible connection
Lid, the stent are equipped with the supporting rod of flexible connection, and the supporting rod bottom is equipped with hydraulic stem, and the hydraulic stem includes hydraulic pressure
Cylinder and the piston rod being movably set in hydraulic cylinder, described piston rod one end are equipped with disk, the disk bottom below hydraulic cylinder
Portion is equipped with universal wheel, and the tray bottom is equipped with the Rotational Cylindrical of rotation connection, and the Rotational Cylindrical two bottom sides are arranged with baffle,
Be connected with rotating bar between two baffles, the rotating bar is equipped with video camera, the video camera include host and
The camera lens of host front surface is located at, is arranged with sealant in the camera lens, along light by the incidence in foreign minister in the sealant
Direction is equipped with the first lens, the second lens, third lens, the 4th lens, diaphragm, the 5th lens, the 6th lens and the 7th successively
Lens, the connecting rod are equipped with rotor, and the connecting rod is equipped with limited cap above rotor.
Preferably, the outer movable sleeve of the camera lens is equipped with dust cover.
Preferably, first lens are equipped with outer lens on the outside of sealant, and the outer lens are closely pasted with the first lens
It closes.
Preferably, the limited cap is flexibly connected with connecting rod, and the limited cap is in semi-circular.
Preferably, first lens, third lens and the 7th lens are biconvex positive lens, and second lens are
Half-moon-shaped negative lens, the 4th lens and the 6th lens are double concave type positive lens.
Preferably, spring is equipped between the hydraulic cylinder and disk, the piston rod is located at spring inner.
Compared with prior art, the present invention provides a kind of unmanned plane optical mirror slip, have following
Advantageous effect：
1st, the unmanned plane optical mirror slip by setting up defences dust hood in camera lens housing, is arranged sealant, prime lens in camera lens
It is respectively positioned in sealant, avoids the entrance of impurity in air, reduce influence of the bad weather to machine；
2nd, the unmanned plane optical mirror slip, by setting supporting rod, hydraulic stem, spring and universal wheel, reduces because of unmanned plane
Falling speed is too fast, angle tilt is damaged caused by eyeglass when falling；
3rd, the unmanned plane optical mirror slip by chassis, Rotational Cylindrical and rotating bar, realizes the Multidirectional-moving to camera lens,
The rotation of fuselage need not be controlled to carry out the shooting in specified orientation.
It is same as the prior art or the prior art can be used realized that part is not directed in the device, structure of the present invention
Simply, easy to operate, camera lens sealing performance is strong, reduces influence of the harsh weather to machine, reduce unmanned plane landing when pair
The impact of eyeglass.
Description of the drawings
Fig. 1 is a kind of structure diagram of unmanned plane optical mirror slip proposed by the present invention；
Fig. 2 is the structure diagram of video camera in a kind of unmanned plane optical mirror slip proposed by the present invention；
Fig. 3 is the structure diagram of camera lens in a kind of unmanned plane optical mirror slip proposed by the present invention.
In figure：1 body, 2 stents, 3 chassis, 4 connecting rods, 5 covers, 6 supporting rods, 7 hydraulic stems, 8 hydraulic cylinders, 9 piston rods,
10 disks, 11 universal wheels, 12 Rotational Cylindricals, 13 baffles, 14 rotating bars, 15 video cameras, 16 hosts, 17 camera lenses, 18 sealants, 19
One lens, 20 second lens, 21 third lens, 22 the 4th lens, 23 diaphragms, 24 the 5th lens, 25 the 6th lens, 26 the 7th are thoroughly
Mirror, 27 rotors, 28 limited caps, 29 dust covers, 30 outer lens, 31 springs.
Specific embodiment
Below in conjunction with the attached drawing in the embodiment of the present invention, the technical solution in the embodiment of the present invention is carried out clear, complete
Site preparation describes, it is clear that described embodiment is only part of the embodiment of the present invention, instead of all the embodiments.
In the description of the present invention, it is to be understood that term " on ", " under ", "front", "rear", "left", "right", " top ",
The orientation or position relationship of the instructions such as " bottom ", " interior ", " outer " are based on orientation shown in the drawings or position relationship, merely to just
In the description present invention and simplify description rather than instruction or imply signified device or element must have specific orientation, with
Specific azimuth configuration and operation, therefore be not considered as limiting the invention.
With reference to Fig. 1-3, a kind of unmanned plane optical mirror slip, including body 1,1 two bottom sides of body are arranged with stent
2,1 bottom centre of body is equipped with chassis 3, and the 1 top both sides of body are arranged with connecting rod 4, in 1 top of body
The heart is equipped with the cover 5 of flexible connection, and the stent 2 is equipped with the supporting rod 6 of flexible connection, and 6 bottom of supporting rod is equipped with liquid
Compression bar 7, the hydraulic stem 7 include hydraulic cylinder 8 and the piston rod 9 that is movably set in hydraulic cylinder 8, described 9 one end of piston rod in
8 lower section of hydraulic cylinder is equipped with disk 10, and 10 bottom of disk is equipped with universal wheel 11, and 3 bottom of chassis is equipped with rotation connection
Rotational Cylindrical 12,12 two bottom sides of Rotational Cylindrical are arranged with baffle 13, rotation are connected between two baffles 13
Bar 14, the rotating bar 14 are equipped with video camera 15, and the video camera 15 includes host 16 and is located at the mirror of 16 front surface of host
First 17, sealant 18 is arranged in the camera lens 17, is set successively by the incident direction in foreign minister along light in the sealant 18
There are the first lens 19, the second lens 20, third lens 21, the 4th lens 22, diaphragm 23, the 5th lens 24,25 and of the 6th lens
7th lens 26, the connecting rod 4 are equipped with rotor 27, and the connecting rod 4 is equipped with limited cap 28 above rotor 27.
The 17 outer movable sleeve of camera lens is equipped with dust cover 29, and first lens 19 are equipped with outer lens on the outside of sealant
30, the outer lens 30 are fitted closely with the first lens 19, and the limited cap 28 is flexibly connected with connecting rod 4, the limited cap
28 be in semi-circular, and first lens 19,21 and the 7th lens 26 of third lens are biconvex positive lens, second lens
20 be half-moon-shaped negative lens, and the 4th lens 22 and the 6th lens 25 are double concave type positive lens, the hydraulic cylinder 8 and disk 10
Between be equipped with spring 31, the piston rod 9 is located inside spring 31.
In the present invention, by the way that dust cover 29 is unloaded, the supporting rod 6 of reinflated 1 bottom of body is placed horizontally at user
Ground, the lift-off of remotely pilotless machine, unmanned plane in the air shoot object by video camera 15, and remote-controlled Rotational Cylindrical 3 rotates
So as to be shot to unmanned plane surrounding, pass through the first lens 19, the second lens 20.Third lens 21, the 4th lens 22, diaphragm
23rd, the mutual cooperation between the 5th lens 24, the 6th lens 25 and the 7th lens 26, increases image-capturing resolution and shooting is wide
Degree, universal wheel 11 contacts first with ground when unmanned plane falls, if falling operation is improper when leading to fuselage shakiness, unmanned plane leads to
The hydraulic stem 7 crossed on universal wheel 11 and the impact for reducing gravity to eyeglass is slided, the configuration of the present invention is simple is easy to operate, safety
Stablize.
Herein, relational terms such as first and second and the like be used merely to by an entity or operation with it is another
One entity or operation distinguish, and without necessarily requiring or implying between these entities or operation, there are any this reality
Relationship or sequence.Moreover, term " comprising ", "comprising" or its any other variant are intended to the packet of nonexcludability
Contain so that process, method, article or equipment including a series of elements not only include those elements, but also including
It other elements that are not explicitly listed or further includes as elements inherent to such a process, method, article, or device.
In the absence of more restrictions, the element limited by sentence "including a ...", it is not excluded that including the element
Process, method, also there are other identical elements in article or equipment.
It although an embodiment of the present invention has been shown and described, for the ordinary skill in the art, can be with
Understanding without departing from the principles and spirit of the present invention can carry out these embodiments a variety of variations, modification, replace
And modification, the scope of the present invention is defined by the appended.
The foregoing is only a preferred embodiment of the present invention, but protection scope of the present invention be not limited thereto,
Any one skilled in the art in the technical scope disclosed by the present invention, according to the technique and scheme of the present invention and its
Inventive concept is subject to equivalent substitution or change, should be covered by the protection scope of the present invention.
Claims (6)
1. a kind of unmanned plane optical mirror slip, including body (1), which is characterized in that body (1) two bottom sides are arranged with branch
Frame (2), body (1) bottom centre are equipped with chassis (3), and both sides are arranged with connecting rod (4), institute at the top of the body (1)
The cover (5) that body (1) top center is equipped with flexible connection is stated, the stent (2) is equipped with the supporting rod (6) of flexible connection,
Supporting rod (6) bottom is equipped with hydraulic stem (7), and the hydraulic stem (7) is including hydraulic cylinder (8) and is movably set in hydraulic cylinder
(8) piston rod (9) in, described piston rod (9) one end are equipped with disk (10), disk (10) bottom below hydraulic cylinder (8)
Portion is equipped with universal wheel (11), and chassis (3) bottom is equipped with the Rotational Cylindrical (12) of rotation connection, Rotational Cylindrical (12) bottom two
Side is arranged with baffle (13), is connected with rotating bar (14) between two baffles (13), on the rotating bar (14)
Equipped with video camera (15), the video camera (15) is including host (16) and is located at the camera lens (17) of host (16) front surface, described
It is arranged with sealant (18) in camera lens (17), is equipped with by the incident direction in foreign minister along light the in the sealant (18) successively
One lens (19), the second lens (20), third lens (21), the 4th lens (22), diaphragm (23), the 5th lens (24), the 6th
Lens (25) and the 7th lens (26), the connecting rod (4) are equipped with rotor (27), and the connecting rod (4) is on rotor (27)
Side is equipped with limited cap (28).
2. a kind of unmanned plane optical mirror slip according to claim 1, which is characterized in that be slidingly connected outside the camera lens (17)
There is dust cover (29).
3. a kind of unmanned plane optical mirror slip according to claim 1, which is characterized in that first lens (19) are in sealing
Layer outside is equipped with outer lens (30), and the outer lens (30) fit closely with the first lens (19).
4. a kind of unmanned plane optical mirror slip according to claim 1, which is characterized in that the limited cap (27) and connecting rod
(4) it is flexibly connected, the limited cap (27) is in semi-circular.
5. a kind of unmanned plane optical mirror slip according to claim 1, which is characterized in that first lens (19), third
Lens (21) and the 7th lens (26) they are biconvex positive lens, and second lens (20) are half-moon-shaped negative lens, and described the
Four lens (22) and the 6th lens (25) are double concave type positive lens.
6. a kind of unmanned plane optical mirror slip according to claim 1, which is characterized in that the hydraulic cylinder (8) and disk
(10) spring (31) is equipped between, the piston rod (9) is internal positioned at spring (31).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810054815.6A CN108248882A (en) | 2018-01-19 | 2018-01-19 | A kind of unmanned plane optical mirror slip |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810054815.6A CN108248882A (en) | 2018-01-19 | 2018-01-19 | A kind of unmanned plane optical mirror slip |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108248882A true CN108248882A (en) | 2018-07-06 |
Family
ID=62741546
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810054815.6A Pending CN108248882A (en) | 2018-01-19 | 2018-01-19 | A kind of unmanned plane optical mirror slip |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108248882A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020238982A1 (en) * | 2019-05-29 | 2020-12-03 | 深圳市大疆创新科技有限公司 | Lens system, photographing apparatus, and moving body |
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| CN204674822U (en) * | 2015-05-14 | 2015-09-30 | 深圳市大疆创新科技有限公司 | Alighting gear and use the unmanned vehicle of this alighting gear |
| CN205469856U (en) * | 2016-02-29 | 2016-08-17 | 深圳市大疆创新科技有限公司 | Power supply module , Unmanned vehicles and remote control mobile device |
| KR101706110B1 (en) * | 2015-09-24 | 2017-02-15 | 안동대학교 산학협력단 | A surface inspection apparatus using a multi-coptor |
| CN206270582U (en) * | 2016-11-25 | 2017-06-20 | 襄阳市雄狮光电科技有限公司 | A kind of big field-depth vehicular lens |
| CN107079090A (en) * | 2016-04-21 | 2017-08-18 | 深圳市大疆创新科技有限公司 | Unmanned plane and camera assembly |
| CN107128481A (en) * | 2017-06-07 | 2017-09-05 | 西北工业大学 | A kind of roller hydraulic damps unmanned plane shatter-resistant undercarriage |
| CN208070039U (en) * | 2018-01-19 | 2018-11-09 | 东莞市蓝姆光学科技有限公司 | A kind of unmanned plane optical mirror slip |
-
2018
- 2018-01-19 CN CN201810054815.6A patent/CN108248882A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204674822U (en) * | 2015-05-14 | 2015-09-30 | 深圳市大疆创新科技有限公司 | Alighting gear and use the unmanned vehicle of this alighting gear |
| KR101706110B1 (en) * | 2015-09-24 | 2017-02-15 | 안동대학교 산학협력단 | A surface inspection apparatus using a multi-coptor |
| CN205469856U (en) * | 2016-02-29 | 2016-08-17 | 深圳市大疆创新科技有限公司 | Power supply module , Unmanned vehicles and remote control mobile device |
| CN107079090A (en) * | 2016-04-21 | 2017-08-18 | 深圳市大疆创新科技有限公司 | Unmanned plane and camera assembly |
| CN206270582U (en) * | 2016-11-25 | 2017-06-20 | 襄阳市雄狮光电科技有限公司 | A kind of big field-depth vehicular lens |
| CN107128481A (en) * | 2017-06-07 | 2017-09-05 | 西北工业大学 | A kind of roller hydraulic damps unmanned plane shatter-resistant undercarriage |
| CN208070039U (en) * | 2018-01-19 | 2018-11-09 | 东莞市蓝姆光学科技有限公司 | A kind of unmanned plane optical mirror slip |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2020238982A1 (en) * | 2019-05-29 | 2020-12-03 | 深圳市大疆创新科技有限公司 | Lens system, photographing apparatus, and moving body |
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| Date | Code | Title | Description |
|---|---|---|---|
| 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 | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20180706 |