CN209427020U - A kind of unmanned plane mission payload connection structure - Google Patents
A kind of unmanned plane mission payload connection structure Download PDFInfo
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- CN209427020U CN209427020U CN201920063009.5U CN201920063009U CN209427020U CN 209427020 U CN209427020 U CN 209427020U CN 201920063009 U CN201920063009 U CN 201920063009U CN 209427020 U CN209427020 U CN 209427020U
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- fixedly installed
- unmanned plane
- connection structure
- mission payload
- clamp
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Abstract
The utility model relates to air vehicle technique fields, and disclose a kind of unmanned plane mission payload connection structure, including unmanned plane main body, the inside of the unmanned plane main body is fixedly installed with gondola, the left and right sides of the gondola is fixedly installed with support arm, two opposite sides of the support arm are fixedly installed with fixer, and the inside of two fixers is fixedly installed with power motor, is fixedly installed with flabellum on the output shaft of two power motors.Unmanned plane mission payload connection structure, by having opened up card slot to link block, achieve the effect that limit clamp, by being mounted with adjustable spring to clamp, having reached activity template can be with movable effect, and by being mounted with squeezing rod to activity template, having reached can be with Compressive activities piece purpose outside clamp, by being mounted with to extend to the bail of inside grooves to activity template, achieve the effect that load connection structure is easy for installation and removal.
Description
Technical field
The utility model relates to air vehicle technique field, specially a kind of unmanned plane mission payload connection structure.
Background technique
UAV abbreviation unmanned plane is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft without cockpit on machine, but is equipped with the equipment such as automatic pilot and presetting apparatus, can be in wireless remotecontrol
It is lower to take off as conventional airplane or launched with booster rocket, can also be taken to by machine tool it is aerial launch flight, can when recycling
With the mode automatic Landing as conventional airplane landing mission, can also be recycled by remote control parachute or block, it can be repeatedly
Using multiple.
Mission payload, refer to those be provided on unmanned plane be completion task equipment, including execute electronic warfare, scout and
The equipment of the required by task such as weapons delivery, the fast development of the mission payload of unmanned plane greatly extend the application neck of unmanned plane
Domain, for unmanned plane according to the difference of its function and type, the mission payload equipped thereon is also different, but current mission payload is set
Standby not to be easy for installation and removal, to investigation efficiency, there is certain influences, so propose a kind of unmanned plane mission payload
Connection structure.
Utility model content
(1) the technical issues of solving
In view of the deficiencies of the prior art, the utility model provides a kind of unmanned plane mission payload connection structure, has
The advantages of being easy for installation and removal, solving current mission payload equipment is inconvenient to mount and dismount, and exists to investigation efficiency
Certain the problem of influencing.
(2) technical solution
To realize the above-mentioned purpose being easy for installation and removal, the utility model is provided the following technical solutions: a kind of unmanned plane
With mission payload connection structure, including unmanned plane main body, the inside of the unmanned plane main body is fixedly installed with gondola, the gondola
The left and right sides be fixedly installed with support arm, two opposite sides of the support arm are fixedly installed with fixer, two
The inside of the fixer is fixedly installed with power motor, and fan is fixedly installed on the output shaft of two power motors
Leaf, the bottom of the gondola are fixedly installed with connecting plate, and the left and right sides of the connecting plate is fixedly installed with support leg, described
The bottom of connecting plate and it is located at and is formed by crevice place between two support legs and is fixedly installed with link block, the link block
Bottom offer card slot, the left and right sides of the card slot inner wall opens up fluted, and the bottom of the link block is fixedly mounted
There is snap-gauge, the clamp extended to inside card slot is fixedly installed at the top of the snap-gauge, the inside of the clamp is fixedly installed with
Fixinig plate, the left and right sides of the fixinig plate and the inside for being located at clamp are fixedly installed with adjustable spring, two flexible bullets
The opposite side of spring is fixedly installed with activity template, and two opposite sides of the activity template are fixedly installed with and extend to clamp
External squeezing rod, the opposite side of two activity templates is fixedly installed with the bail for extending to inside grooves, the card
The bottom of plate is fixedly installed with camera, and the left and right sides of the camera offers thread groove, the bottom of the snap-gauge and
It is fixedly installed with fixture block positioned at the left and right sides of camera, the inside of two fixture blocks, which is threaded with, extends to screw thread
Threaded post inside slot.
Preferably, the front and back of the gondola is fixedly mounted there are two support arm, and the outside of the support arm is solid
Dingan County is equipped with reinforcing bar.
Preferably, the output shaft of the power motor is through flabellum, the outside of the power motor output shaft and positioned at fan
Anti-drop block is fixedly installed at the top of leaf.
Preferably, the bottom of the support leg is fixedly installed with non-slip mat, and the thickness of the non-slip mat is not less than half centimeter.
Preferably, two opposite sides of the squeezing rod are fixedly installed with crushing block, and two crushing blocks are opposite
Side offer anti-skid chequer.
Preferably, the depth of the groove is not more than 2/3rds of adjustable spring length, and two threaded posts are opposite
Side be fixedly installed with and turn block.
(3) beneficial effect
Compared with prior art, the utility model provides a kind of unmanned plane mission payload connection structure, has following
The utility model has the advantages that
1, unmanned plane mission payload connection structure is mounted with gondola to unmanned plane main body by setting, has reached solid
The effect for determining support arm is mounted with fixer to support arm by setting, has achieved the effect that fixed power motor, passed through setting
Flabellum is mounted with to force motor is determined, has achieved the effect that unmanned plane can take off, and support leg is mounted with to connecting plate by setting,
Achieve the effect that support entire fuselage when unmanned plane landing.
2, unmanned plane mission payload connection structure has opened up card slot to link block by setting, has reached to clamp
The effect limited is mounted with adjustable spring to clamp by setting, and having reached activity template can be with movable effect, by setting
It sets and squeezing rod is mounted with to activity template, activity template can be pacified by setting with Compressive activities piece purpose outside clamp by having reached
The bail for extending to inside grooves has been filled, has achieved the effect that load connection structure is easy for installation and removal.
Detailed description of the invention
Fig. 1 is the utility model structure front view;
Fig. 2 is the enlarged drawing of A in the utility model Fig. 1.
In figure: 1 unmanned plane main body, 2 gondolas, 3 support arms, 4 fixers, 5 power motors, 6 flabellums, 7 connecting plates, 8 supports
Foot, 9 link blocks, 10 card slots, 11 grooves, 12 snap-gauges, 13 clamps, 14 fixinig plates, 15 adjustable springs, 16 activity templates, 17 squeezing rods,
18 bails, 19 cameras, 20 thread grooves, 21 fixture blocks, 22 threaded posts.
Specific embodiment
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.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
A kind of unmanned plane mission payload connection structure referring to FIG. 1-2, including unmanned plane main body 1, unmanned plane main body 1
Inside be fixedly installed with gondola 2, the left and right sides of gondola 2 is fixedly installed with support arm 3, and the front and back of gondola 2 is equal
It is fixedly mounted there are two support arm 3, the outside of support arm 3 is fixedly installed with reinforcing bar, and two opposite sides of support arm 3 are solid
Dingan County is equipped with fixer 4, and the inside of two fixers 4 is fixedly installed with power motor 5, the output shaft of two power motors 5
On be fixedly installed with flabellum 6, the output shaft of power motor 5 runs through flabellum 6, the outside of 5 output shaft of power motor and is located at flabellum
6 top is fixedly installed with anti-drop block, and the bottom of gondola 2 is fixedly installed with connecting plate 7, and the left and right sides of connecting plate 7 is fixed
Support leg 8 is installed, the bottom of support leg 8 is fixedly installed with non-slip mat, and the thickness of non-slip mat is not less than half centimeter, connecting plate 7
Bottom and be located at and be formed by crevice place between two support legs 8 and be fixedly installed with link block 9, the bottom of link block 9 opens up
There is card slot 10, the left and right sides of 10 inner wall of card slot opens up fluted 11, and the bottom of link block 9 is fixedly installed with snap-gauge 12, card
The top of plate 12 is fixedly installed with the clamp 13 extended to inside card slot 10, and the inside of clamp 13 is fixedly installed with fixinig plate 14,
The left and right sides of the fixinig plate 14 and inside for being located at clamp 13 is fixedly installed with adjustable spring 15, two adjustable springs 15 are opposite
Side is fixedly installed with activity template 16, and the opposite side of two activity templates 16, which is fixedly installed with, to be extended to outside clamp 13
Squeezing rod 17, two opposite sides of squeezing rod 17 are fixedly installed with crushing block, and two opposite sides of crushing block open up
There is anti-skid chequer, the opposite side of two activity templates 16 is fixedly installed with the bail 18 extended to inside groove 11, snap-gauge 12
Bottom is fixedly installed with camera 19, and the left and right sides of camera 19 offers thread groove 20, the bottom of snap-gauge 12 and is located at
The left and right sides of camera 19 is fixedly installed with fixture block 21, and the inside of two fixture blocks 21, which is threaded with, extends to thread groove
Threaded post 22 inside 20, the depth of groove 11 are not more than 2/3rds of 15 length of adjustable spring, and two threaded posts 22 are opposite
Side be fixedly installed with and turn block.
When in use, squeezing rod 17 is pressed, activity template 16 can be by the contraction of adjustable spring 15 to the side of fixinig plate 14
It is mobile, while activity template 16 will drive bail 18 and exit groove 11, then can take out clamp 13 from card slot 10, by twisting
Dynamic threaded post 22 can remove snap-gauge 12 from camera 19, be finally reached the mesh that load connection structure is easy for installation and removal
's.
In conclusion unmanned plane mission payload connection structure, is mounted with gondola 2 to unmanned plane main body 1 by setting,
Fixed support arm 3 is achieved the effect that, fixer 4 is mounted with to support arm 3 by setting, has reached fixed power motor 5
Effect is mounted with flabellum 6 to determining force motor 5 by setting, has achieved the effect that unmanned plane can take off, by being arranged to connection
Plate 7 is mounted with support leg 8, has achieved the effect that support entire fuselage when unmanned plane landing.
Also, card slot 10 is opened up to link block 9 by setting, has achieved the effect that limit clamp 13, pass through
Setting is mounted with adjustable spring 15 to clamp 13, and having reached activity template 16 can be with movable effect, by being arranged to activity template 16
It is mounted with squeezing rod 17, activity template 16 can be installed by setting with 16 purpose of Compressive activities piece outside clamp 13 by having reached
The bail 18 inside groove 11 is extended to, has achieved the effect that load connection structure is easy for installation and removal.
It should be noted that the terms "include", "comprise" or its any other variant are intended to the packet of nonexcludability
Contain, so that the process, method, article or equipment for including a series of elements not only includes those elements, but also including
Other elements that are not explicitly listed, or further include for 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, article or equipment in there is also other identical elements.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of unmanned plane mission payload connection structure, including unmanned plane main body (1), it is characterised in that: the unmanned owner
The inside of body (1) is fixedly installed with gondola (2), and the left and right sides of the gondola (2) is fixedly installed with support arm (3), and two
The opposite side of the support arm (3) is fixedly installed with fixer (4), the fixed peace in the inside of two fixers (4)
Equipped with power motor (5), it is fixedly installed with flabellum (6) on the output shaft of two power motors (5), the gondola (2)
Bottom is fixedly installed with connecting plate (7), and the left and right sides of the connecting plate (7) is fixedly installed with support leg (8), the connection
The bottom of plate (7) and it is located at and is formed by crevice place between two support legs (8) and is fixedly installed with link block (9), it is described
The bottom of link block (9) offers card slot (10), and the left and right sides of card slot (10) inner wall opens up fluted (11), described
The bottom of link block (9) is fixedly installed with snap-gauge (12), is fixedly installed at the top of the snap-gauge (12) and is extended to card slot (10)
Internal clamp (13), the inside of the clamp (13) are fixedly installed with fixinig plate (14), the left and right two of the fixinig plate (14)
Side and be located at clamp (13) inside be fixedly installed with adjustable spring (15), two opposite sides of the adjustable spring (15) are equal
It is fixedly installed with activity template (16), two opposite sides of the activity template (16) are fixedly installed with and extend to clamp (13) outside
The squeezing rod (17) in portion, two opposite sides of the activity template (16), which are fixedly installed with, extends to the internal card of groove (11)
It follows closely (18), the bottom of the snap-gauge (12) is fixedly installed with camera (19), and the left and right sides of the camera (19) opens up
Have thread groove (20), the bottom of the snap-gauge (12) and be located at camera (19) the left and right sides be fixedly installed with fixture block
(21), the inside of two fixture blocks (21), which is threaded with, extends to the internal threaded post (22) of thread groove (20).
2. a kind of unmanned plane mission payload connection structure according to claim 1, it is characterised in that: the gondola (2)
Front and back be fixedly mounted there are two support arm (3), the outside of the support arm (3) is fixedly installed with reinforcing bar.
3. a kind of unmanned plane mission payload connection structure according to claim 1, it is characterised in that: the power motor
(5) output shaft runs through flabellum (6), the outside of power motor (5) output shaft and the top fixed installation for being located at flabellum (6)
There is anti-drop block.
4. a kind of unmanned plane mission payload connection structure according to claim 1, it is characterised in that: the support leg
(8) bottom is fixedly installed with non-slip mat, and the thickness of the non-slip mat is not less than half centimeter.
5. a kind of unmanned plane mission payload connection structure according to claim 1, it is characterised in that: two extruding
The opposite side of column (17) is fixedly installed with crushing block, and two opposite sides of the crushing block offer anti-skid chequer.
6. a kind of unmanned plane mission payload connection structure according to claim 1, it is characterised in that: the groove (11)
Depth be not more than adjustable spring (15) length 2/3rds, two opposite sides of the threaded post (22) are fixedly mounted
Turn block.
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CN201920063009.5U CN209427020U (en) | 2019-01-15 | 2019-01-15 | A kind of unmanned plane mission payload connection structure |
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CN201920063009.5U CN209427020U (en) | 2019-01-15 | 2019-01-15 | A kind of unmanned plane mission payload connection structure |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111746811A (en) * | 2020-07-17 | 2020-10-09 | 杭州同济测绘有限公司 | Unmanned aerial vehicle photogrammetry mounting platform |
CN113895621A (en) * | 2021-10-15 | 2022-01-07 | 浙江科比特科技有限公司 | Unmanned aerial vehicle with carry megaphone |
-
2019
- 2019-01-15 CN CN201920063009.5U patent/CN209427020U/en active Active
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111746811A (en) * | 2020-07-17 | 2020-10-09 | 杭州同济测绘有限公司 | Unmanned aerial vehicle photogrammetry mounting platform |
CN113895621A (en) * | 2021-10-15 | 2022-01-07 | 浙江科比特科技有限公司 | Unmanned aerial vehicle with carry megaphone |
CN113895621B (en) * | 2021-10-15 | 2024-05-07 | 浙江科比特科技有限公司 | Unmanned aerial vehicle with carry megaphone |
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