CN209581854U - A kind of unmanned plane Anti-seismic undercarriage - Google Patents

A kind of unmanned plane Anti-seismic undercarriage Download PDF

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Publication number
CN209581854U
CN209581854U CN201920142940.2U CN201920142940U CN209581854U CN 209581854 U CN209581854 U CN 209581854U CN 201920142940 U CN201920142940 U CN 201920142940U CN 209581854 U CN209581854 U CN 209581854U
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China
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unmanned plane
connecting rod
spring
bull stick
sliding block
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CN201920142940.2U
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Chinese (zh)
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高明
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Standard Defense Technology Ltd By Share Ltd
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Standard Defense Technology Ltd By Share Ltd
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Abstract

The utility model provides a kind of unmanned plane Anti-seismic undercarriage, including stabilizer blade, tension spring, sliding slot, first bull stick, connecting rod, unmanned plane mounting platform, sliding block, T-type fixture block, spring, card slot, rectangular channel and guide rod, stabilizer blade inner side end offers sliding slot, spring is fixed on upper surface in sliding slot, sliding block is mounted on lower spring end, sliding block lower end surface offers card slot, T-type fixture block is mounted on inside card slot, upper surface offers rectangular channel in card slot, T-type fixture block is installed on the guide bar, T-type fixture block left end passes through spring and sliding block elastic connection, T-type fixture block right end extends right up on the downside of the first bull stick, it is rotatablely connected on the outside of first bull stick by shaft and sliding block, connecting rod is mounted on unmanned plane mounting platform lower end surface left and right part, connecting rod lower end, which is inlayed, is fixed on the first bull stick upper end, first bull stick passes through connecting rod and nobody Machine mounting platform lower end is connected, and the design achieves damping and the functions of folding storage.

Description

A kind of unmanned plane Anti-seismic undercarriage
Technical field
The utility model is a kind of unmanned plane Anti-seismic undercarriage, belongs to unmanned plane apparatus field.
Background technique
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, is using radio robot and to provide for oneself The not manned aircraft of presetting apparatus manipulation, or fully or intermittently automatically operated by car-mounted computer, unmanned plane It by application field, can be divided into military with civilian, military aspect, unmanned plane is divided into reconnaissance plane and target drone, civilian aspect, unmanned plane+ Industrial application, is that unmanned plane has really just needed, and existing unmanned plane undercarriage mostly uses greatly rigid support, due to rigid support Lack buffering, even normally landing, it is also possible to which the precision equipment that will lead on unmanned plane damages, and existing unmanned plane Undercarriage can not very easily dismantle storage, not readily portable.
Utility model content
In view of the deficienciess of the prior art, the utility model aim is to provide a kind of unmanned plane Anti-seismic undercarriage, To solve the problems mentioned in the above background technology, the utility model is easy to use, realizes the function of damping and folding storage Can, structurally reasonable, high reliablity.
To achieve the goals above, the utility model is achieved through the following technical solutions: a kind of unmanned plane use is anti- Shake type undercarriage, including stabilizer blade, tension spring, sliding slot, the first bull stick, connecting rod, unmanned plane mounting platform, sliding block, T-type fixture block, bullet Spring, card slot, rectangular channel and guide rod, the stabilizer blade inner side end offer sliding slot, and the sliding block and spring are installed in Inside sliding slot, the spring is fixed on upper surface in sliding slot, and the sliding block is mounted on lower spring end, the sliding block by spring with Stabilizer blade elastic connection, the sliding block lower end surface offer card slot, and the T-type fixture block is mounted on inside card slot, in the card slot on End face offers rectangular channel, and the guide rod and spring are installed in inside rectangular channel, and the T-type fixture block is mounted on guide rod On, T-type fixture block left end is extended right up under the first bull stick by spring and sliding block elastic connection, the T-type fixture block right end Side, the first bull stick outside are rotatablely connected by shaft and sliding block, and the connecting rod is mounted on unmanned plane mounting platform lower end Face left and right part, the connecting rod lower end, which is inlayed, is fixed on the first bull stick upper end, and first bull stick passes through connecting rod and unmanned plane Mounting platform lower end is connected.
Further, the stabilizer blade quantity is two, and two stabilizer blade lower ends are welded with arc contact plate.
Further, the first bull stick quantity is two, offers column on the inside of two first bull stick upper surfaces Shape slot is welded with connecting column, connecting rod annular side and connecting column annular side inside the cylindrical groove It is threaded, the connecting rod is detachably connected by screw thread and connecting column.
Further, unmanned plane mounting platform lower end surface left and right part is welded with through post, and the through post is to downward It extends to inside connecting rod, the connecting rod upper end is detachably connected by screw thread and through post.
The utility model has the beneficial effects that a kind of unmanned plane Anti-seismic undercarriage of the utility model, the utility model By addition stabilizer blade, tension spring, sliding slot, the first bull stick, connecting rod, unmanned plane mounting platform, sliding block, T-type fixture block, spring, card slot, Rectangular channel and guide rod, the design achieves damping and the functions of folding storage, solve existing unmanned plane undercarriage, Rigid support is mostly used greatly, is buffered since rigid support lacks, even normally landing, it is also possible to will lead to the essence on unmanned plane Close equipment is damaged, and existing unmanned plane undercarriage can not very easily dismantle storage, not readily portable problem.
Because being added to arc contact plate, which improves stability of the undercarriage when out-of-flatness ground is landed, because adding Cylindrical groove and connecting column are added, the design is convenient for the connection between connecting rod and the first bull stick, because being added to through post, the design Convenient for the connection between connecting rod and unmanned plane mounting platform, the utility model is easy to use, realizes damping and folds and receives The function of receiving, structurally reasonable, high reliablity.
Detailed description of the invention
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model Sign, objects and advantages will become more apparent upon:
Fig. 1 is a kind of structural schematic diagram of unmanned plane Anti-seismic undercarriage of the utility model;
Fig. 2 is the enlarged diagram in a kind of unmanned plane Anti-seismic undercarriage of the utility model at A;
In figure: 1- stabilizer blade, 2- tension spring, 3- sliding slot, the first bull stick of 4-, 5- connecting rod, 6- unmanned plane mounting platform, 7- are sliding Block, 8-T type fixture block, 9- spring, 10- card slot, 11- rectangular channel, 12- guide rod.
Specific embodiment
To be easy to understand the technical means, creative features, achievement of purpose, and effectiveness of the utility model, below In conjunction with specific embodiment, the utility model is further described.
Fig. 1 and Fig. 2 are please referred to, the utility model provides a kind of technical solution: a kind of unmanned plane Anti-seismic undercarriage, packet Include stabilizer blade 1, tension spring 2, sliding slot 3, the first bull stick 4, connecting rod 5, unmanned plane mounting platform 6, sliding block 7, T-type fixture block 8, spring 9, card Slot 10, rectangular channel 11 and guide rod 12,1 inner side end of stabilizer blade offer sliding slot 3, and sliding block 7 and spring 9 are installed in sliding slot Inside 3, spring 9 is fixed on upper surface in sliding slot 3, and sliding block 7 is mounted on 9 lower end of spring, and sliding block 7 passes through 1 elasticity of spring 9 and stabilizer blade Connection, 7 lower end surface of sliding block offer card slot 10, and T-type fixture block 8 is mounted on inside card slot 10, and upper surface offers square in card slot 10 Shape slot 11, guide rod 12 and spring 9 are installed in inside rectangular channel 11, and T-type fixture block 8 is mounted on guide rod 12, T-type fixture block By spring 9 and 7 elastic connection of sliding block, 8 right end of T-type fixture block is extended right up on the downside of the first bull stick 4 for 8 left ends, outside the first bull stick 4 Side is rotatablely connected by shaft and sliding block 7, and connecting rod 5 is mounted on 6 lower end surface left and right part of unmanned plane mounting platform, under connecting rod 5 End, which is inlayed, is fixed on 4 upper end of the first bull stick, and the first bull stick 4 is connected by connecting rod 5 with 6 lower end of unmanned plane mounting platform, nothing It is man-machine in landing, arc contact plate and ground touch, and then unmanned plane mounting platform 6 generates downward rush to connecting rod 5 Power is hit, then connecting rod 5 moves down under downward impact force action, and connecting rod 5 moves down the first bull stick of drive 4 downwards Mobile, the first bull stick 4 moves down band movable slider 7 and moves down, the first bull stick 4 move down band movable slider 7 along sliding slot 3 to Lower movement, sliding block 7 moves down so that tension spring 2 extends and generates elastic force, so that downward impact force is converted into spring 9 Elastic force, and then the function of damping is realized, when needing to store undercarriage, user of service first holds connecting rod 5 And rotate clockwise, connecting rod 5 is rotated clockwise and is moved up under the action of screw thread, when 5 company of being moved upward to of connecting rod When connecing on the upside of column, connecting rod of stopping rotating 5, then user of service holds T-type fixture block 8 and is moved to the left, and T-type fixture block 8 is to moving to left It moves so that spring 9 compresses and generates elastic force, when T-type fixture block 8 is moved to the left 10 inside of card slot, stopping is moved to the left T-type card Block 8, then user of service holds the first bull stick 4 and rotates clockwise 90 °, and then user of service unclamps T-type fixture block 8, then T-type Fixture block 8 moves right under the action of spring 9 and carries out clamping fixation to the first bull stick 4, carries out to realize to undercarriage The function of folding storage.
1 quantity of stabilizer blade is two, and two 1 lower ends of stabilizer blade are welded with arc contact plate, the design of arc contact plate Improve stability when unmanned plane landing.
First bull stick, 4 quantity is two, offers cylindrical groove on the inside of two 4 upper surfaces of the first bull stick, inside cylindrical groove It is welded with connecting column, 5 annular side of connecting rod and connecting column annular side are threaded, and connecting rod 5 is logical It crosses screw thread to be detachably connected with connecting column, the design of connecting column can very easily dismantle connecting rod 5.
6 lower end surface left and right part of unmanned plane mounting platform is welded with through post, and through post extends downward into inside connecting rod 5, 5 upper end of connecting rod is detachably connected by screw thread and through post.
The basic principles and main features of the present invention and the advantages of the present invention have been shown and described above, for For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this In the case where the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent elements of the claims All changes are embraced therein.It should not treat any reference in the claims as limiting related right It is required that.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art The other embodiments being understood that.

Claims (4)

1. a kind of unmanned plane Anti-seismic undercarriage, including the installation of stabilizer blade, tension spring, sliding slot, the first bull stick, connecting rod, unmanned plane Platform, sliding block, T-type fixture block, spring, card slot, rectangular channel and guide rod, it is characterised in that: the stabilizer blade inner side end opens up There is sliding slot, the sliding block and spring are installed in inside sliding slot, and the spring is fixed on upper surface in sliding slot, the sliding block peace Mounted in lower spring end, for the sliding block by spring and stabilizer blade elastic connection, the sliding block lower end surface offers card slot, the T-type Fixture block is mounted on inside card slot, and upper surface offers rectangular channel in the card slot, and the guide rod and spring are installed in square Inside shape slot, on the guide bar, T-type fixture block left end is described by spring and sliding block elastic connection for the T-type fixture block installation T-type fixture block right end extends right up on the downside of the first bull stick, is rotatablely connected on the outside of first bull stick by shaft and sliding block, described Connecting rod is mounted on unmanned plane mounting platform lower end surface left and right part, and the connecting rod lower end, which is inlayed, is fixed on the first bull stick upper end, First bull stick is connected by connecting rod with unmanned plane mounting platform lower end.
2. a kind of unmanned plane Anti-seismic undercarriage according to claim 1, it is characterised in that: the stabilizer blade quantity is two A, two stabilizer blade lower ends are welded with arc contact plate.
3. a kind of unmanned plane Anti-seismic undercarriage according to claim 1, it is characterised in that: the first bull stick quantity It is two, offers cylindrical groove on the inside of two first bull stick upper surfaces, the equal company of being welded with inside the cylindrical groove Connect column, connecting rod annular side and connecting column annular side are threaded, the connecting rod by screw thread with Connecting column is detachably connected.
4. a kind of unmanned plane Anti-seismic undercarriage according to claim 1, it is characterised in that: the unmanned plane installation is flat Platform lower end surface left and right part is welded with through post, and the through post extends downward into inside connecting rod, and the connecting rod upper end passes through Screw thread is detachably connected with through post.
CN201920142940.2U 2019-01-25 2019-01-25 A kind of unmanned plane Anti-seismic undercarriage Active CN209581854U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201920142940.2U CN209581854U (en) 2019-01-25 2019-01-25 A kind of unmanned plane Anti-seismic undercarriage

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201920142940.2U CN209581854U (en) 2019-01-25 2019-01-25 A kind of unmanned plane Anti-seismic undercarriage

Publications (1)

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CN209581854U true CN209581854U (en) 2019-11-05

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111031724A (en) * 2019-12-19 2020-04-17 林义 Shock-proof mounting rack for vibration element of electronic device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111031724A (en) * 2019-12-19 2020-04-17 林义 Shock-proof mounting rack for vibration element of electronic device
CN111031724B (en) * 2019-12-19 2021-01-12 林义 Shock-proof mounting rack for vibration element of electronic device

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