CN207759077U - A kind of waterproof test flight device of unmanned plane - Google Patents
A kind of waterproof test flight device of unmanned plane Download PDFInfo
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- CN207759077U CN207759077U CN201721758859.4U CN201721758859U CN207759077U CN 207759077 U CN207759077 U CN 207759077U CN 201721758859 U CN201721758859 U CN 201721758859U CN 207759077 U CN207759077 U CN 207759077U
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- China
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- unmanned plane
- hydraulic pipeline
- water pipe
- waterproof test
- test flight
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Abstract
The utility model discloses a kind of waterproof test flight devices of unmanned plane, including supporting rack, porous nozzle, water pump, hydraulic pipeline and unmanned plane during flying simulator, support frame as described above top is equipped with head piece, the head piece is equipped with sliding slot, sliding block is equipped in the sliding slot, and sliding block can slide in sliding slot, the porous nozzle is connect with slider locking, the water pump is connect with hydraulic pipeline end, multiple water pipe joints are equidistantly equipped on the hydraulic pipeline, the water pipe joint lower end is equipped with conduit switch, the unmanned plane during flying simulator setting and lower end among supporting rack, and it is fixedly connected with the ground, the porous nozzle is connected by rubber hose and water pipe joint, to solve the technological deficiency of unmanned plane rainy day waterproof test flight.
Description
Technical field
The utility model belongs to unmanned plane during flying technical field of measurement and test, specifically, the utility model is related to it is a kind of nobody
The waterproof test flight device of machine.
Background technology
With the further development of unmanned air vehicle technique, our demands to unmanned plane are higher and higher, till now, to meet nothing
The man-machine needs that operation can be carried out in the environment that rains, we have further developed waterproof unmanned plane.But with waterproof without
Man-machine development, in terms of the waterproof test of unmanned plane, we or one side blank are basic at present only using tap to it
Sprinkling is simply detected, and rainy environment, and the accurately state of flight under control rainfall can not be accurately imitated out,
Therefore, the needs of test be cannot be satisfied at all.
Utility model content
The utility model provides a kind of waterproof test flight device of unmanned plane, to solve above-mentioned unmanned plane rainy day anti-fine grinding
The technological deficiency of row test.
To achieve the goals above, the technical solution that the utility model is taken is：A kind of waterproof test flight of unmanned plane
Device, including supporting rack, porous nozzle, water pump, hydraulic pipeline and unmanned plane during flying simulator, support frame as described above top are equipped with
Head piece, the head piece is equipped with sliding slot, is equipped with sliding block in the sliding slot, and sliding block can slide in sliding slot, described porous
Nozzle is connect with slider locking, and the water pump is connect with hydraulic pipeline end, and multiple water are equidistantly equipped on the hydraulic pipeline
Pipe connector, the water pipe joint lower end is equipped with conduit switch, in the unmanned plane during flying simulator setting and supporting rack
Between lower end, and be fixedly connected with the ground, the porous nozzle is connected by rubber hose and water pipe joint.
Preferably, the hydraulic pipeline is equipped with pressure display table.
Preferably, the unmanned plane during flying simulator is made of fixed seat, motor, rotating seat, cylinder and rotating bar, institute
It states fixed seat to be fixedly connected with the ground, be connect inside the motor and fixed seat, the output shaft of the motor passes through deep-groove ball axis
Hold and be rotatablely connected with fixed seat, the output axis connection of the rotating seat and motor, the cylinder barrel lower end of the cylinder by bolt with
Rotating seat is fixedly connected, and the piston rod end of the cylinder is equipped with ball groove, and the rotating bar lower end is equipped with steel ball, and upper end, which is equipped with, to be pricked
Band, and the rotating bar forms ball pair by steel ball and ball groove.
Preferably, the rotating seat is cross.
It is using the advantageous effect of above technical scheme：The waterproof test flight device of the unmanned plane, the porous nozzle
It is equidistantly uniformly provided on head piece multiple so that water outlet is uniform, can simulate rainfall environment well；In addition the control
Case is equipped with water, water spraying time and unmanned plane during flying simulator control button, and difference can be simulated by realizing porous nozzle
The rainfall and rain time of size；It, can be with by the mutual cooperation of rotating seat and cylinder in unmanned plane during flying simulator
The case where allowing tested unmanned plane flexibly to simulate each flight angle improves the rich of test, the experiment of test
Data area is wide, and reliability is high.
Description of the drawings
Fig. 1 is the waterproof test flight device integral installation distribution structure schematic diagram of the unmanned plane；
Fig. 2 is the waterproof test flight device front view of the unmanned plane；
Fig. 3 is the waterproof test flight device vertical view of the unmanned plane；
Fig. 4 is unmanned plane during flying simulator structural schematic diagram.
Wherein：
1, supporting rack；2, porous nozzle；3, water pump；4, hydraulic pipeline；5, unmanned plane during flying simulator；10, head piece；
10-1, sliding slot；11, sliding block；12, control cabinet；40, pressure display table；41, water pipe joint；41-1, conduit switch；50, fixed
Seat；51, motor；52, rotating seat；53, cylinder；53-1, ball groove；54, rotating bar；54-1, steel ball；54-2, band.
Specific implementation mode
Below against attached drawing, by the description of the embodiment, making to specific embodiment of the present utility model further detailed
Thin explanation, it is therefore an objective to help those skilled in the art to the design of the utility model, technical solution have it is more complete, accurate and
Deep understanding, and contribute to its implementation.
As shown in Figures 1 to 4, the utility model is a kind of waterproof test flight device of unmanned plane, to solve unmanned plane
The technological deficiency of rainy day waterproof test flight.
Including supporting rack 1, porous nozzle 2, water pump 3, hydraulic pipeline 4 and unmanned plane specifically, as shown in Figures 1 to 4,
Aerolog 5,1 top of support frame as described above are equipped with head piece 10, and the head piece 10 is equipped with sliding slot 10-1, the sliding slot
Sliding block 11 is equipped in 10-1, and sliding block 11 can slide in sliding slot 10-1, the porous nozzle 2 is connected with the locking of sliding block 11, institute
It states water pump 3 to connect with 4 end of hydraulic pipeline, multiple water pipe joints 41, the water pipe is equidistantly equipped on the hydraulic pipeline 4
41 lower end of connector is equipped with conduit switch 41-1, the setting of unmanned plane during flying simulator 5 and 1 intermediate lower end of supporting rack, and
It is fixedly connected with the ground, the porous nozzle 2 is connected by rubber hose and water pipe joint 41.
As shown in Fig. 2, the hydraulic pipeline 4 is equipped with pressure display table 41.
As shown in Figure 1, Figure 2, Figure 3, Figure 4, the unmanned plane during flying simulator 5 is by fixed seat 50, motor 51, rotating seat
52, cylinder 53 and rotating bar 54 form, and the fixed seat 50 is fixedly connected with the ground, connects inside the motor 51 and fixed seat 50
It connects, the output shaft of the motor 51 is rotatablely connected by deep groove ball bearing and fixed seat 50, the rotating seat 52 and motor 51
Axis connection is exported, the cylinder barrel lower end of the cylinder 53 is fixedly connected by bolt with rotating seat 52, the piston rod of the cylinder 53
End is equipped with ball groove 53-1, and 54 lower end of the rotating bar is equipped with steel ball 54-1, and upper end is equipped with band 54-2, and the rotating bar 54
Ball pair is formed by steel ball 54-1 and ball groove 53-1.
As shown in Figure 1, the rotating seat 52 is cross.
Specific working mode is illustrated with specific embodiment below：
The cantilever of unmanned plane to be measured is bundled in cylinder by the waterproof test flight device of the unmanned plane by band 54-2
The end of 53 piston rod because the rotating seat 52 is cross, taken in the present embodiment be four cantilever unmanned planes into
Capable test flight changes the structure of rotating seat 52, can also test six cantilevers or eight cantilever unmanned planes, wait for that cantilever bundlees
Afterwards, then start water pump 3 to supply water to hydraulic pipeline 4, pressure of supply water is observed by the pressure display table 41 on hydraulic pipeline 4, is protected
The hydraulic pressure demonstrate,proved in every hydraulic pipeline 4 is consistent, indirectly ensure that the uniformity that porous nozzle 2 is discharged, then waits for that hydraulic pressure is consistent
Afterwards, conduit switch 41-1 is opened manually, and then water pump 3 pumps water by rubber hose to porous nozzle 2 from water pipe joint 41
It is discharged, rainfall environment can be simulated well；In addition the control cabinet 12 is equipped with water, water spraying time and unmanned plane and flies
Row simulator control button, different size of rainfall and rain time can be simulated by realizing porous nozzle 2.
Then by control cabinet 12, start motor 51 and rotating seat 52 is driven to rotate, then drive the fuselage of unmanned plane slow
Rotation, while the rotor of unmanned plane being made also to be rotated under the motor effect of itself, it is stretched out by four 53 piston rods of cylinder
Length, change the inclined degree of unmanned aerial vehicle body because the piston rod end of the cylinder 53 is equipped with ball groove 53-1, described turn
54 lower end of lever is equipped with steel ball 54-1, and upper end is equipped with band 54-2, and the rotating bar 54 passes through steel ball 54-1 and ball groove 53-1
Ball pair is formed, so being not in mechanical interference phenomenon by the position of four band 54-2 bindings, passes through unmanned plane during flying mould
The mutual cooperation of rotating seat 52 and cylinder 53 in quasi- device, can allow tested unmanned plane flexibly to simulate each flight
The case where angle, improves the rich of test, and the experimental data range of test is wide, and reliability is high.
The utility model is exemplarily described above in association with attached drawing, it is clear that the utility model implements not
It is limited by aforesaid way, as long as using the various unsubstantialities of the methodology and technical solution progress of the utility model
Improvement；Or it is not improved, above-mentioned design and technical solution by the utility model directly apply to other occasions, at this
Within the protection domain of utility model.
Claims (4)
1. a kind of waterproof test flight device of unmanned plane, it is characterised in that：Including supporting rack (1), porous nozzle (2), water pump
(3), hydraulic pipeline (4) and unmanned plane during flying simulator (5), support frame as described above (1) top are equipped with head piece (10), the top
Crossbeam (10) is equipped with sliding slot (10-1), is equipped with sliding block (11) in the sliding slot (10-1), and sliding block (11) can be in sliding slot (10-
1) sliding in, the porous nozzle (2) connect with sliding block (11) locking, and the water pump (3) connect with hydraulic pipeline (4) end,
Multiple water pipe joints (41) are equidistantly equipped on the hydraulic pipeline (4), water pipe joint (41) lower end is equipped with water pipe
It switchs (41-1), unmanned plane during flying simulator (5) setting and the intermediate lower end of supporting rack (1), and is fixedly connected with the ground,
The porous nozzle (2) is connected by rubber hose and water pipe joint (41).
2. a kind of waterproof test flight device of unmanned plane according to claim 1, it is characterised in that：The hydraulic pipeline
(4) it is equipped with pressure display table (40).
3. a kind of waterproof test flight device of unmanned plane according to claim 1, it is characterised in that：The unmanned plane flies
Row simulator (5) is made of fixed seat (50), motor (51), rotating seat (52), cylinder (53) and rotating bar (54), described solid
Reservation (50) is fixedly connected with the ground, and is connect inside the motor (51) and fixed seat (50), the output shaft of the motor (51)
It is rotatablely connected by deep groove ball bearing and fixed seat (50), the output axis connection of the rotating seat (52) and motor (51) is described
The cylinder barrel lower end of cylinder (53) is fixedly connected by bolt with rotating seat (52), and the piston rod end of the cylinder (53) is equipped with ball
Slot (53-1), rotating bar (54) lower end are equipped with steel ball (54-1), and upper end is equipped with band (54-2), and the rotating bar (54)
Ball pair is formed by steel ball (54-1) and ball groove (53-1).
4. a kind of waterproof test flight device of unmanned plane according to claim 3, it is characterised in that：The rotating seat
(52) it is cross.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721758859.4U CN207759077U (en) | 2017-12-16 | 2017-12-16 | A kind of waterproof test flight device of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721758859.4U CN207759077U (en) | 2017-12-16 | 2017-12-16 | A kind of waterproof test flight device of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207759077U true CN207759077U (en) | 2018-08-24 |
Family
ID=63187248
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721758859.4U Active CN207759077U (en) | 2017-12-16 | 2017-12-16 | A kind of waterproof test flight device of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207759077U (en) |
-
2017
- 2017-12-16 CN CN201721758859.4U patent/CN207759077U/en active Active
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