CN108382585A - A kind of floated aerial device - Google Patents
A kind of floated aerial device Download PDFInfo
- Publication number
- CN108382585A CN108382585A CN201810085532.8A CN201810085532A CN108382585A CN 108382585 A CN108382585 A CN 108382585A CN 201810085532 A CN201810085532 A CN 201810085532A CN 108382585 A CN108382585 A CN 108382585A
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- Prior art keywords
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- interlocking
- line wheel
- rotor
- parachute
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- 239000000523 sample Substances 0.000 claims description 16
- 238000003466 welding Methods 0.000 claims description 15
- 238000009434 installation Methods 0.000 claims description 14
- 230000015572 biosynthetic process Effects 0.000 claims 1
- 239000000203 mixture Substances 0.000 abstract description 3
- 238000010586 diagram Methods 0.000 description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000007935 neutral effect Effects 0.000 description 2
- 230000006641 stabilisation Effects 0.000 description 2
- 238000011105 stabilization Methods 0.000 description 2
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000030214 innervation Effects 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
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- 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
- B64D47/02—Arrangements or adaptations of signal or lighting devices
-
- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
The invention discloses a kind of floated aerial devices,Its structure includes screw wing,Rotor motor,Rotor assembly head,Rotor assembles connecting rod,Landing ejection lid,It takes photo by plane main body,Land supporting rack,It takes photo by plane camera,Main body of taking photo by plane is cross,4 jiaos of equal interlockings have rotor assembly connecting rod one end,Bottom end interlocking has landing supporting rack,Top middle portion is snapped with landing ejection lid,Landing supporting rack center bottom interlocking is taken photo by plane camera,Rotor assembles connecting rod and is equipped with 4,Make user's use device encounter device it is unbalance out of control when,Device can by equipped with spring,Drawstring,Meet the mechanism of the compositions such as battery plate,Make device in the out of service of the unbalance constantly automatic normal rotor of carry out out of control,And parachute capping can be automatically terminated,The parachute of assembly is set to open,Enable devices to ensure when unbalance out of control the landing of steady safety,Ensure the safe to use of device,It is more convenient for using.
Description
Technical field
The present invention is a kind of floated aerial device, belongs to aerial device field.
Background technology
It takes photo by plane also known as aerophotography or aeroplane photography, refers to obtaining vertical view from aerial photographing earth landforms, this figure is
Photo map.The video camera taken photo by plane can be controlled by photographer, can also be automatically snapped or remote control.Platform packet used in taking photo by plane
Include model airplane, aircraft, helicopter, fire balloon, blimp, rocket, kite, parachute etc..In order to allow aerial photograph to stablize,
It utilizes three-axis gyroscope stabilization function, provides the stabilization picture of high quality, in addition under long focal length lens it is also highly stable.Boat
Bat figure can clearly show geographical form, therefore other than the ring as photography art, also be employed for military, traffic
Construction, hydraulic engineering, ecological Studies, urban planning etc..
And aerial device be can take photo by plane all kinds of model airplanes, aircraft, helicopter, fire balloon, blimp,
The general designation of rocket, kite, parachute etc..
The prior art leads to the unbalance out of control of device and falls, lead in use, the easy damage because of device aviation mechanism
Cause device falls damage, causes dangerous and inconvenient.
Invention content
In view of the deficienciess of the prior art, it is an object of the present invention to provide a kind of floated aerial device, it is existing to solve
Technology leads to the unbalance out of control of device and falls, lead to falling for device in use, the easy damage because of device aviation mechanism
Damage causes dangerous and inconvenient problem.
To achieve the goals above, the present invention is to realize by the following technical solutions：A kind of floated aerial device,
Its structure includes screw wing, rotor motor, rotor assembly head, rotor assembly connecting rod, landing ejection lid, main body of taking photo by plane, landing
Supporting rack, camera of taking photo by plane, the main body of taking photo by plane are cross, and 4 jiaos of equal interlockings have rotor assembly connecting rod one end, bottom end interlocking
There is a landing supporting rack, top middle portion is snapped with landing ejection lid, and the landing supporting rack center bottom interlocking is taken photo by plane camera,
Rotor assembly connecting rod is equipped with 4, and the other end is welded with rotor assembly head, respectively with rotor assembly head, main body of taking photo by plane
Electrical connection, the rotor assembly head are correspondingly provided with 4, and interlocking is run through at middle part rotor motor, is electrically connected with rotor motor, institute
It states rotor motor and is correspondingly provided with 4, it includes speed probe, sensing that the equal interlocking in top, which has screw wing, the rotor assembly connecting rod,
Device Assembly rail, urgent trigger device, lifting connecting plate, failure warning device, link body, the link body is equipped with 4, one
With main body interlocking of taking photo by plane, and there is speed probe at end in the middle part of, the other end by sensor Assembly rail interlocking, described urgent
Trigger device is correspondingly provided with 4, and corresponding inlay is glued by speed probe side inside link body, is run through sensor and is assembled
Bar is electrically connected with speed probe, is electrically connected with main body of taking photo by plane through link body, with lifting connecting plate one end interlocking, institute
It states failure warning device and is equipped with 8, be correspondingly arranged at left and right sides of 4 sensor Assembly rails, inlay lock with sensor Assembly rail
It connects, is set to lifting connecting plate both sides, locked with lifting connecting plate interlocking, the lifting connecting plate other end and main body of taking photo by plane
Connect, the main body of taking photo by plane include machine main body, accumulator, parachute assembly cylinder, emergency stop pulling apparatus, unbutton linkage,
Cover buckle, rotor control core plate, core plate break-make electric installation, parachute fitting groove, the machine main body be cross, 4 jiaos points
Not with 4 link body interlockings, middle part front side integral, which is inlayed, is welded with parachute assembly cylinder, in the middle part of the parachute assembly cylinder
Integration is equipped with parachute fitting groove, and the capping buckle is cylinder, is equipped with 4, is combined with each other into torus, inlays snapping
Assemble cylinder inner front side in parachute, be biased in the middle part of parachute fitting groove direction side with unbutton linkage interlocking, the solution
It detains linkage to weld with emergency stop pulling apparatus, be set to above emergency stop pulling apparatus, with lifting connecting plate interlocking, the emergency stop carries
Drawing device is correspondingly provided with 4, respectively with 4 urgent trigger device interlockings, welding is inlayed with machine main body, with core plate break-make Denso
Left and right sides interlocking is set, with lifting connecting plate interlocking, the core plate break-make electric installation is glued on rear side of rotor control core plate, is set to
On rear side of parachute fitting groove, it is electrically connected with accumulator through rotor control core plate, the accumulator inlays splicing with machine main body.
Further, the urgent trigger device includes electromagnet, electromagnet assembly head, the first compressed spring, triggering limit
Splicings is inlayed in position baffle, triggering lifting plate, the first drawstring, the electromagnet left and right ends with electromagnet assembly head, one end and
Speed probe is electrically connected, and the electromagnet assembly head is integrated with link body, is hung down towards landing ejection lid side
Straight to be welded with triggering postive stop baffle, the triggering lifting plate is glued in the middle part of one end by the first compressed spring and electromagnet, another
End middle part passes through the first drawstring and lifting connecting plate interlocking.
Further, the failure warning device includes attention device, extension spring, warning energization head, warning limiting plate, police
Show and connect battery plate, warning pulley buck plate, the first line wheel, the second drawstring, the attention device is equipped with 2, inlays interlocking respectively in even
At left and right sides of bar main body, being vertically glued towards link body upper and lower sides has warning limiting plate, logical towards link body middle part
The splicing of overstretching spring has warning energization head, the warning to connect battery plate and be equipped with 4 pieces, be electrically connected with accumulator, it is corresponding respectively and
2 pieces of warning limiting plates of the left and right sides inlay splicing, are located at 2 pieces of warning limiting plates towards the close angle in link body side, the police
Show that pulley buck plate is equipped with 2 pieces, be glued respectively on rear side of left and right sides warning limiting plate, towards link body side top front side
Be snapped with the first line wheel, second drawstring is equipped with 2, one end correspond to respectively with the warning energization head interlocking of the left and right sides, separately
One end respectively with lifting connecting plate at left and right sides of interlocking.
Further, the emergency stop pulling apparatus includes third drawstring, the second line wheel, the first line wheel buck plate, third line
Wheel, the 4th line wheel, the second line wheel buck plate, lifting buck plate, the lifting buck plate are equipped with 4 pieces, and correspondence is welded in machine respectively
It is orthogonal each other 4 jiaos inside phosphor bodies, towards parachute fitting groove at be vertically welded with the first line wheel buck plate, lead to
It crosses the first line wheel buck plate and is snapped with third line wheel, the second line wheel buck plate is equipped with 2 pieces, is welded with lifting buck plate
It connects, is respectively arranged on the upper left corner and the lower right corner that lifting buck plate is formed, 2 pieces are snapped with the towards inlaying at parachute fitting groove
Four line wheels, second line wheel are equipped with 2, inlay be buckled in side and downside lifting dress to the left in the middle part of upside lifting buck plate respectively
Side to the right in the middle part of matching board, the third drawstring are equipped with 4, one end two-by-two respectively with interlocking at left and right sides of core plate break-make electric installation,
Wherein two other ends are respectively with the urgent trigger device interlocking of left and right sides link body, and in addition two other ends are respectively around upper
Second line wheel of lower both sides, the urgent trigger device interlocking of third line wheel, the 4th line wheel and upper and lower both sides link body.
Further, the linkage of unbuttoning includes the 4th drawstring, the 5th line wheel, the 6th line wheel, linkage line wheel assembly
Plate, the 5th drawstring, the second compressed spring, linkage assembly head, the linkage line wheel buck plate be equipped with 8 pieces, 2 pieces be one group, first
Group welding is in the middle part of upside lifting buck plate and left side, the second group welding lift buck plate middle part and upside, third group in right side
It is welded in the middle part of downside lifting buck plate and right side, the 4th group welding lifts buck plate middle part and downside, 8 pieces of connection in left side
Moving-wire wheel buck plate is inlayed towards middle part at parachute fitting groove is snapped with the 6th line wheel, and the linkage assembly head is equipped with 4,
One end, which is respectively perpendicular, is welded in back side middle part of 4 blocks of capping buckles towards parachute fitting groove, passes through the 5th in the middle part of the other end
The drawstring lifting connecting plate interlocking with 4 link bodies respectively, interlocking has one end of the 4th drawstring on the right side of the other end, and described the
Four drawstrings are equipped with 4, and the other end bypasses the 5th line wheel of 4 sides, the 6th line wheel and interlocking in the middle part of the linkage assembly head of adjacent side respectively,
Second compressed spring is equipped with 4, corresponds to and is socketed on the outside of linkage assembly head, inlays snapping with parachute assembly cylinder.
Further, the core plate break-make electric installation includes that third compressed spring, core plate energization head, core plate connect battery plate, core
Plate limiting plate, be powered assembly baffle, and the core plate limiting plate is concave shape, is glued the middle part on front side of rotor control core plate, groove
Forward, splicing is inlayed at left and right sides of groove has energization assembly baffle, the core plate to connect battery plate and be equipped with 2 pieces, controlled with rotor
Core plate, accumulator electrical connection, the core plate energization head are set in the groove of core plate limiting plate, and core plate limiting plate clearance fit,
With emergency stop pulling apparatus interlocking in the middle part of left and right ends, the third compressed spring is equipped with 2, one end respectively with core plate energization head
Left and right ends are glued, and the other end is powered with the left and right sides assembles baffle splicing respectively.
Advantageous effect
When a kind of floated aerial device of the present invention is taken photo by plane, the dress of parachute can be carried out in parachute fitting groove again
Match, after can be by wirelessly carrying out the operation of control device, device operation is in use, can pass through the rotor that a rotor assembles connecting rod
The screw wing of assembly head assembly carries out the lift-off neutral buoyancy of device, after can carry out photography of taking photo by plane by camera of taking photo by plane, and
Device goes up to the air in use, a screw wing that the speed probe that device is equipped with can assemble device rotor on connecting rod carries out rotation sense
It answers, when occurring failure in a screw wing that rotor assembles connecting rod, can be powered to the electromagnet of urgent trigger device,
So that electromagnet is drawn triggering lifting plate, so that triggering lifting plate is passed through the first drawstring and pull lifting connecting plate, lifting is made to connect
Plate pulls the second drawstring and third drawstring, the 5th drawstring, make the second drawstring pull warning energization head be moved to warning connect battery plate it
Between, to make attention device energization light, while third drawstring can pull core plate energization head and move to left or move to right, and keep core plate energization head de-
Off-chip plate connects battery plate, makes rotor control core plate power-off, the screw wing for keeping remaining lossless is also out of service, while the 5th drawstring can also
The capping buckle of respective side is pullled, and when there is any one side seal cover buckle plate to be pullled, linkage assembly head provided therewith can pass through
4th drawstring, which synchronizes, pulls remaining capping buckle, so that capping buckle is detached from the snapping to landing ejection lid, makes parachute fitting groove
The parachute of interior placement can be opened, and to steadily fall unbalance device out of control, so that user's use device is encountered device unbalance
When out of control, device can by equipped with spring, drawstring, the mechanism for connecing the compositions such as battery plate, make device it is unbalance it is out of control constantly from
It is dynamic to carry out the out of service of normal rotor, and parachute capping can be automatically terminated, so that the parachute of assembly is opened, makes dress
The landing of steady safety can be ensured when unbalance out of control by setting, and ensured the safe to use of device, be more convenient for using.
Description of the drawings
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other feature of the invention,
Objects and advantages will become more apparent upon：
Fig. 1 is a kind of structural schematic diagram of floated aerial device of the present invention.
Fig. 2 is the attachment structure schematic diagram that rotor of the present invention assembles connecting rod and main body of taking photo by plane.
Fig. 3 is the detailed attachment structure schematic diagram that rotor of the present invention assembles connecting rod and main body of taking photo by plane.
Fig. 4 is the structural schematic diagram of A in Fig. 3 of the present invention.
Fig. 5 is the structural schematic diagram of B in Fig. 3 of the present invention.
In figure：Screw wing -1, rotor motor -2, rotor assembly head -3, rotor assembly connecting rod -4, landing ejection lid -5, boat
Clap main body -6, landing supporting rack -7, camera -8 of taking photo by plane, speed probe -401, sensor Assembly rail -402, urgent triggering
Device -403, lifting connecting plate -404, failure warning device -405, link body -406, machine main body -601, accumulator -
602, parachute assembles cylinder -603, emergency stop pulling apparatus -604, unbuttons linkage -605, capping buckle -606, rotor control
Core plate -607, core plate break-make electric installation -608, parachute fitting groove -609, electromagnet -40301, electromagnet assembly head -40302,
First compressed spring -40303, triggering postive stop baffle -40304, triggering lifting plate -40305, the first drawstring -40306, attention device -
40501, extension spring -40502, warning energization head -40503, warning limiting plate -40504, warning connect battery plate -40505, warning
Pulley buck plate -40506, the first line wheel -40507, the second drawstring -40508, third drawstring -60401, the second line wheel -60402,
First line wheel buck plate -60403, third line wheel -60404, the 4th line wheel -60405, the second line wheel buck plate -60406, lifting
Buck plate -60407, the 4th drawstring -60501, the 5th line wheel -60502, the 6th line wheel -60503, linkage line wheel buck plate -
60504, the 5th drawstring -60505, the second compressed spring -60506, linkage assembly head -60507, third compressed spring -60801,
Core plate energization head -60802, core plate connect battery plate -60803, core plate limiting plate -60804, be powered assembly baffle -60805.
Specific implementation mode
To make the technical means, the creative features, the aims and the efficiencies achieved by the present invention be easy to understand, with reference to
Specific implementation mode, the present invention is further explained.
- Fig. 5 is please referred to Fig.1, the present invention provides a kind of floated aerial device technical solution：Its structure include screw wing 1,
Rotor motor 2, rotor assembly connecting rod 4, landing ejection lid 5, main body 6 of taking photo by plane, landing supporting rack 7, is taken photo by plane at rotor assembly head 3
Camera 8, the main body 6 of taking photo by plane are cross, and 4 jiaos of equal interlockings have 4 one end of rotor assembly connecting rod, bottom end interlocking to have landing branch
Support 7, top middle portion are snapped with landing ejection lid 5, and the 7 center bottom interlocking of landing supporting rack is taken photo by plane camera 8, described
Rotor assemble connecting rod 4 be equipped with 4, the other end is welded with rotor assembly head 3, respectively with rotor assembly head 3, main body 6 of taking photo by plane
Electrical connection, the rotor assembly head 3 are correspondingly provided with 4, and interlocking is run through at middle part rotor motor 2, is electrically connected with rotor motor 2
It connects, the rotor motor 2 is correspondingly provided with 4, and the equal interlocking in top has screw wing 1, and the rotor assembly connecting rod 4 includes revolution speed sensing
Device 401, sensor Assembly rail 402, urgent trigger device 403, lifting connecting plate 404, failure warning device 405, link body
406, the link body 406 is equipped with 4, and one end with 6 interlocking of main body of taking photo by plane, and passes through sensor in the middle part of, the other end
402 interlocking of Assembly rail has speed probe 401, the urgent trigger device 403 to be correspondingly provided with 4, and corresponding inlay is glued in even
401 side of speed probe is leaned in 406 inside of bar main body, is electrically connected with speed probe 401 through sensor Assembly rail 402,
It is electrically connected with main body 6 of taking photo by plane through link body 406, with lifting 404 one end interlocking of connecting plate, the failure warning device
405 are equipped with 8, are correspondingly arranged at 4 402 left and right sides of sensor Assembly rail, inlay interlocking with sensor Assembly rail 402,
Set on lifting connecting plate 404 both sides, with lifting 404 interlocking of connecting plate, 404 other end of lifting connecting plate and host of taking photo by plane
6 interlocking of body, the main body 6 of taking photo by plane include machine main body 601, accumulator 602, parachute assembly cylinder 603, emergency stop pulling apparatus
604, linkage 605, capping buckle 606, rotor control core plate 607, core plate break-make electric installation 608, parachute assembly are unbuttoned
Slot 609, the machine main body 601 are cross, 4 jiaos respectively with 4 406 interlockings of link body, middle part front side integral inlays
It is welded with parachute assembly cylinder 603, parachute assembly 603 integral middleization of cylinder is equipped with parachute fitting groove 609, the envelope
Cover buckle plate 606 is cylinder, is equipped with 4, is combined with each other into torus, inlays and is buckled in parachute assembly 603 inner front side of cylinder,
Be biased in the middle part of 609 direction side of parachute fitting groove with unbutton 605 interlocking of linkage, it is described unbutton linkage 605 with it is anxious
Stop the welding of pulling apparatus 604, be set to 604 top of emergency stop pulling apparatus, with lifting 404 interlocking of connecting plate, the emergency stop lifting dress
It sets 604 and is correspondingly provided with 4, respectively with 4 403 interlockings of urgent trigger device, inlay welding with machine main body 601, it is logical with core plate
608 left and right sides interlocking of breaker device, with lifting 404 interlocking of connecting plate, the core plate break-make electric installation 608 is glued in rotor control
607 rear side of coremaking plate is set to 609 rear side of parachute fitting groove, is electrically connected with accumulator 602 through rotor control core plate 607, institute
It states accumulator 602 and inlays splicing with machine main body 601, the urgent trigger device 403 includes electromagnet 40301, electromagnet dress
Plate 40305, the first drawstring 40306 are lifted with the first 40302, first compressed spring 40303, triggering postive stop baffle 40304, triggering,
Splicing is inlayed in 40301 left and right ends of the electromagnet with electromagnet assembly head 40302, and one end is electrically connected with speed probe 401
It connects, the electromagnet assembly head 40302 is integrated with link body 406, towards the landing ejection equal vertical welding in 5 side of lid
There are triggering postive stop baffle 40304, the triggering lifting plate to pass through the first compressed spring 40303 and electromagnet in the middle part of 40305 one end
40301 are glued, and pass through the first drawstring 40306 and lifting 404 interlocking of connecting plate, the failure warning device 405 in the middle part of the other end
Battery plate is connect including attention device 40501, extension spring 40502, warning energization head 40503, warning limiting plate 40504, warning
40505, warning pulley buck plate 40506, the first line wheel 40507, the second drawstring 40508, the attention device 40501 are equipped with 2,
Interlocking is inlayed respectively in 406 left and right sides of link body, and being vertically glued towards 406 upper and lower sides of link body has warning limiting plate
40504, there is warning energization head 40503 by the splicing of extension spring 40502 towards 406 middle part of link body, the warning connects
Battery plate 40505 is equipped with 4 pieces, is electrically connected with accumulator 602, and corresponding 2 pieces of warning limiting plates 40504 with the left and right sides are inlayed respectively
Embedding splicing is located at 2 pieces of warning limiting plates 40504 towards the close angle in 406 side of link body, the warning pulley buck plate 40506
Equipped with 2 pieces, it is glued respectively with 40504 rear side of left and right sides warning limiting plate, towards the equal snapping in 406 side of link body top front side
Have the first line wheel 40507, second drawstring 40508 is equipped with 2, one end correspond to respectively with the warning energization head of the left and right sides
40503 interlockings, the other end respectively with lifting 404 left and right sides interlocking of connecting plate, the emergency stop pulling apparatus 604 include third drawing
The 60401, second line wheel 60402 of rope, the first line wheel buck plate 60403, third line wheel 60404, the 4th line wheel 60405, the second line
Buck plate 60406, lifting buck plate 60407 are taken turns, the lifting buck plate 60407 is equipped with 4 pieces, and correspondence is welded in body master respectively
4 jiaos of the inside of body 601, it is orthogonal each other, towards parachute fitting groove 609 at be vertically welded with the first line wheel buck plate
60403, third line wheel 60404 is snapped with by the first line wheel buck plate 60403, the second line wheel buck plate 60406 is set
There are 2 pieces, welded with lifting buck plate 60407, is respectively arranged on and lifts the upper left corner and the lower right corner that buck plate 60407 is formed, 2 pieces
It is inlayed at towards parachute fitting groove 609 and is snapped with the 4th line wheel 60405, second line wheel 60402 is equipped with 2, respectively
It inlays and is buckled in 60407 middle part side to the right of upside lifting buck plate 60407 middle part side to the left and downside lifting buck plate, described the
Three drawstrings 60401 be equipped with 4, one end two-by-two respectively with 608 left and right sides interlocking of core plate break-make electric installation, wherein two other ends
Respectively with 403 interlocking of urgent trigger device of left and right sides link body 406, in addition two other ends are respectively around upper and lower both sides
The urgent trigger device of second line wheel 60402, third line wheel 60404, the 4th line wheel 60405 and upper and lower both sides link body 406
403 interlockings, the linkage 605 of unbuttoning includes the 4th drawstring 60501, the 5th line wheel 60502, the 6th line wheel 60503, linkage
Line wheel buck plate 60504, the 5th drawstring 60505, the second compressed spring 60506, linkage assembly head 60507, the linkage line wheel
Buck plate 60504 is equipped with 8 pieces, and 2 pieces are one group, and the first group welding is in upside lifting buck plate 60407 middle part and left side, second group
It is welded in 60407 middle part of right side lifting buck plate and upside, third group welding is in the middle part of downside lifting buck plate 60407 and right
Side, the 4th group welding is in left side lifting buck plate 60407 middle part and downside, and 8 pieces of linkage line wheels buck plate 60504 is towards drop
It falls in the middle part of at umbrella fitting groove 609 to inlay and is snapped with the 6th line wheel 60503, the linkage assembly head 60507 is equipped with 4, one end
It is respectively perpendicular and is welded in 4 blocks of capping buckles 606 towards in the middle part of the back side of parachute fitting groove 609, by the in the middle part of the other end
404 interlocking of lifting connecting plate with 4 link bodies 406, other end right side interlocking have the 4th drawstring to five drawstrings 60505 respectively
60501 one end, the 4th drawstring 60501 are equipped with 4, and the other end bypasses the 5th line wheel 60502, the 6th line of 4 sides respectively
The 60507 middle part interlocking of linkage assembly head of wheel 60503 and adjacent side, second compressed spring 60506 are equipped with 4, corresponding socket
In 60507 outside of linkage assembly head, snapping is inlayed with parachute assembly cylinder 603, the core plate break-make electric installation 608 includes third
Compressed spring 60801, core plate energization head 60802, core plate connect battery plate 60803, core plate limiting plate 60804, be powered assembly baffle
60805, the core plate limiting plate 60804 is concave shape, is glued in 607 front side middle part of rotor control core plate, groove is facing forward, groove
Splicing is inlayed in the left and right sides has energization assembly baffle 60805, the core plate to connect battery plate 60803 and be equipped with 2 pieces, controlled with rotor
Core plate 607, accumulator 602 are electrically connected, and the core plate energization head 60802 is set in the groove of core plate limiting plate 60804, with core plate
60804 clearance fit of limiting plate, in the middle part of left and right ends with 604 interlocking of emergency stop pulling apparatus, the third compressed spring 60801
Equipped with 2, one end is glued with 60802 left and right ends of core plate energization head respectively, and the other end is powered with the left and right sides assembles gear respectively
Plate 60805 is glued.
User can carry out the assembly of parachute in parachute fitting groove 609 again when taking photo by plane by the present apparatus, after energy
Enough operations by wirelessly carrying out control device, device operation is in use, the rotor that can assemble connecting rod 4 by 4 rotors assembles
The screw wings 1 of first 3 assembly carry out the lift-off neutral buoyancy of devices, after can carry out photography of taking photo by plane by camera 8 of taking photo by plane, and filling
Lift-off is set in use, the speed probe 401 that device is equipped with can assemble device rotor 1 turn of 4 screw wings of connecting rod 4
Innervation is answered, can be to the electromagnetism of urgent trigger device 403 when occurring failure in 4 screw wings 1 that rotor assembles connecting rod 4
Iron 40301 is powered, and so that electromagnet 40301 is drawn triggering lifting plate 40305, makes triggering lifting plate 40305 by the
One drawstring 40306 pulls lifting connecting plate 404, make lifting connecting plate 404 pull the second drawstring 40508 and third drawstring 60401,
5th drawstring 60505 makes the second drawstring 40508 pull warning energization head 40503 and is moved between warning connects battery plate 40505, from
And the energization of attention device 40501 is made to light, while third drawstring 60401 can pull core plate energization head 60802 and move to left or move to right, and make core
Plate energization head 60802 is detached from core plate and connects battery plate 60803, so that rotor control core plate 607 is powered off, makes remaining lossless screw wing 1
It is out of service, while the 5th drawstring 60505 can also pull the capping buckle 606 of respective side, and having any one side seal cover buckle plate
606 when being pullled, and linkage assembly head 60507 provided therewith can be synchronized by the 4th drawstring 60501 pulls remaining capping buckle
606, so that capping buckle 606 is detached from the snapping to landing ejection lid 5, enables the parachute placed in parachute fitting groove 609
It opens, to steadily fall unbalance device out of control.
Problems solved by the invention is the prior art in use, the easy damage because of device aviation mechanism, leads to device
It is unbalance out of control and fall, lead to the damage that falls of device, cause dangerous and inconvenient, the present invention pass through above-mentioned component mutual group
Close, make user's use device encounter device it is unbalance out of control when, device can by equipped with spring, drawstring, connect the compositions such as battery plate
Mechanism, make device in the out of service of the unbalance constantly automatic normal rotor of carry out out of control, and can automatically terminate parachute envelope
Lid, enables the parachute of assembly to open, and enables devices to the landing for ensureing steady safety when unbalance out of control, ensures device
It is safe to use, it is more convenient for using.
The above shows and describes the basic principles and main features of the present invention and the advantages of the present invention, for this field skill
For art personnel, it is clear that invention is not limited to the details of the above exemplary embodiments, 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, in all respects, should all incite somebody to action
Embodiment regards exemplary as, and is non-limiting, the scope of the present invention by appended claims rather than on state
Bright restriction, it is intended that including all changes that come within the meaning and range of equivalency of the claims in the present invention
It is interior.Any reference signs in the claims should not be construed as limiting the involved claims.
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 embodiment being appreciated that.
Claims (6)
1. a kind of floated aerial device, structure includes screw wing (1), rotor motor (2), rotor assembly head (3), rotor dress
With connecting rod (4), landing ejection lid (5), main body of taking photo by plane (6), landing supporting rack (7), camera of taking photo by plane (8), the master that takes photo by plane
Body (6) is cross, and 4 jiaos of equal interlockings have rotor to assemble connecting rod (4) one end, and bottom end interlocking has a landing supporting rack (7), in top
Portion is snapped with landing ejection lid (5), it is characterised in that：
Landing supporting rack (7) the center bottom interlocking is taken photo by plane camera (8), and the rotor assembly connecting rod (4) is equipped with 4,
The other end is welded with rotor assembly head (3), is electrically connected respectively with rotor assembly head (3), main body of taking photo by plane (6), the rotor
Assembly head (3) is correspondingly provided with 4, and interlocking is run through at middle part rotor motor (2), is electrically connected with rotor motor (2), the rotor
Motor (2) is correspondingly provided with 4, and the equal interlocking in top has screw wing (1)；
The rotor assembly connecting rod (4) includes speed probe (401), sensor Assembly rail (402), urgent trigger device
(403), lifting connecting plate (404), failure warning device (405), link body (406), the link body (406) are equipped with 4
A, with main body of taking photo by plane (6) interlocking, and there is rotating speed biography in one end in the middle part of, the other end by sensor Assembly rail (402) interlocking
Sensor (401), the urgent trigger device (403) are correspondingly provided with 4, correspond to inlay to be glued and be leaned on inside link body (406)
Speed probe (401) side is electrically connected through sensor Assembly rail (402) with speed probe (401), runs through connecting rod master
Body (406) is electrically connected with main body of taking photo by plane (6), with lifting connecting plate (404) one end interlocking, the failure warning device (405)
Equipped with 8, it is correspondingly arranged at left and right sides of 4 sensor Assembly rails (402), inlays interlocking with sensor Assembly rail (402),
Set on lifting connecting plate (404) both sides, with lifting connecting plate (404) interlocking, lifting connecting plate (404) other end with navigate
Main body (6) interlocking is clapped, the main body of taking photo by plane (6) includes machine main body (601), accumulator (602), parachute assembly cylinder
(603), emergency stop pulling apparatus (604), unbutton linkage (605), capping buckle (606), rotor control core plate (607), core
Plate break-make electric installation (608), parachute fitting groove (609), the machine main body (601) be cross, 4 jiaos respectively with 4 companies
Bar main body (406) interlocking, middle part front side integral, which is inlayed, is welded with parachute assembly cylinder (603), and the parachute assembles cylinder
(603) integral middleization is equipped with parachute fitting groove (609), and the capping buckle (606) is cylinder, is equipped with 4, mutual group
Torus is synthesized, inlays and is buckled in parachute assembly cylinder (603) inner front side, be biased in parachute fitting groove (609) direction side
Portion with unbutton linkage (605) interlocking, the linkage (605) of unbuttoning is welded with emergency stop pulling apparatus (604), is set to
Above emergency stop pulling apparatus (604), with lifting connecting plate (404) interlocking, the emergency stop pulling apparatus (604) is correspondingly provided with 4,
Respectively with 4 urgent trigger device (403) interlockings, welding is inlayed with machine main body (601), with core plate break-make electric installation (608)
Left and right sides interlocking, with lifting connecting plate (404) interlocking, the core plate break-make electric installation (608) is glued controls core plate in rotor
(607) rear side is set on rear side of parachute fitting groove (609), is electrically connected with accumulator (602) through rotor control core plate (607),
The accumulator (602) inlays splicing with machine main body (601).
2. a kind of floated aerial device according to claim 1, it is characterised in that：The urgent trigger device (403)
Including electromagnet (40301), electromagnet assembly head (40302), the first compressed spring (40303), triggering postive stop baffle
(40304), triggering lifting plate (40305), the first drawstring (40306), electromagnet (40301) left and right ends are and electromagnet
Assembly head (40302) inlays splicing, and one end is electrically connected with speed probe (401), the electromagnet assembly head (40302) and company
Bar main body (406) is integrated, and triggering postive stop baffle (40304), institute are vertically welded with towards landing ejection lid (5) side
It states and is glued by the first compressed spring (40303) and electromagnet (40301) in the middle part of triggering lifting plate (40305) one end, the other end
Middle part passes through the first drawstring (40306) and lifting connecting plate (404) interlocking.
3. a kind of floated aerial device according to claim 1, it is characterised in that：The failure warning device (405)
It is connect including attention device (40501), extension spring (40502), warning energization head (40503), warning limiting plate (40504), warning
Battery plate (40505), warning pulley buck plate (40506), the first line wheel (40507), the second drawstring (40508), the attention device
(40501) 2 are equipped with, inlays interlocking respectively at left and right sides of link body (406), it is equal towards link body (406) upper and lower sides
Vertical splicing has warning limiting plate (40504), has towards link body (406) middle part by extension spring (40502) splicing
Energization head (40503), the warning is warned to connect battery plate (40505) and be equipped with 4 pieces, be electrically connected with accumulator (602), correspond to respectively
Splicing is inlayed with 2 pieces of warning limiting plates (40504) of the left and right sides, is located at 2 pieces of warning limiting plates (40504) towards link body
(406) the close angle in side, the warning pulley buck plate (40506) are equipped with 2 pieces, warn limiting plate with the left and right sides respectively
(40504) rear side is glued, and is snapped with the first line wheel (40507) towards link body (406) side top front side, described second draws
Restrict (40508) be equipped with 2, one end correspond to respectively with warning energization head (40503) interlocking of the left and right sides, the other end respectively with carry
Draw interlocking at left and right sides of connecting plate (404).
4. a kind of floated aerial device according to claim 1, it is characterised in that：The emergency stop pulling apparatus (604)
Including third drawstring (60401), the second line wheel (60402), the first line wheel buck plate (60403), third line wheel (60404),
Four line wheels (60405), the second line wheel buck plate (60406), lifting buck plate (60407), the lifting buck plate (60407) set
There are 4 pieces, the corresponding machine main body (601) that is welded in is 4 jiaos internal respectively, orthogonal each other, towards parachute fitting groove (609)
Place is vertically welded with the first line wheel buck plate (60403), and third line wheel is snapped with by the first line wheel buck plate (60403)
(60404), the second line wheel buck plate (60406) is equipped with 2 pieces, is welded with lifting buck plate (60407), is respectively arranged on and carries
Load the upper left corner and the lower right corner of matching board (60407) formation, 2 pieces are snapped with the towards inlaying at parachute fitting groove (609)
Four line wheels (60405), second line wheel (60402) are equipped with 2, inlay be buckled in upside lifting buck plate (60407) respectively
Side to the right in the middle part of middle part side to the left and downside lifting buck plate (60407), the third drawstring (60401) are equipped with 4, one end two
Two respectively with core plate break-make electric installation (608) at left and right sides of interlocking, wherein two other ends respectively with left and right sides link body
(406) urgent trigger device (403) interlocking, in addition two other ends respectively bypass upper and lower both sides the second line wheel (60402),
Third line wheel (60404), the 4th line wheel (60405) and the urgent trigger device (403) of upper and lower both sides link body (406) are locked
It connects.
5. a kind of floated aerial device according to claim 1 or 4, it is characterised in that：It is described to unbutton linkage
(605) include the 4th drawstring (60501), the 5th line wheel (60502), the 6th line wheel (60503), linkage line wheel buck plate
(60504), the 5th drawstring (60505), the second compressed spring (60506), linkage assembly head (60507), the linkage line wheel dress
Matching board (60504) is equipped with 8 pieces, and 2 pieces are one group, and the first group welding is in the middle part of upside lifting buck plate (60407) and left side, and second
Group welding is lifted in downside in the middle part of buck plate (60407) in the middle part of right side lifting buck plate (60407) with upside, third group welding
And right side, the 4th group welding is in left side lifting buck plate (60407) middle part and downside, 8 pieces of linkages line wheel buck plates
(60504) it is inlayed towards middle part at parachute fitting groove (609) and is snapped with the 6th line wheel (60503), the linkage assembly head
(60507) 4 are equipped with, one end, which is respectively perpendicular, is welded in back side of 4 pieces of capping buckles (606) towards parachute fitting groove (609)
Middle part, other end middle part are locked with the lifting connecting plate (404) of 4 link bodies (406) by the 5th drawstring (60505) respectively
It connects, interlocking has one end of the 4th drawstring (60501), the 4th drawstring (60501) to be equipped with 4 on the right side of the other end, the other end
It bypasses and is locked in the middle part of the 5th line wheel (60502), the 6th line wheel (60503) and the linkage assembly head (60507) of adjacent side of 4 sides respectively
It connects, second compressed spring (60506) is equipped with 4, corresponds to and is socketed on the outside of linkage assembly head (60507), is filled with parachute
Snapping is inlayed with cylinder (603).
6. a kind of floated aerial device according to claim 1, it is characterised in that：The core plate break-make electric installation
(608) include that third compressed spring (60801), core plate energization head (60802), core plate connect battery plate (60803), core plate limiting plate
(60804), be powered assembly baffle (60805), and the core plate limiting plate (60804) is concave shape, is glued and controls core plate in rotor
(607) front side middle part, groove is facing forward, and splicing is inlayed at left and right sides of groove has energization assembly baffle (60805), the core plate to connect
Battery plate (60803) is equipped with 2 pieces, is electrically connected with rotor control core plate (607), accumulator (602), the core plate energization head
(60802) it is set in the groove of core plate limiting plate (60804), with core plate limiting plate (60804) clearance fit, left and right ends middle part
With emergency stop pulling apparatus (604) interlocking, the third compressed spring (60801) be equipped with 2, one end respectively with core plate energization head
(60802) left and right ends are glued, and the other end is powered with the left and right sides assembles baffle (60805) splicing respectively.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810085532.8A CN108382585A (en) | 2018-01-29 | 2018-01-29 | A kind of floated aerial device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810085532.8A CN108382585A (en) | 2018-01-29 | 2018-01-29 | A kind of floated aerial device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108382585A true CN108382585A (en) | 2018-08-10 |
Family
ID=63074037
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810085532.8A Pending CN108382585A (en) | 2018-01-29 | 2018-01-29 | A kind of floated aerial device |
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| Country | Link |
|---|---|
| CN (1) | CN108382585A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2752037C1 (en) * | 2021-02-01 | 2021-07-22 | Федеральное государственное бюджетное научное учреждение "Федеральный научный агроинженерный центр ВИМ" (ФГБНУ ФНАЦ ВИМ) | Unmanned aerial vehicle gimbal for multispectral camera |
| RU2783091C1 (en) * | 2022-04-11 | 2022-11-08 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Петрозаводский государственный университет" | Suspension of the multispectral camera to the drone |
-
2018
- 2018-01-29 CN CN201810085532.8A patent/CN108382585A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| RU2752037C1 (en) * | 2021-02-01 | 2021-07-22 | Федеральное государственное бюджетное научное учреждение "Федеральный научный агроинженерный центр ВИМ" (ФГБНУ ФНАЦ ВИМ) | Unmanned aerial vehicle gimbal for multispectral camera |
| RU2783091C1 (en) * | 2022-04-11 | 2022-11-08 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Петрозаводский государственный университет" | Suspension of the multispectral camera to the drone |
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Application publication date: 20180810 |
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