CN109436343A - Unmanned plane - Google Patents
Unmanned plane Download PDFInfo
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- CN109436343A CN109436343A CN201811568284.9A CN201811568284A CN109436343A CN 109436343 A CN109436343 A CN 109436343A CN 201811568284 A CN201811568284 A CN 201811568284A CN 109436343 A CN109436343 A CN 109436343A
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- unmanned plane
- folded piece
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/62—Deployment
- B64D17/72—Deployment by explosive or inflatable means
-
- 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
- B64D17/00—Parachutes
- B64D17/80—Parachutes in association with aircraft, e.g. for braking thereof
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
- Toys (AREA)
Abstract
The present invention relates to aircraft fields, more particularly, to a kind of unmanned plane, including gas release device, San Tong mechanism and support frame；Gas release device is installed in San Tong mechanism, and San Tong mechanism is installed on support frame as described above；Gas release device includes trigger mechanism, striker relieving mechanism and storage cylinder；Striker relieving mechanism includes hollow mounting cylinder, the firing pin assembly in mounting cylinder and trigger member, limit body is arranged in mounting cylinder one end, trigger member is limited between limit body and the shock end of firing pin assembly, trigger member can drive firing pin assembly to move in mounting cylinder, also, mounting cylinder is connected to cylinder；Support frame as described above has multiple lightening holes；The present invention can be improved parachute pop-up distance, and improve the ejection success rate of parachute, and the multiple lightening holes being arranged on support frame can mitigate unmanned plane weight, can be with the flight safety of effective guarantee unmanned plane in conjunction with gas release device and San Tong mechanism.
Description
Technical field
The present invention relates to vehicle technology fields, more particularly, to a kind of unmanned plane.
Background technique
It when preventing unmanned plane is out of control from falling, is easy to cause and injures by a crashing object by increasing parachute assembly in the unmanned plane having at present
Or the case where smashing pedestrian and other facilities and unmanned plane is caused to be broken into pieces；Wherein, parachute assembly mainly uses bullet
The mode of spring ejection pops up parachute,
But in use, often there is causing due to spring force deficiency the parachute distance of parachute ejection failure or pop-up not
Enough situations, in addition, it is also to cause the certain reason out of control fallen that unmanned plane weight is larger, it is also to have very much for unmanned plane loss of weight
It is necessary.
Summary of the invention
The purpose of the present invention is to provide a kind of unmanned planes, existing in the prior art due to spring force deficiency to solve
Lead to the technical problem that the parachute distance of parachute ejection failure or pop-up is inadequate and unmanned plane weight is larger.
The present invention provides a kind of unmanned planes, including gas release device, San Tong mechanism and support frame；The gas release
Device is installed in the San Tong mechanism, and the San Tong mechanism is installed on support frame as described above；
The San Tong mechanism includes cylinder, clamping cap and cover；The clamping cap is installed on the cylinder of one end of the cylinder
Intracavitary, the cover is installed on the tube port position of one end of the cylinder；
The gas release device includes trigger mechanism, striker relieving mechanism and storage cylinder；The striker relieving mechanism,
Including hollow mounting cylinder, the firing pin assembly in the mounting cylinder and trigger member, mounting cylinder one end setting limit
Body, the trigger member are limited between the limit body and the shock end of the firing pin assembly, and the trigger member can drive
The firing pin assembly moves in the mounting cylinder；The bottleneck end of the storage cylinder is connected to the mounting cylinder far from the limit
One end of body, the bottleneck rectify the shock end to the firing pin assembly；, also, the mounting cylinder is connected to the cylinder；
The trigger mechanism is located at striker relieving mechanism side；It is described when the trigger member is in off working state
Firing pin assembly extend out to outside the mounting cylinder far from the joint end for hitting end and is clamped with the trigger mechanism；
When the trigger member is in running order, the firing pin assembly is made to hit the bottleneck end, while the joint end
It is detached from the trigger mechanism；
Support frame as described above includes first support, second support, connector and pipe clamp；
By multiple connectors connections between the first support and the second support, the first support and/
Or multiple lightening holes are set in the second support.
Further, the firing pin assembly includes striker ontology, needle stand and shank；The striker ontology and the needle stand
One end connection, the shank connect with the other end of the needle stand.
Further, there is axially disposed air passage in the striker ontology and be radially connected to the air passage
Airtube, the air passage run through the striker ontology needle point.
Further, the trigger mechanism includes driving device, linkage and shackle member；
The driving device drives the shackle member mobile by linkage, makes the shackle member and the firing pin assembly
The joint end connection or be detached from.
Further, the San Tong mechanism further includes pedestal, and the pedestal is installed on the barrel chamber of the other end of the cylinder
It is interior；The pedestal is used to support the trigger mechanism, the striker relieving mechanism and the storage cylinder.
Further, the linkage includes swinging rod piece, and the swing rod piece is hinged on the pedestal by shaft
On, to contact the driving device, the other end is hinged by shaft and the shackle member for described swing rod piece one end.
Further, guide groove is set in the shackle member, shackle member of the mounting cylinder close to the firing pin assembly
Positioning pin is arranged in side, and the positioning pin and the guide groove cooperate, so that radial direction of the shackle member along the firing pin assembly
It is mobile.
Further, the clamping cap includes being sequentially connected the boss portion connect, interconnecting piece and compressed part；The compressed part is leaned on
The other end of the nearly cylinder, the other end of the boss portion far from the cylinder；The barrel of the interconnecting piece and the cylinder
It is in contact；
Further, including pipe clamp, horn and foldable assembly, multiple pipe clamps are arranged in first support and described second
Between bracket；The horn includes fixed arm and folds arm, and described fixed arm one end connects the pipe clamp, and the fixed arm is another
End is connect by the foldable assembly with the folding arm.
Further, the foldable assembly includes the first folded piece, the second folded piece, fastener and the first washer；
First folded piece is socketed on the fixed arm, and second folded piece is socketed on the folding arm；
First folded piece is connect by rotating mechanism with second folded piece, is provided on first folded piece
First limiting section；
First washer is socketed on first folded piece, also, first washer is supported in first limit
Position portion has elasticity close to the side of second folded piece, first washer；
The fastener can be socketed on first folded piece and second folded piece, also, the fastener
Port can support in side of first washer far from first limiting section.
Further, the foldable assembly includes second packing ring；
Cricoid second limiting section is provided on second folded piece；
The second packing ring is socketed on second folded piece, also, the second packing ring is supported in second limit
Side of the position portion far from first folded piece.
Further, including battery holding mechanism, the battery holding mechanism include fixed plate, lock-screw and battery
Mounting plate；
The fixed plate is connect with the second support far from the side of first support；
The battery mounting plate is detachably connected by lock-screw and the fixed plate.
Further, clamping groove, the quantity pair of the clamping groove and the lock-screw are set on the battery mounting plate
It answers, also, the clamping groove includes larger diameter end and smaller diameter end, the head diameter of the screw is less than the larger diameter end
Diameter, greater than the diameter of smaller diameter end.
Further, including locked mechanism, the locked mechanism include the mounting groove being arranged in the second support, with
The elastic plate that side connects in the mounting groove, and the trigger member being connect with the elastic plate；The trigger member be provided with according to
The secondary hook across the elastic plate, the fixed plate and the battery mounting plate, the hook being capable of the peaces of battery described in hook joint
Loading board.
Further, including delivery storehouse, the delivery storehouse are connected with support frame as described above, and the delivery storehouse is for transporting goods
The material of object, the delivery storehouse is flexible material or elastic material.
Further, the delivery storehouse includes connecting rope and delivery storehouse main body, and the delivery storehouse main body is located at the support
One end of the lower section of frame, the connecting rope is connect with support frame as described above, the other end of the connecting rope and delivery storehouse main body
It is connected.
Further, including foot prop, camera assembly and first connecting rod；
The foot prop is arranged in support frame as described above two sides, and the camera assembly is fixed on the foot prop by first connecting rod
On, also, the camera assembly is located at below the delivery storehouse.
Compared with prior art, the invention has the benefit that
Unmanned plane provided by the invention, popping up parachute using compressed gas, mentioning in the way of triggering storage cylinder
High parachute pops up distance, and improves the ejection success rate of parachute；In addition, can avoid the prior art using compressed gas
In spring aging, the problem of caused elastic force declines ensures that parachute pop-up apart from unaffected, and trigger mechanism, is hit
Needle relieving mechanism and storage cylinder are used in combination, and reduce assembly difficulty, convenient for manipulation.Meanwhile what is be arranged on support frame multiple subtracts
Repeated hole can mitigate unmanned plane weight, in conjunction with gas release device and San Tong mechanism, can be pacified with the flight of effective guarantee unmanned plane
Entirely.
Detailed description of the invention
It, below will be to specific in order to illustrate more clearly of the specific embodiment of the invention or technical solution in the prior art
Embodiment or attached drawing needed to be used in the description of the prior art are briefly described.
Fig. 1 is the installation diagram of San Tong mechanism provided in an embodiment of the present invention；
Fig. 2 is the schematic diagram at another visual angle of San Tong mechanism provided in an embodiment of the present invention；
Fig. 3 is the explosive view of San Tong mechanism provided in an embodiment of the present invention；
Fig. 4 is the structural schematic diagram of clamping cap provided in an embodiment of the present invention；
Fig. 5 is the cross-sectional view in Fig. 4 along line A-A；
Fig. 6 is the schematic diagram of tube stent provided in an embodiment of the present invention；
Fig. 7 is the partial sectional view of San Tong mechanism provided in an embodiment of the present invention；
Fig. 8 is the partial enlargement diagram in Fig. 7 at B；
Fig. 9 is the structural schematic diagram of gas release device provided in an embodiment of the present invention；
Figure 10 is the explosive view of gas release device provided in an embodiment of the present invention；
Figure 11 is cuing open after the striker relieving mechanism gas storage cylinder in gas release device provided in an embodiment of the present invention is matched
View；
Figure 12 is the structural representation at bottleneck end and striker body contacts in gas release device provided in an embodiment of the present invention
Figure；
Figure 13 is the perspective view of parachute catapult-launching gear provided in an embodiment of the present invention；
Figure 14 is the schematic diagram after striker relieving mechanism provided in an embodiment of the present invention is matched with gas storage cylinder；
Figure 15 is the first structural schematic diagram of support frame provided in an embodiment of the present invention；
Figure 16 is second of structural schematic diagram of support frame provided in an embodiment of the present invention；
Figure 17 is the structural schematic diagram at another visual angle in support frame shown in Figure 16；
Figure 18 is the structural schematic diagram of battery mounting plate in support frame shown in Figure 16；
Figure 19 is the structural schematic diagram of trigger member in support frame shown in Figure 16；
Figure 20 is the structural schematic diagram under the first visual angle of foldable assembly provided in an embodiment of the present invention；
Figure 21 is the cross-sectional view under the first visual angle of foldable assembly provided in an embodiment of the present invention；
Figure 22 is the enlarged drawing in Figure 21 at C；
Figure 23 is structural schematic diagram of the foldable assembly provided in an embodiment of the present invention under the second visual angle；
Figure 24 is the enlarged drawing in Figure 23 at D；
Figure 25 is the structural schematic diagram of unmanned plane provided in an embodiment of the present invention；
Figure 26 is the enlarged diagram in Figure 25 at E.
Icon: 100- trigger mechanism, 110- driving device, 111- pushing block, 120- shackle member, 121- guide groove, 122-
Positioning pin, 130- swing rod piece, 200- striker relieving mechanism, 210- mounting cylinder, 211- limit body, 212- flow-guiding channel, 213-
Connector sleeve, 220- firing pin assembly, 221- striker ontology, 222- needle stand, 223- shank, 224- air passage, 225- airtube, 226-
First card slot, the second card slot of 227-, 230- trigger member, 240- sealing ring, 300- storage cylinder, 310- bottleneck end, 400- support frame,
401- first support, 402- second support, 403- connector, 404- pipe clamp, 405- lightening hole, 406- fixed plate, 407- locking
Screw, 408- battery mounting plate, 409- clamping groove, 410- larger diameter end, 411- smaller diameter end, 412- nut, 413- mounting groove,
414- elastic plate, 415- trigger member, 416- hook, 417- limiting slot, the press section 418-, 419- weight loss groove, 500- elastic reset
Part, 600- San Tong mechanism, 601- cylinder；602- cover, 604- boss portion, 605- interconnecting piece, 606- compressed part, 607- pedestal,
608- flap, 609- enclosing, 610- clamping cap, 611- tube stent, 612- through-hole, 613- gap, 614- bracket mounting post, 615-
Air inlet, the first folded piece of 700-, the first limiting section of 701-, the second folded piece of 702-, the second limiting section of 703-, 704- fastening
Part, 705- protrusion, the first washer of 706-, 707- first lug, the second lug of 708-, 709- bolt, 710- second packing ring,
711- fixed arm, 712- fold arm, and 802- delivers storehouse, 803- camera assembly, 804- foot prop, 805- first connecting rod, 806- company
Splicing, 807- deliver storehouse main body, 808- link, 809- hook.
Specific embodiment
Technical solution of the present invention is clearly and completely described below in conjunction with attached drawing.
As shown in Figure 25, Figure 13 and Figure 14, the embodiment of the invention provides a kind of unmanned plane, which includes that gas is released
Put device, San Tong mechanism 600 and support frame 400；Gas release device is installed in San Tong mechanism 600, and San Tong mechanism 600 is installed
On support frame 400.
Referring to shown in Fig. 1 to Fig. 8, the San Tong mechanism 600 in the embodiment includes cylinder 601, clamping cap 610 and cover
602；Cylinder 601 is tiltedly mounted on support frame 400, and clamping cap 610 is installed in the barrel chamber of one end of cylinder 601, cover 602
It is installed on the tube port position of one end of cylinder 601；Clamping cap 610 includes being sequentially connected the boss portion 604 connect, interconnecting piece 605 and pressure
Tight portion 606；The other end of the compressed part 606 close to cylinder 601, the other end of the boss portion 604 far from cylinder 601；Interconnecting piece 605 with
The barrel of cylinder 601 is in contact.
Specifically, cylinder 601 is circular cylinder；The both ends open of cylinder 601, such one end are easily installed clamping cap
610 and cover 602.Clamping cap 610 can be connected by interconnecting piece 605 with barrel.In use, parachute is installed on cylinder
601 inside.The compressed part 606 of the perpendicular lid of pressure can be in contact with parachute.Boss portion 604, interconnecting piece 605 and compressed part 606
It can be structure as a whole.
The San Tong mechanism 600 that the embodiment provides, by using clamping cap 610 and cover 602 together be mounted on cylinder
After design on 601, when the vibration that generates in unmanned plane during flying can gradually shake clamping cap 610 pine, and boss portion 604 can will
Canopy top deforms or falls, so that the internal state of cylinder 601 can be examined from appearance, and at this time clamping cap 610 still in umbrella
In cylinder, parachute can't be fallen extremely in several flight cycles, be skidded off so as to avoid the parachute in cylinder due to abnormal
It is caused to twine paddle problem, it ensure that the flight safety of unmanned plane.
In the optional scheme of the embodiment, it is connected by way of interference fit between interconnecting piece 605 and cylinder 601,
That is, being interference fitted between interconnecting piece 605 and the inner tube wall of cylinder 601, clamping cap 610 and cylinder both may be implemented in this way
It is connected between 601, it on the other hand can also can be convenient for by discharging high pressure gas into cylinder 601, by clamping cap 610 from cylinder
One end of body 601 is gone out, so that parachute be made to open.
Compressed part 606 is round-like structure, and maximum one end of diameter of round-like structure is connected with interconnecting piece 605.
In this way, the diameter of the smallest one end of the diameter of round-like structure is not more than the internal diameter of cylinder 601, it is convenient for 610 energy of clamping cap in this way
Enough smoothly insertion cylinders 601.
Gap setting between boss portion 604 and the barrel of cylinder 601, the vibration of the unmanned plane in this way in flight course
In the case of, boss portion 604 can push up canopy outward or make its deformation.Boss portion 604 is annular structure.Be conducive in this way to umbrella
The uniform force application of lid.Specifically, the outer diameter of annular structure is not more than the internal diameter of cylinder 601, optionally, annular structure
Outer diameter is less than the internal diameter of cylinder 601.It should be noted that boss portion 604 can also be column structure, when for column structure
When, the internal diameter of column structure is less than the internal diameter of cylinder 601.
The material of canopy can be with elastic rubber, or silica gel is matched between canopy and the outer wall of cylinder 601 by interference
The mode of conjunction is connected, in this way convenient for by discharging high pressure gas into cylinder 601, canopy is gone out from one end of cylinder 601,
To make parachute open.Canopy, which is done, using silica gel or elastic rubber is conducive to anti-light photograph and low temperature aging.
The material of clamping cap 610 is foam, silica gel or sponge.Between the outer circle of interconnecting piece 605 and the inner tube wall of cylinder 601
Interference fit is squeezed inside cylinder 601 by the deformation of clamping cap 610, can be compressed parachute and is compacted and prevent vibration from falling off, make
It is more advantageous to gas with the clamping cap 610 of foam, silica gel or sponge material disposably to spray, to improve spray distance.
In the optional scheme of the embodiment, San Tong mechanism further includes pedestal 607, and pedestal 607 is installed on the another of cylinder 601
In the barrel chamber at end, other components are easily installed by the way that pedestal 607 is arranged.Specifically, pedestal 607 includes flap 608 with fixation
Enclosing 609 around seat bottom, enclosing 609 are structure as a whole with flap 608.Enclosing 609 is inserted into the other end of cylinder 601
In barrel chamber；It is bolted to connection between enclosing 609 and the barrel of cylinder 601.The centre of flap offers air inlet 615,
High pressure gas for the release of supplied gas release device enters in cylinder from air inlet, and parachute is gone out out of cylinder.Cylinder
On the barrel of the other end of body 601, tool is easily installed in this way there are two the gap 613 being oppositely arranged in other components, such as:
One of gap 613 is used to concede installation site to the storage cylinder of installation, another gap 613 is used to discharge to gas and fill
The shank for the striker relieving mechanism set is by out position.
In the optional scheme of the embodiment, San Tong mechanism further includes tube stent 611, tube stent 611 and the fixed company of pedestal 607
It connects.Tube stent 611 is triangular structure of right angle, which includes three and end to end surround enclosed construction
Connecting rod；Pedestal 607 is fixedly connected with the longest edge (i.e. the longest connecting rod of length) of triangular structure of right angle, in this way when umbrella cylinder
When mechanism 600 is installed on the support frame 400 of unmanned plane, San Tong mechanism 600 can be inclined to set with horizontal direction, in order to
Parachute ejects outward, and the San Tong mechanism 600 being obliquely installed can reduce unmanned plane whole design height.Tube stent 611
Quantity is two, two 611 parallel clearance of tube stent settings.It is in the bracket mounting post of array distribution there are four having on flap 608
614, it is bolted to connection between bracket mounting post and tube stent 611.
In the optional scheme of the embodiment, through-hole 612 can be opened up on canopy and clamping cap 610, for for parachute
Umbrella rope be pierced by, umbrella rope is fixedly connected with the base of unmanned plane.It should be noted that in the embodiment, it can also be in cylinder 601
One end nozzle one notch of edge, for drawing umbrella rope, such umbrella rope can not have to from canopy and clamping cap 610
On be pierced by, and after parachute is launched out of cylinder 601, canopy and clamping cap 610 are not left on the umbrella rope of parachute.
Compression after parachute is placed into cylinder 601, then is installed when in use by the San Tong mechanism 600 that the embodiment provides
Lid 610, parachute is compressed, and is finally sealed up again with canopy.
As shown in Fig. 9, Figure 10 and Figure 11, the gas release device in the embodiment includes trigger mechanism 100, striker release
Mechanism 200 and storage cylinder 300.The gas release device is installed on flap 608, in the cylinder 601 to San Tong mechanism
Gas is discharged, so that parachute is projected out of cylinder 601.Wherein, storage cylinder 300 is to store compressed gas, trigger mechanism 100
Striker relieving mechanism 200 can be triggered, so that striker relieving mechanism 200 is hit the bottleneck end 310 of storage cylinder 300, to discharge pressure
Contracting gas provides ejection force to parachute.The gas that storage cylinder 300 discharges enters cylinder 601, will be placed in cylinder 601
Parachute is gone out.
Specifically, striker relieving mechanism 200 includes hollow mounting cylinder 210, the firing pin assembly in mounting cylinder 210
220 and trigger member 230.Limit body 211 is arranged in 210 one end of mounting cylinder, and 220 one end of firing pin assembly is set as hitting end, another
End setting joint end, hits bottleneck end 310 of the end to hit storage cylinder 300, compressed gas is discharged；Trigger member 230 is limited
Between limit body 211 and the shock end of firing pin assembly 220, trigger member 230 can drive firing pin assembly 220 in mounting cylinder for position
It is moved in 210；
The bottleneck end 310 of storage cylinder 300 is connected to the one end of mounting cylinder 210 far from limit body 211, also, the bottleneck end
The triggering end of 310 face firing pin assemblies 220 is hit when so that firing pin assembly 220 moving in mounting cylinder 210 by triggering end
Bottleneck end 310 is expelled to compressed gas in storage cylinder 300 in mounting cylinder 210, then is emitted into corresponding member through mounting cylinder 210
In part, pop up parachute under the active force of compressed gas.
In the present embodiment, trigger mechanism 100 is located at 200 side of striker relieving mechanism；
When trigger member 230 is in off working state, firing pin assembly 220 extend out to mounting cylinder far from the joint end for hitting end
It is clamped outside 210 and with trigger mechanism 100；Firing pin assembly 220 is set to hold it away from the position of storage cylinder 300 using trigger mechanism 100
It sets；
When trigger member 230 is in running order, so that joint end is detached from trigger mechanism 100, make firing pin assembly 220 towards storage
300 direction of gas cylinder is mobile, and using the bottleneck end 310 for hitting end shock storage cylinder 300, arranges compressed gas in storage cylinder 300
Out in mounting cylinder 210.
The gas release device provided in the present embodiment, middle utilization spring pops up the side of parachute compared with the prior art
Formula has the advantage that
1. popping up parachute using compressed gas in the way of triggering storage cylinder 300, improves parachute and pop up distance.
2. can avoid spring aging in the prior art using compressed gas, the problem of caused elastic force declines, drop is ensured
Umbrella pop-up is fallen apart from unaffected.
3. trigger mechanism 100, striker relieving mechanism 200 and storage cylinder 300 are used in combination, assembly difficulty is reduced, is convenient for
Manipulation.
In one preferred embodiment, as shown in Figure 10 and Figure 11, above-mentioned storage cylinder 300 is used with mounting cylinder 210 can
For example, connecting using thread connecting mode outer spiral shell can be arranged in 310 side of bottleneck end of storage cylinder 300 in dismantling connection mode
Internal screw thread is arranged in 210 inner wall of mounting cylinder, consequently facilitating the connection of storage cylinder 300 and mounting cylinder 210, is conveniently replaceable gas storage in line
Bottle 300.The type of the storage cylinder 300 can be using liquefaction CO2 storage cylinder 300, or uses other liquified compressed gas gas cylinders
It is substituted.
In the present embodiment, connector sleeve 213 is set preferably in mounting cylinder 210, connector sleeve 213 has threaded hole, storage cylinder
300 are threadedly coupled with connecting cylinder 213.
As shown in Figure 10 and Figure 11, in one embodiment of the invention, firing pin assembly 220 includes striker ontology 221, needle
Seat 222 and shank 223；Striker ontology 221 is connect with one end of needle stand 222, and shank 223 is connect with the other end of needle stand 222,
Striker ontology 221 is to hit the bottleneck end 310 of storage cylinder 300, to puncture bottleneck, discharges compressed gas；Shank 223 to
In a non-operative state, it is pierced by limit body 211, is clamped with trigger mechanism 100, makes position of the firing pin assembly 220 in mounting cylinder 210
It sets and remains unchanged.
Striker ontology 221 can use solid or hollow structure, when using solid construction, the needle of striker ontology 221
It will receive the enormous pressure of compressed gas behind the bottleneck end 310 of point shock storage cylinder 300, to buffer a part of impact force, lead
Cause the opening at bottleneck end 310 smaller, the speed that compressed gas releases storage cylinder 300 is slower.
In order to ensure that striker ontology 221 preferably punctures the bottleneck end 310 of storage cylinder 300, the abundant of compressed gas is ensured
It discharges, in a preferred embodiment of the invention, as shown in figure 12, there is axially disposed ventilation in striker ontology 221
Road 224, and radially it is connected to the airtube 225 of air passage 224, wherein air passage 224 runs through the needle point of striker ontology 221,
Airtube 225 runs through striker ontology 221.When the needle point of striker ontology 221 hits the bottleneck end 310 of storage cylinder 300, it is partially compressed
From leading to outside striker ontology 221 through air passage 224, airtube 225, (compressed gas is flowed to as shown in arrow in attached drawing 12 gas
Direction), the pressure of portion gas is released, to reduce the pressure that striker ontology 221 is discharged by compressed gas, makes striker sheet
The needle point of body 221 can more smoothly puncture the bottleneck end 310 of storage cylinder 300.The gas being more advantageous in storage cylinder 300 in this way
Body disposable is released, and throughput is increased, and ensures the ejection force demand to parachute.
In order to ensure the leakproofness between needle stand 222 and mounting cylinder 210, avoids compressed gas from being arranged by mounting cylinder 210 and limit
One end of position body 211 is revealed, and in one embodiment of the present of invention, is arranged in the periphery of needle stand 222 to contact mounting cylinder 210
Sealing ring 240, to make compressed gas release between the needle stand 222 in mounting cylinder 210 and the bottleneck end 310 of storage cylinder 300.
In addition, as shown in figure 11, there is flow-guiding channel 212 in mounting cylinder 210, flow-guiding channel 212 is to make storage cylinder
300 releases go out mounting cylinder 210 to the gas flow guiding in mounting cylinder 210, are emitted into the cylinder for placing parachute.Mounting cylinder 210
It is fixed by bolts on flap, and the outlet of flow-guiding channel 212 is corresponding with the air inlet 615 on flap and is connected, gas
Body is flowed out through flow-guiding channel, and is entered in cylinder from air inlet 615；It, will be on cylinder since the intracorporal air pressure of cylinder instantaneously enhances
After clamping cap and cover are washed out from cylinder, parachute is released out of cylinder.
In order to facilitate the stability that trigger member 230 and shank 223 are clamped, in a preferred embodiment of the invention, needle
Bar 223 is provided with the first card slot 226 to be clamped trigger mechanism 100, and specifically when setting, the first card slot 226 is set as annular
Slot, the annular groove are positioned close to the medium position of shank 223, and shank 223 is enabled sufficiently to stretch out mounting cylinder 210.
After the completion of the work of firing pin assembly 220, need to readjust position of the firing pin assembly 220 in mounting cylinder 210, this
In one preferred embodiment of invention, shank 223 is provided with the second card slot 227 to connecting tooling, and the second card slot 227 is set
It sets in one end far from striker ontology 221, the second card slot 227 is caught on by corresponding tooling, so that shank 223 is returned to peace
Outside fitted tube 210.
In one embodiment of the invention, trigger member 230 uses elastic element, which preferably uses spring.
Elastic element is when in a compressed state, and firing pin assembly 220 is extend out to outside mounting cylinder 210 far from the joint end for hitting end
And it is clamped with trigger mechanism 100；
When elastic element is in reset state, firing pin assembly 220 hits bottleneck end 310, while joint end is detached from triggering machine
Structure 100.
Certainly, the above-mentioned trigger member 230 in the embodiment of the present invention is not limited to may be used also using a kind of this structure type of spring
To use such as electromagnetic launch, explosive other to be designed as power and hit gas cylinder to leak for alternative solution.
In one embodiment of the invention, trigger mechanism 100 includes driving device 110, linkage and shackle member
120；Driving device 110 drives shackle member 120 mobile by linkage, makes the joint end of shackle member 120 Yu firing pin assembly 220
Connection is detached from, and specifically, shackle member 120 connect or is detached from the first card slot 226 of shank 223.Driving device 110 is adopted
With steering engine, motor drive, electromagnetic driver, cylinder or hydraulic cylinder, the present embodiment is set on the output shaft of steering engine by taking steering engine as an example
Pushing block 111 is set, pushes linkage to act using pushing block 111, to drive shackle member 120 mobile.
In one embodiment of the invention, pedestal 607 be used to support trigger mechanism 100, striker relieving mechanism 200 and
Storage cylinder 300.
In one embodiment of the invention, linkage includes swinging rod piece 130, swings rod piece 130 and is cut with scissors by shaft
It connects on pedestal 607, swings 130 one end of rod piece and cut with scissors to contact driving device 110, the other end by shaft and shackle member 120
It connects.Swinging rod piece 130 can be rotated using the shaft being hinged on pedestal 607 as rotation center, to drive shackle member 120 close
Or far from shank 223.
It is limited for the ease of the moving direction to shackle member 120, ensures and be clamped with the first card slot 226 on shank 223
In one embodiment of the invention, 121 mounting cylinder 210 of guide groove is arranged close to card in the accuracy of position in shackle member 120
Positioning pin 122 is arranged in the side of fitting 120, and positioning pin 122 and guide groove 121 cooperate, and guide groove 121 can be along positioning pin 122
It is mobile, to make the moving radially along firing pin assembly 220 of shackle member 120, ensure the accuracy of 120 shift position of shackle member.
In one embodiment of the invention, including dynamic clamping head and quiet clamping head 500,500 one end of dynamic clamping head and quiet clamping head pass through locating piece
It is fixed on pedestal 607, the other end is connect with swing rod piece 130 far from the side of institute's shackle member 120；
When trigger member 230 is in off working state, dynamic clamping head and quiet clamping head 500, which pulls, swings rod piece 130, by swinging rod piece
130 make shackle member 120 keep being clamped with the joint end of firing pin assembly 220.
When work, using driving device 110 make swing rod piece 130 towards opposite direction rotate, thus make shackle member 120 with
The shank 223 of firing pin assembly 220 is detached from, at this point, discharging elastic force using the elastic element in mounting cylinder 210, makes firing pin assembly 220
The bottleneck end 310 for hitting storage cylinder 300, is discharged compressed gas sufficiently.
As shown in figure 15, above-mentioned support frame 400 include first support 401, second support 402, connector 403, first
It is connected between bracket 401 and second support 402 by multiple connectors 403, connector 403 can be excellent using pin, bolt etc.
Selection of land, it is convenient to carry out demolition and replacement to first support 401 and second support 402.In first support 401, multiple lightening holes are set
405, the position of the lightening hole 405 of setting and quantity according to the structural strength of unmanned plane load capacity and first support 401 and
Specific setting, multiple lightening holes 405 can effectively mitigate the weight of first support 401.Similarly, it is also set in second support 402
Set multiple lightening holes 405；Mitigate the weight of second support 402.
Multiple pipe clamps 404 for clamping horn are arranged between first support 401 and second support 402.One preferably
In embodiment, multiple pipe clamps 404 are evenly arranged on the circumferential direction of first support 401 and second support 402.Above-mentioned pipe clamp 404 uses
Separate structure, including first point of folder and second point of folder, wherein first point of folder is connected by screw to first support 401, and second point
Folder is connected by screw to second support 402, and is connected by screw between first point of folder and second point of folder, to adjust two
The distance between a point of folder, and then adjust the application to the horn of different-diameter, and the clamping force to horn.
In one embodiment, which further includes battery holding mechanism, plays the role of facilitating installation battery；Specifically
Ground, as shown in figure 16, the battery holding mechanism include fixed plate 406, lock-screw 407 and battery mounting plate 408；Fixed plate
406 connect with second support 402 far from the side of first support 401；Battery mounting plate 408 is by lock-screw 407 and fixes
Plate 406 is detachably connected.By the way that battery mounting plate 408 is arranged, facilitate installation battery, battery mounting plate 408 passes through lock-screw
407 are detachably connected with fixed plate 406, when replacing battery, only need to dismantle battery mounting plate 408, have disassembly, replacement
The quick feature of battery.
In one embodiment, clamping groove 409, clamping groove 409 and lock-screw 407 are provided on battery mounting plate 408
Quantity it is corresponding, also, clamping groove 409 includes larger diameter end 410 and smaller diameter end 411, and 412 diameter of nut of screw is less than big
The diameter of diameter end 410, greater than the diameter of smaller diameter end 411.
In concrete application, since clamping groove 409 includes larger diameter end 410 and smaller diameter end 411, battery mounting plate 408 exists
When installation, nut 412 is passed through by larger diameter end 410 and is fastened in fixed plate 406, then mobile battery mounting plate 408 makes
Smaller diameter end 411 and nut 412, which are formed, to be clamped, and realizes the fixation to battery mounting plate 408 and fixed plate 406；It needs to dismantle electricity
When the mounting plate 408 of pond, battery mounting plate 408 is moved backward, larger diameter end 410 is made to be moved to the position where nut 412, is released
Position-limiting action of the nut 412 to battery mounting plate 408.
Battery mounting plate 408 is connect by 409 attachment screw mode of clamping groove with fixed plate 406, has disassembly and installation
Convenient, fast feature.
As shown in Figure 16 to 19, in a preferred embodiment, which further includes locked mechanism, and locked mechanism includes
The mounting groove 413 being arranged in second support 402, the elastic plate 414 being connect with side in mounting groove 413, and and elastic plate
The trigger member 415 of 414 connections；Trigger member 415, which is provided with, sequentially passes through elastic plate 414, fixed plate 406 and battery mounting plate 408
Hook 416, hook 416 being capable of hook joint battery mounting plate 408.Wherein, elastic plate 414 is under non-stress, hook 416
Elastic plate 414, fixed plate 406 and battery mounting plate 408 are sequentially passed through, the position-limiting action to battery mounting plate 408 is played.
Hook 416 is under stress, i.e., user pushes trigger member 415 to the direction far from battery mounting plate 408, makes card
It hooks 416 and generates movement, do not limited to battery mounting plate 408, realize unlock, battery mounting plate 408 easy to disassemble.
In one preferred embodiment, battery mounting plate 408 is provided with the limiting slot 417 for accommodating hook 416.Battery
When mounting plate 408 is mounted in fixed plate 406, hook 416 be can extend into limiting slot 417, and be installed by mobile battery
Plate 408 is clamped the side of limiting slot 417 and hook 416, reaches the position-limiting action to battery mounting plate 408.
In one preferred embodiment, trigger member 415 is provided with press section 418, press section far from one end of elastic plate 414
418 extend out to side of the second support 402 far from first support 401.In application, by manipulation press section 418, convenient for triggering
Part 415 and 416 position of hook thereon are adjusted, so that battery mounting plate 408 is locked or be unlocked.
Using above-mentioned support frame, the installation process of battery mounting plate 408 is as follows:
S1. by the nut in the land in the 410 face fixed plate 406 of larger diameter end of the clamping groove 409 of battery mounting plate 408
412, so that the larger diameter end 410 of clamping groove 409 is passed through nut 412, and then make battery mounting plate 408 is resisted against fixed plate 406
On, meanwhile, battery mounting plate 408 compresses hook 416, keeps hook 416 mobile to the direction far from battery mounting plate 408；
S2. the position of mobile battery mounting plate 408 makes the smaller diameter end 411 of clamping groove 409 be moved to nut 412 and consolidate
Between fixed board 406；Meanwhile the limiting slot 417 on battery mounting plate 408 is moved to 416 present position of hook, hook 416 is in bullet
Property plate 414 under the action of set back, extend out to outside limiting slot 417, play the position-limiting action to limiting slot 417, prevent battery
Mounting plate 408 is mobile.
The specific installation process of battery mounting plate 408 is as follows:
S1. press section 418 is pushed, it is mobile to separate 408 direction of battery mounting plate to make trigger member 415, and then make hook 416
It is detached from limiting slot 417；
S2. the position of mobile battery mounting plate 408 makes position of the clamping groove 409 with respect to nut 412, by smaller diameter end 411
It is moved to larger diameter end 410, so as to dismantle battery mounting plate 408.
In one embodiment, multiple weight loss grooves 419 are arranged in battery mounting plate 408.It can reduce electricity by weight loss groove 419
The weight of pond mounting plate 408, and then reduce the power consumption of unmanned plane.
As shown in figure 20, unmanned plane provided by the invention further includes horn 720 and foldable assembly 730, and horn 720 includes solid
Fixed arm 711 and fold arm 712,711 one end of fixed arm connect pipe clamp 404,711 other end of fixed arm by foldable assembly 730 with
Arm 712 is folded to connect.
Specifically, as shown in Figure 20-Figure 24, the foldable assembly 730 include: the first folded piece 700, the second folded piece 702,
Fastener 704 and the first washer 706；First folded piece 700 is connect by rotating mechanism with the second folded piece 702；First folding
The front end of overlapping piece 700 is connect with the fixed arm 711 close to support frame 400, the rear end of the first folded piece 700 and the second folded piece
702 front end is connected by rotating mechanism, and the rear end of the second folded piece 702 is connect with far from folding arm 712；Using such connection
Mode enables to fold arm 712 under the rotary action of the second folded piece 702 and the first folded piece 700 relative to fixed arm 711
Up and down or left and right rotation；
Preferably, as shown in figure 22, rotating mechanism includes the first lug 707 being set on the first folded piece 700, setting
In the second lug 708 and bolt 709 on the second folded piece 702；Bolt 709 is connected to first lug 707 and the second lug 708
On.First lug 707 is set as two, and the rear end of the first folded piece 700 is arranged in first lug 707；Two first lugs 707
Upper upright position respectively opens up a through-hole；Second lug 708 is set as one, and the second lug 708 is arranged in the second folded piece 702
Front end；A through-hole is opened up on second lug 708；When first folded piece 700 is abutted with the second folded piece 702, second is convex
Ear 708 is located between two first lugs 707, and first lug 707 is corresponding with the lead to the hole site on the second lug 708 accurately to wear
Connecting bolt 709；
The rear end of first folded piece 700 and the front end of the second folded piece 702 are additionally provided with the matched limited block of shape；When logical
Limit hole and the second folding when crossing rotating mechanism the first folded piece 700 of connection and the second folded piece 702, on the first folded piece 700
The limit hole of overlapping piece 702 can grafting it is integral so that the rotation angle between the first folded piece 700 and the second folded piece 702
Less than 180 °；On the one hand playing prevents from causing to connect the case where not fastening because rotation angle is spent greatly, on the other hand
Convenient for operation.
As shown in Figure 21, Figure 22, the first limiting section 701 is provided on the first folded piece 700；First washer 706 is socketed in
On first folded piece 700, also, the first washer 706 is supported in the first limiting section 701 close to the side of the second folded piece 702；
The first above-mentioned limiting section 701 is the annular protrusion structure for being set to 700 periphery of the first folded piece；Also, first
Limiting section 701 is located at the middle part of the first folded piece 700；First limiting section 701 can play the first washer 706 of limitation to far from the
The mobile effect in 702 direction of eighty percent discount overlapping piece；First washer 706 has elasticity, can select the elasticity such as nitrile rubber or silicon rubber
Material is made, also, the size of the first washer 706 is identical as the size of the first limiting section 701.
As shown in Figure 20, Figure 23, Figure 24, fastener 704 can be socketed in the first folded piece 700 and the second folded piece 702
On, also, the port of fastener 704 can be supported in side of first washer 706 far from the first limiting section 701.Fastener 704
Using the nut structure of both ends open；When fastener 704 is socketed on the first folded piece 700 and the second folded piece 702, close to the
One end of one folded piece 700 is front end, is rear end close to one end of the second folded piece 702；For the intensity of foldable assembly, first
Folded piece 700, the second folded piece 702 and fastener 704 are all made of metal material and are made.
In one preferred embodiment, above-mentioned fastener 704 is connected through a screw thread with the first folded piece 700.
First folded piece 700 is provided with outer from the outer wall between the rear end of 701 to the first folded piece 700 of the first limiting section
Screw thread, the inner wall of fastener 704 are provided with internal screw thread, and the two thread rotary orientation is consistent；Installation personnel first will in specific setting
Second folded piece 702 turns to the position horizontal with the first folded piece 700；Then fastener 704 is socketed in the second folded piece
702 and first on folded piece 700, and along thread rotary orientation turn Fastener 704, fastener 704 can be gradually to close to the first pad
The direction of circle 706 is mobile until the front-end port of fastener 704 is supported on the first washer 706；Since the first washer 706 has
Elasticity can produce slight deformation under the squeezing action by fastener 704, in the compression limit value for reaching the first washer 706
The preceding extruding degree that can further deepen between fastener 704 and the first washer 706 promotes fastener 704 and first with this
The stability connected between washer 706 reduces fastener 704 and loosens because connection is not tight when unmanned plane is vibrated
The probability of phenomenon, at this point, fastener 704 is capable of fixing in the junction of the first folded piece 700 and the second folded piece 702, therefore,
Second folded piece 702 can not be rotated relative to the first folded piece 700, and foldable assembly is in locking state.
As shown in figure 22, cricoid second limiting section 703 is provided on the second folded piece 702.The second above-mentioned limiting section
703 be the annular protrusion structure for being set to 702 periphery of the second folded piece；Before second limiting section 703 is located at the second folded piece 702
End；
As shown in figure 22, foldable assembly includes second packing ring 710；Second packing ring 710 is socketed on the second folded piece 702,
Also, second packing ring 710 is supported in side of second limiting section 703 far from the first folded piece 700.Second limiting section 703 plays
Second packing ring 710 is limited to the effect mobile close to the direction of the first folded piece 700；Second packing ring 710 uses metal material system
At or second packing ring 710 be made of plastic material.Second packing ring 710 can be made of material copper, can also select PC
The plastic materials such as plastics, nylon, abs plastics are made, and can also select steel material spring；
Second packing ring 710 can be supported after being socketed on the second folded piece 702 on the second limiting section 703, second packing ring
710 diameter is slightly larger than the diameter of the second limiting section 703, therefore when fastener 704 is socketed on the second folded piece 702, tightly
The inner wall of firmware 704 can be contacted with second packing ring 710；When turn Fastener 704 carries out locking operation, second packing ring 710
Barrier effect by the second limiting section 703 is without as fastener 704 is to close to the movement of the direction of the first folded piece 700；
In addition, the inner wall that fastener 704 is avoided by the way that second packing ring 710 is arranged directly is contacted with the outer wall of the second folded piece 702, from
And the thread pressure and frictional force effect generated when solving the outer wall of the second folded piece 702 by the rotation of fastener 704 causes
The outer wall of second folded piece 702 leads to the problem of abrasion and deformation.
Preferably, as shown in figure 24, the inner wall of fastener 704 is provided with protrusion 705；Protrusion 705 can be supported
Side of the second packing ring 710 far from the second limiting section 703.One circle protrusion 705 of setting on the rear end inner wall of fastener 704, when
When turn Fastener 704 carries out locking operation, protrusion 705 is as fastener 704 moves closer to second packing ring 710 until folding
When component reaches locking state, protrusion 705 can be supported in second packing ring 710 just；Using the above structure, it on the one hand rises
To the effect of fixed second packing ring 710, on the other hand further enhances and connected between fastener 704 and the second folded piece 702
Stability.
Referring to fig. 2 shown in 5 and Figure 26, unmanned plane provided by the present application further includes delivery storehouse 802；Deliver storehouse 802 and second
Bracket 101 is connected, and delivery storehouse 802 is flexible material, or the material in delivery storehouse 802 for transporting cargo, the material in delivery storehouse 802
Material is elastic material.
Since the density of flexible material and elastic material is smaller, i.e., using size made of flexible material or elastic material
Biggish delivery storehouse 802, weight also tend to be less than by the prior art by EPP (polypropylene plastics foamed material) or plastics
The container of comparable size made of equal materials.And the container made of EPP or plastic or other material, form are fixed, and are being transported
When the lesser cargo of size, it is easy to happen the case where cargo is fallen.And flexible material or elastic material have form flexible
Characteristic, transportation clearance much smaller than delivery 802 capacity of storehouse cargo when, delivery storehouse 802 geomery can also be with goods
The geomery of object and change, prevent logistics unmanned plane during flight, the case where cargo of generation is fallen.
Referring to fig. 2 shown in 6, delivery storehouse 802 includes connecting rope 806 and delivery storehouse main body 807, and delivery storehouse main body 807 is located at
One end of the lower section of second support 101, connecting rope 806 is connected with second support 101, the other end of connecting rope 806 and delivery
Storehouse main body 807 is connected.
In this embodiment, delivery storehouse 802 includes connecting rope 806 and delivery storehouse main body 807, and connecting rope 806 will be for that will transport
Storehouse main body 807 is carried to be connected with second support 101, optionally, one end and the second support 101 of connecting rope 806 are detachably connected,
The other end of connecting rope 806 is detachably connected with delivery storehouse main body 807.Delivery storehouse main body 807 is located under second support 101
Side can be sling delivery storehouse main body 807 by connecting rope 806 in logistics unmanned plane during flying.
In the optional scheme of the embodiment, the lower end surface of second support 101 is provided with link 808, is arranged in connecting rope 806
There is hook 809, hook 809 is hung on link 808.The quantity of link 808 can be multiple, and multiple links 808 are uniformly arranged
It is distributed in the lower end surface of second support 101, the quantity of connecting rope 806 is multiple, and the number of the quantity of connecting rope 806 and link 808
Measure identical, one end of connecting rope 806 is connected with delivery storehouse main body 807, and the weight for delivering storehouse 802 and cargo is evenly distributed on often
In a connecting rope 806, it is ensured that when transport cargo, logistics unmanned plane during flying is steady.The other end of connecting rope 806 is provided with hook
809, hook 809 is hung on link 808, be can be realized and is sling delivery storehouse main body 807.
As shown in figure 25, unmanned plane provided by the present application further includes foot prop 804, camera assembly 803 and first connecting rod
805；The setting of foot prop 804 is fixed on foot prop 804 in 403 two sides of second support, camera assembly 803 by first connecting rod 805,
Also, camera assembly 803 is located at 802 lower section of delivery storehouse.Camera assembly 803 can acquire the image information on ground, utilize calculating
After machine vision technique carries out image procossing, obtains environmental information and then realize navigation, the external worlds such as GPS can lost in unmanned plane
When aided location positions, it can continue to according to regulation airline operation.Delivery storehouse 802 is located at the lower section of second support 402, and images
Component 803 is located at the lower section in delivery storehouse 802, so that the visual field of camera assembly 803 not will receive delivery storehouse 802 and delivery cargo
Block.
Claims (17)
1. a kind of unmanned plane, which is characterized in that including gas release device, San Tong mechanism and support frame；The gas release dress
It sets and is installed in the San Tong mechanism, the San Tong mechanism is installed on support frame as described above；
The San Tong mechanism includes cylinder, clamping cap and cover；The clamping cap is installed in the barrel chamber of one end of the cylinder,
The cover is installed on the tube port position of one end of the cylinder；
The gas release device includes trigger mechanism, striker relieving mechanism and storage cylinder；
The striker relieving mechanism, including hollow mounting cylinder, the firing pin assembly in the mounting cylinder and trigger member, institute
State mounting cylinder one end setting limit body, the trigger member be limited in the limit body and the firing pin assembly shock end it
Between, the trigger member can drive the firing pin assembly to move in the mounting cylinder；The bottleneck end of the storage cylinder is connected to
The one end of the mounting cylinder far from the limit body, the bottleneck rectify the shock end to the firing pin assembly, also, the peace
Fitted tube is connected to the cylinder；
The trigger mechanism is located at striker relieving mechanism side；When the trigger member is in off working state, the striker
Component extend out to outside the mounting cylinder far from the joint end for hitting end and is clamped with the trigger mechanism；
When the trigger member is in running order, the firing pin assembly is set to hit the bottleneck end, while the joint end is detached from
The trigger mechanism；
Support frame as described above includes first support, second support and connector；
Pass through multiple connector connections, the first support and/or institute between the first support and the second support
It states and multiple lightening holes is set in second support.
2. unmanned plane according to claim 1, which is characterized in that the firing pin assembly include striker ontology, needle stand and
Shank；The striker ontology is connect with one end of the needle stand, and the shank is connect with the other end of the needle stand.
3. unmanned plane according to claim 2, which is characterized in that have axially disposed ventilation in the striker ontology
Road and the airtube for being radially connected to the air passage, the air passage run through the needle point of the striker ontology.
4. unmanned plane according to claim 2, which is characterized in that the trigger mechanism includes driving device, linkage
And shackle member；
The driving device drives the shackle member mobile by linkage, makes the institute of the shackle member Yu the firing pin assembly
It states joint end connection or is detached from.
5. unmanned plane according to claim 4, which is characterized in that the San Tong mechanism further includes pedestal, the pedestal peace
In the barrel chamber of the other end loaded on the cylinder；The pedestal be used to support the trigger mechanism, the striker relieving mechanism with
And the storage cylinder.
6. unmanned plane according to claim 5, which is characterized in that the linkage includes swinging rod piece, the swing
Rod piece passes through shaft hingedly on the base, and described swing rod piece one end passes through to contact the driving device, the other end
Shaft and the shackle member are hinged.
7. unmanned plane according to claim 4, which is characterized in that guide groove, the mounting cylinder are arranged in the shackle member
Positioning pin is set close to the side of the shackle member of the firing pin assembly, the positioning pin and the guide groove cooperate, so that described
Shackle member is moved radially along the firing pin assembly.
8. unmanned plane according to claim 1, which is characterized in that the clamping cap include be sequentially connected the boss portion connect,
Interconnecting piece and compressed part；The other end of the compressed part close to the cylinder, the other end of the boss portion far from the cylinder；
The interconnecting piece is in contact with the barrel of the cylinder.
9. unmanned plane according to claim 1, which is characterized in that including pipe clamp, horn and foldable assembly, multiple pipes
Sandwiched is set between first support and the second support；The horn includes fixed arm and folding arm, described fixed arm one end
The pipe clamp is connected, the fixed arm other end is connect by the foldable assembly with the folding arm.
10. unmanned plane according to claim 9, which is characterized in that the foldable assembly includes the first folded piece, the second folding
Overlapping piece, fastener and the first washer；
First folded piece is socketed on the fixed arm, and second folded piece is socketed on the folding arm；
First folded piece is connect by rotating mechanism with second folded piece, is provided with first on first folded piece
Limiting section；
First washer is socketed on first folded piece, also, first washer is supported in first limiting section
Close to the side of second folded piece, first washer has elasticity；
The fastener can be socketed on first folded piece and second folded piece, also, the end of the fastener
Mouth can be supported in side of first washer far from first limiting section.
11. unmanned plane according to claim 10, which is characterized in that the foldable assembly includes second packing ring；
Cricoid second limiting section is provided on second folded piece；
The second packing ring is socketed on second folded piece, also, the second packing ring is supported in second limiting section
Side far from first folded piece.
12. unmanned plane according to claim 1, which is characterized in that including battery holding mechanism, the battery holding mechanism
Including fixed plate, lock-screw and battery mounting plate；
The fixed plate is connect with the second support far from the side of first support；
The battery mounting plate is detachably connected by lock-screw and the fixed plate.
13. unmanned plane according to claim 12, which is characterized in that clamping groove is set on the battery mounting plate, it is described
Clamping groove is corresponding with the quantity of the lock-screw, also, the clamping groove includes larger diameter end and smaller diameter end, the screw
Head diameter be less than the larger diameter end diameter, greater than the diameter of smaller diameter end.
14. unmanned plane according to claim 13, which is characterized in that including locked mechanism, the locked mechanism includes setting
It sets in the mounting groove in the second support, the elastic plate that is connect with side in the mounting groove, and connects with the elastic plate
The trigger member connect；The trigger member is provided with the card for sequentially passing through the elastic plate, the fixed plate and the battery mounting plate
It hooks, the hook being capable of battery mounting plate described in hook joint.
15. unmanned plane according to claim 1, which is characterized in that including delivering storehouse, the delivery storehouse and support frame as described above
It is connected, for transporting cargo, the material in the delivery storehouse is flexible material or elastic material in the delivery storehouse.
16. unmanned plane according to claim 15, which is characterized in that the delivery storehouse includes connecting rope and delivery storehouse master
Body, the delivery storehouse main body are located at the lower section of support frame as described above, and one end of the connecting rope is connect with support frame as described above, the company
The other end of splicing is connected with delivery storehouse main body.
17. unmanned plane according to claim 15, which is characterized in that including foot prop, camera assembly and first connecting rod；
The foot prop is arranged in support frame as described above two sides, and the camera assembly is fixed on the foot prop by first connecting rod,
Also, the camera assembly is located at below the delivery storehouse.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811568284.9A CN109436343B (en) | 2018-12-20 | 2018-12-20 | Unmanned plane |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811568284.9A CN109436343B (en) | 2018-12-20 | 2018-12-20 | Unmanned plane |
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| Publication Number | Publication Date |
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| CN109436343A true CN109436343A (en) | 2019-03-08 |
| CN109436343B CN109436343B (en) | 2024-02-20 |
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| CN201811568284.9A Active CN109436343B (en) | 2018-12-20 | 2018-12-20 | Unmanned plane |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110979647A (en) * | 2019-12-24 | 2020-04-10 | 广东电网有限责任公司 | Air fault protection device and method suitable for multi-rotor unmanned aerial vehicle |
| CN111634422A (en) * | 2020-06-11 | 2020-09-08 | 潍坊中达凯盛机械科技有限公司 | Unmanned aerial vehicle carrier |
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| CN111634422B (en) * | 2020-06-11 | 2022-04-29 | 浙江南瑞飞翼航空技术有限公司 | Unmanned aerial vehicle carrier |
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