CN108928489A - The long-range jettison device of unmanned plane carry hand-throw type grenade, pinking bullet - Google Patents
The long-range jettison device of unmanned plane carry hand-throw type grenade, pinking bullet Download PDFInfo
- Publication number
- CN108928489A CN108928489A CN201811069760.2A CN201811069760A CN108928489A CN 108928489 A CN108928489 A CN 108928489A CN 201811069760 A CN201811069760 A CN 201811069760A CN 108928489 A CN108928489 A CN 108928489A
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- electric cylinders
- trapezoidal
- carry
- bomb
- supporting plate
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- 230000007246 mechanism Effects 0.000 claims abstract description 61
- 230000005611 electricity Effects 0.000 claims 1
- 230000001105 regulatory effect Effects 0.000 claims 1
- 239000007787 solid Substances 0.000 claims 1
- 230000001960 triggered effect Effects 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 4
- 238000009434 installation Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- ZLSWBLPERHFHIS-UHFFFAOYSA-N Fenoprop Chemical compound OC(=O)C(C)OC1=CC(Cl)=C(Cl)C=C1Cl ZLSWBLPERHFHIS-UHFFFAOYSA-N 0.000 description 1
- 241000219991 Lythraceae Species 0.000 description 1
- 235000014360 Punica granatum Nutrition 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 238000005474 detonation Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004079 fireproofing Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000009527 percussion Methods 0.000 description 1
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
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/04—Dropping, ejecting, or releasing articles the articles being explosive, e.g. bombs
- B64D1/06—Bomb releasing; Bombs doors
-
- 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
-
- 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
- B64U2101/15—UAVs specially adapted for particular uses or applications for conventional or electronic warfare
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Catching Or Destruction (AREA)
Abstract
The present invention provides the long-range jettison device of a kind of unmanned plane carry hand-throw type grenade, pinking bullet, including the carry platform for loading battery and is suspended on the trigger mechanism that drops a bomb of carry mesa base;The trigger mechanism that drops a bomb includes drop a bomb fixed frame, longitudinal electric cylinders, lateral electric cylinders, body fixing seat and pull ring clamp mechanism;Longitudinal electric cylinders, lateral electric cylinders and body fixing seat are separately fixed at and play on fixed frame, the U-type groove for accommodating fixed body is offered in body fixing seat, the locking channel being connected to U-type groove is offered in the side of body fixing seat, sliding is provided with latch segment in locking channel, one end of latch segment protrudes into U-type groove and body is locked in U-type groove, and the other end of latch segment is connect by pull ring clamp mechanism with the piston rod of longitudinal electric cylinders;It is connected with pulling pin fixed block in the end of the piston rod of lateral electric cylinders, is protruding with pulling pin in pulling pin fixed block.The present invention replaces combatant to throw body, and security demonstrate,proves the personal safety of combatant.
Description
Technical field
The present invention relates to police equipment technical fields, more specifically, be related to a kind of unmanned plane carry hand-throw type grenade,
The long-range jettison device of pinking bullet.
Background technique
Currently, hand-throw type grenade, pinking bullet mainly use in miniwar or local battlefield operation, it to be used for firepower
Terrorist or quick-fried probably molecule are suppressed, shot dead or frightened, stability maintenance is played the role of.Existing hand-throw type grenade, pinking bullet
Trigger method is manual pull ring throwing percussion, and larger by surrounding environment influence, by the strength of people, angle etc. is affected, cannot
Accurately, it is rapidly achieved throwing purpose, certain danger is caused to the personal safety of combatant.
Summary of the invention
In view of the above problems, the object of the present invention is to provide a kind of unmanned plane carry hand-throw type grenade, pinking bullet it is remote
Journey jettison device, it is larger with there are air resistances the flow field that solves inside SOFA device, in the equipment such as bellows flow dead zone compared with
More, turbulent extent is larger, and it is lower to touch mouth jet stream rigidity, and jet stream is decayed rapid problem.
The long-range jettison device of unmanned plane carry hand-throw type grenade provided by the invention, pinking bullet, comprising: for loading
The carry platform of battery and the trigger mechanism that drops a bomb for being suspended on carry mesa base;Wherein, the trigger mechanism that drops a bomb includes dropping a bomb admittedly
Determine frame, longitudinal electric cylinders, lateral electric cylinders, body fixing seat and pull ring clamp mechanism;Longitudinal electric cylinders, lateral electric cylinders and body fixing seat point
It is not fixed on and plays on fixed frame, the U-type groove for accommodating fixed body is offered in body fixing seat, in body fixing seat
Side offers the locking channel being connected to U-type groove, and sliding is provided with latch segment in locking channel, one end of latch segment be with
The compatible arc end of body outer surface radian, and protrude into U-type groove and body is locked in U-type groove, the other end of latch segment is logical
It crosses pull ring clamp mechanism to connect with the piston rod of longitudinal electric cylinders, in the movement of longitudinal electric cylinders, triggering pull ring clamp mechanism pulls latch segment
It is mobile, it is detached from the arc end of latch segment and body;It is connected with pulling pin fixed block in the end of the piston rod of lateral electric cylinders, is being drawn
Pin fixed block is protruding with pulling pin, and in the movement of lateral electric cylinders, triggering pulling pin draws the insurance pull ring for removing body.
Furthermore it is preferred that structure be, one end that latch segment is connect with pull ring clamp mechanism have connection bump, and, pull ring
Clamp mechanism includes connecting rod, rotation axis, rotating shaft base, linking arm and connecting shaft, and connecting rod is rotatably connected on rotation axis by rotation axis
On seat, one end of connecting rod and connection bump respectively run through a connecting shaft, and the corresponding both ends of two connecting shafts pass through one respectively
Linking arm connection, the other end of connecting rod is tilted to be connect with the piston rod of longitudinal electric cylinders.
Furthermore it is two sets that preferred structure, which is the drop a bomb quantity of trigger mechanism, and the shared fixed frame that drops a bomb, two sets
The two sides for the fixed frame that drops a bomb are arranged in trigger mechanism reverse symmetry of dropping a bomb.
Furthermore it is preferred that structure be that carry platform includes battery supporting plate, by the first articulated shaft is hinged on battery supporting plate bottom
The carry base in portion is hinged on the clamping mechanism of battery supporting plate two sides by the second hinged axial symmetry, is symmetrically connected to battery tray
Plate two sides are close to the angle adjustment arm of clamping mechanism, the trapezoidal grafting block for being connected to carry base bottom, setting in trapezoidal grafting
The spring retaining mechanism of block front end and the trapezoidal plug socket for being connected to trapezoidal grafting block bottom.
Additionally, it is preferred that structure be to be opened up on battery supporting plate there are two lightening hole, in the two sides of battery supporting plate band respectively
There are two connection shaft seat and two engaging lugs, two connection shaft seats are symmetrically fixedly connected below battery supporting plate side, and first
Articulated shaft is hinged by battery supporting plate and carry base by two connection shaft seats, is machined with respectively on two engaging lugs hinged
Hole, the second articulated shaft is hinged with battery supporting plate by clamping mechanism by hinge hole, is additionally provided on two engaging lugs for limiting
The limited block of gyration on fabrication connection mechanism.
Furthermore preferred structure is, opened up on carry base there are two lightening hole, in two sides of carry base point
Hole is not threaded it;Clamping mechanism includes the clamp hinged with battery supporting plate and is connect by fast-assembling bolt with clamp dynamic
Two blocked holes are formed after folder, clamp and dynamic folder connection, are machined with lightening hole respectively in clamp and dynamic folder;Angle adjustment arm is
Arc-shaped flaky structure, is provided with an arc adjustment hole in angle adjustment arm, and angle adjustment arm passes through fixing bolt and battery tray
Plate is fixedly connected, and an adjusting locking bolt is provided in arc adjustment hole, adjusts one end and the carry base of locking bolt
Threaded hole be threadedly coupled.
Furthermore it is preferred that structure be that trapezoidal grafting block is connected by screw in the bottom of carry base, trapezoidal grafting block
Front end has the first protrusion, and the mounting hole for installing spring retaining mechanism is offered in the first protrusion, trapezoidal grafting block
Two sides are the inclined surface being symmetrically inclined outwardly.
Additionally, it is preferred that structure be to offer connection on trapezoidal plug socket to drop a bomb the connecting hole of fixed frame, inserted trapezoidal
It is machined with the trapezoidal inserting groove to match with trapezoidal grafting block on joint chair, the front end of trapezoidal plug socket has the second protrusion, the
It is machined with locking slot corresponding with position of mounting hole in two protrusions, is fixedly connected with below carry base for trapezoidal
Plug socket is inserted into after trapezoidal grafting block the block for playing position-limiting action.
Furthermore preferred structure is, spring retaining mechanism includes spring locking plug and pull ring, and pull ring is fixedly connected on bullet
The top of spring locking plug, the bottom of spring locking plug pass through mounting hole and are caught in locking slot.
Using the unmanned plane carry hand-throw type grenade of aforementioned present invention, the long-range jettison device of pinking bullet, can obtain
Following technical effect:
(1) hand-throw type grenade, pinking bullet are thrown using the trigger mechanism that drops a bomb, the trigger mechanism that drops a bomb is suspended on unmanned plane, is led to
The high maneuverability for crossing unmanned plane replaces combatant to throw hand-throw type grenade, pinking bullet, and hand-throw type hand pomegranate not only may be implemented
Bullet, pinking bullet quickly reach disposition scene, it can also be ensured that the personal safety of combatant;
(2) platform that a variety of carry systems may be implemented shares, and Fast Installation is switched fast;
(3) aluminium shell wrapping device is utilized, fireproofing flame-resistant material is surface-treated, a variety of carry systems are realized in modularized design
Platform share, Fast Installation is switched fast.
Detailed description of the invention
By reference to the explanation below in conjunction with attached drawing, and with a more complete understanding of the present invention, of the invention is other
Purpose and result will be more clearly understood and understood.In the accompanying drawings:
Fig. 1 is according to the entirety of the unmanned plane carry hand-throw type grenade of the embodiment of the present invention, the long-range jettison device of pinking bullet
Structural schematic diagram;
Fig. 2 is the overall structure diagram according to the carry platform of the embodiment of the present invention;
Fig. 3 is the configuration schematic diagram according to the carry platform of the embodiment of the present invention;
Fig. 4 is the structural schematic diagram according to the trigger mechanism that drops a bomb of the embodiment of the present invention.
Specific embodiment
In the following description, for purposes of illustration, it in order to provide the comprehensive understanding to one or more embodiments, explains
Many details are stated.It may be evident, however, that these embodiments can also be realized without these specific details.
In other examples, one or more embodiments for ease of description, well known structure and equipment are shown in block form an.
The long-range throwing that Fig. 1 shows unmanned plane carry hand-throw type grenade, pinking bullet according to an embodiment of the present invention fills
The overall structure set.
As shown in Figure 1, the long-range throwing of unmanned plane carry hand-throw type grenade provided in an embodiment of the present invention, pinking bullet fills
Setting includes: carry platform, batteryWith the trigger mechanism that drops a bomb, batteryIt is mounted on carry platformOn, batteryFor for throw
Play trigger mechanismMiddle electric elements power supply, drop a bomb trigger mechanismIt is suspended on carry platformBottom, for throw hand throw
Formula grenade, pinking bullet;Carry platformIt is suspended on unmanned plane foot propOn, it is flat that unmanned plane foot prop is fixedly connected on fast insert-pull
PlatformBottom end.
Fig. 2 and Fig. 3 respectively illustrates the overall structure and detonation configuration of carry platform according to an embodiment of the present invention.
As shown in Figures 2 and 3, carry platform includes for installing the battery supporting plate 1 of battery, being cut with scissors by the first articulated shaft 2
It connects the carry base 3 below battery supporting plate 1, be symmetrically hinged on the clamping mechanism of 1 two sides of battery supporting plate by the second articulated shaft 4
5,1 two sides of battery supporting plate are symmetrically connected to and closes on the angle adjustment arm 6 of clamping mechanism 5, be connected to the ladder of 3 bottom of carry base
Shape grafting block 7, is connected to the trapezoidal slotting of trapezoidal 7 bottom of grafting block at the spring retaining mechanism 8 that trapezoidal 7 front end of grafting block is arranged in
Joint chair 9;It is opened up on battery supporting plate 1 and is symmetrically fixedly connected on battery supporting plate 1 there are two lightening hole 1-1, two connection shaft seat 1-2
Side in the following, the first articulated shaft 2 by two connection shaft seat 1-2 by battery supporting plate 1 and carry base 3 hinged, battery supporting plate 1
Two sides also band hinge hole 1-4 is machined on engaging lug 1-3, the second articulated shaft 4 passes through hinge hole there are two engaging lug 1-3
1-4 is hinged by clamping mechanism 5 and battery supporting plate 1, is additionally provided with limited block 1-5 on two engaging lug 1-3 of battery supporting plate 1,
Limited block 1-5 is used to limit the upper gyration of clamping mechanism 5, opens up that there are two lightening hole 3-1 on carry base 3, in carry
Two sides of base 3 are threaded hole 3-2 respectively;Clamping mechanism 5 includes the clamp 5-1 hinged with battery supporting plate 1 and leads to
The dynamic folder 5-3 that fast-assembling bolt 5-2 is connect with clamp 5-1 is crossed, clamp 5-1 forms two blocked hole 5-4 after connecting with dynamic folder 5-3,
It is machined with lightening hole 5-5 respectively on clamp 5-1 and dynamic folder 5-3;Angle adjustment arm 6 is arc-shaped flaky structure, in angular adjustment
An arc adjustment hole 6-1 is provided on arm 6, angle adjustment arm 6 is fixedly connected by fixing bolt 6-2 with battery supporting plate 1, in arc
An adjusting locking bolt 6-3 is provided in shape adjustment hole 6-1, the one end and threaded hole 3-2 screw thread for adjusting locking bolt 6-3 connect
It connects;Trapezoidal grafting block 7 is connected to the bottom of carry base 3 by multiple screws, and the front end of trapezoidal grafting block 7 has one first
Raised 7-1 offers one for installing the mounting hole 7-2 of spring retaining mechanism 8, trapezoidal grafting block 7 on the first protrusion 7-1
Two sides be the inclined surface 7-3 being symmetrically inclined outwardly, offered on trapezoidal plug socket 9 it is multiple connection carry objects companies
Hole 9-1 is met, one and the matched trapezoidal inserting groove 9-2 of trapezoidal grafting block 7 are machined on trapezoidal plug socket 9, in trapezoidal grafting
The front end of seat 9 has one second protrusion 9-3, and a locking slot 9-4, locking slot 9-4 and peace are offered on the second protrusion 9-3
It is corresponding to fill hole 7-2, is fixedly connected with a block 10 below carry base 3 behind trapezoidal grafting block 7, block 10 is used for
It is limited after trapezoidal plug socket 9 is inserted into trapezoidal grafting block 7, spring retaining mechanism 8 includes spring locking plug 8-1 and pull ring
8-2, pull ring 8-2 are fixedly connected on the top of spring locking plug 8-1, and the bottom of spring locking plug 8-1 passes through mounting hole card
Enter in locking slot 9-4, in pull ring 8-2 pull-up, spring locking plug 8-1 is retracted, the spring locking plug when pull ring 8-2 is put down
8-1 stretches out, and is caught in locking slot 9-4.
Fig. 4 shows the structure of the trigger mechanism according to an embodiment of the present invention that drops a bomb.
As shown in figure 4, the trigger mechanism that drops a bomb is fixed including the fixed frame 11 that drops a bomb, longitudinal electric cylinders 12, lateral electric cylinders 13, body
Seat 14 and pull ring clamp mechanism;Longitudinal electric cylinders 12, lateral electric cylinders 13 are separately fixed at body fixing seat 14 and play on fixed frame 11,
The U-type groove for accommodating fixed body (referring to hand-throw type grenade, pinking bullet) 15 is offered in body fixing seat 14, in body
The side of fixing seat 14 offers the locking channel being connected to U-type groove, and sliding is provided with latch segment 16 in locking channel, locks
One end of block 16 is arc end compatible with 15 outer surface radian of body, and protrudes into U-type groove and body 15 is locked at U-type groove
Interior, the other end of latch segment 16 is connect by pull ring clamp mechanism with the piston rod of longitudinal electric cylinders 12, in latch segment 16 and pull ring
One end of mechanism connection has connection bump 16-1, and in the movement of longitudinal electric cylinders 12, triggering pull ring clamp mechanism pulls latch segment 16
It is moved in locking channel, is detached from the arc end of latch segment 16 and body 15, body 15 is enable to pop up U-type groove;In transverse direction
The end of the piston rod of electric cylinders 13 is connected with pulling pin fixed block 17, is protruding with pulling pin 17-1, body 15 in pulling pin fixed block 17
Insurance pull ring 15-1 hang on pulling pin 17-1, lateral electric cylinders 13 movement when, pull pulling pin 17-1, triggering pulling pin 17-1 drawing removes
The insurance pull ring 15-1 of body 15.
Pull ring clamp mechanism includes connecting rod 18, rotation axis 19, rotating shaft base 20, linking arm 21 and connecting shaft 22, and connecting rod 18 is logical
It crosses rotation axis 19 to be rotatably connected on rotating shaft base 20, the principle of connecting rod 18 and rotation axis 19 is lever principle, rotation axis 19
Position is position of the fulcrum, in order to laborsaving, the position of rotation axis 19 preferably adjacent to latch segment 16, one end of connecting rod 18 with connect it is convex
It plays 16-1 and respectively runs through a connecting shaft, two corresponding both ends of connecting shaft 22 pass through a linking arm 21 respectively and connect, connecting rod
18 other end is tilted to be connect with the piston rod of longitudinal electric cylinders 12;When the piston rod downward actuation of longitudinal electric cylinders 12, band turn
Moving axis 19 rotates counterclockwise, to pull latch segment 16 mobile to the direction of longitudinal electric cylinders 12, make the arc end of latch segment 16 with
Body 15 is detached from.
In order to realize that a machine two is thrown, the quantity for the trigger mechanism that drops a bomb is two sets, and two sets of trigger mechanisms that drop a bomb share one
Drop a bomb fixed frame, and the two sides for the fixed frame that drops a bomb are arranged in two sets of trigger mechanism reverse symmetries of dropping a bomb, since the insurance of body 15 is drawn
Two sets of trigger mechanism reverse symmetry settings of dropping a bomb, this set can only be also able to maintain the load-carrying of unmanned plane by the positional relationship of ring
Balance.
More than, only a specific embodiment of the invention, but scope of protection of the present invention is not limited thereto, and it is any to be familiar with
Those skilled in the art in the technical scope disclosed by the present invention, can easily think of the change or the replacement, and should all cover
Within protection scope of the present invention.Therefore, protection scope of the present invention should be subject to the protection scope in claims.
Claims (9)
1. the long-range jettison device of a kind of unmanned plane carry hand-throw type grenade, pinking bullet, which is characterized in that including for loading
The carry platform of battery and the trigger mechanism that drops a bomb for being suspended on the carry mesa base;Wherein, the trigger mechanism packet that drops a bomb
Include the fixed frame that drops a bomb, longitudinal electric cylinders, lateral electric cylinders, body fixing seat and pull ring clamp mechanism;The longitudinal direction electric cylinders, the laterally electricity
Cylinder and the body fixing seat are separately fixed on the bullet fixed frame, are offered in the body fixing seat solid for accommodating
The U-type groove for determining body offers the locking channel being connected to the U-type groove in the side of the body fixing seat, in the lock
Sliding is provided with latch segment in tight channel, and one end of the latch segment is arc compatible with body outer surface radian
End, and protrude into the U-type groove and the body is locked in the U-type groove, the other end of the latch segment passes through the pull ring
Clamp mechanism is connect with the piston rod of longitudinal electric cylinders, in longitudinal electric cylinders movement, is triggered the pull ring clamp mechanism and is pulled
The latch segment is mobile, is detached from the arc end of the latch segment and the body;At the end of the piston rod of the lateral electric cylinders
Portion is connected with pulling pin fixed block, is protruding with pulling pin in the pulling pin fixed block, in the lateral electric cylinders movement, described in triggering
Pulling pin draws the insurance pull ring for removing the body.
2. the long-range jettison device of unmanned plane carry hand-throw type grenade according to claim 1, pinking bullet, feature exist
In, one end that the latch segment is connect with the pull ring clamp mechanism has connection bump, and, the pull ring clamp mechanism includes connecting
Bar, rotation axis, rotating shaft base, linking arm and connecting shaft, the connecting rod are rotatably connected on the rotation axis by the rotation axis
On seat, one end of the connecting rod and the connection bump respectively run through a connecting shaft, the corresponding both ends difference of two connecting shafts
It is connected by a linking arm, the other end of the connecting rod is tilted to be connect with the piston rod of longitudinal electric cylinders.
3. the long-range jettison device of unmanned plane carry hand-throw type grenade according to claim 1, pinking bullet, feature exist
In the quantity of the trigger mechanism that drops a bomb is two sets, and shares the fixed frame that drops a bomb, two sets of trigger mechanism reverse symmetries of dropping a bomb
The two sides of the fixed frame that drops a bomb are set.
4. the long-range jettison device of unmanned plane carry hand-throw type grenade according to claim 1, pinking bullet, feature exist
In, the carry platform include battery supporting plate, it is the carry base for being hinged on by the first articulated shaft the battery supporting plate bottom, logical
It crosses the second hinged axial symmetry and is hinged on that the clamping mechanism of the battery supporting plate two sides, to be symmetrically connected to the battery supporting plate two sides tight
The angle adjustment arm of the adjacent clamping mechanism, is arranged described trapezoidal the trapezoidal grafting block for being connected to carry base bottom
The spring retaining mechanism of grafting block front end and the trapezoidal plug socket for being connected to the trapezoidal grafting block bottom.
5. the long-range jettison device of unmanned plane carry hand-throw type grenade according to claim 4, pinking bullet, feature exist
In being opened up on the battery supporting plate there are two lightening hole, be respectively provided with two connection shaft seats in the two sides of the battery supporting plate
With two engaging lugs, two connection shaft seats are symmetrically fixedly connected below battery supporting plate side, and first articulated shaft passes through
Two connection shaft seats are hinged by the battery supporting plate and the carry base, are machined with hinge hole respectively on two engaging lugs,
Second articulated shaft is hinged by the clamping mechanism and the battery supporting plate by the hinge hole, on two engaging lugs also
It is provided with the limited block for limiting gyration on the clamping mechanism.
6. the long-range jettison device of unmanned plane carry hand-throw type grenade according to claim 4, pinking bullet, feature exist
In being opened up on the carry base there are two lightening hole, be threaded hole respectively in two sides of the carry base;
The clamping mechanism includes the clamp hinged with the battery supporting plate and is connect by fast-assembling bolt with the clamp dynamic
Two blocked holes are formed after folder, the clamp and the dynamic folder connection, is machined with and subtracts respectively in the clamp and the dynamic folder
Repeated hole;
The angle adjustment arm is arc-shaped flaky structure, and an arc adjustment hole, the angle are provided in the angle adjustment arm
Degree regulating arm is fixedly connected by fixing bolt with the battery supporting plate, and an adjusting lock is provided in the arc adjustment hole
Determine bolt, described one end for adjusting locking bolt is threadedly coupled with the threaded hole of the carry base.
7. the long-range jettison device of unmanned plane carry hand-throw type grenade according to claim 4, pinking bullet, feature exist
It is connected by screw in, the trapezoidal grafting block in the bottom of the carry base, the front end of the trapezoidal grafting block has the
One protrusion, offers the mounting hole for installing the spring retaining mechanism, the trapezoidal grafting block in first protrusion
Two sides be the inclined surface being symmetrically inclined outwardly.
8. the long-range jettison device of unmanned plane carry hand-throw type grenade according to claim 7, pinking bullet, feature exist
In offering the connecting hole of fixed frame of dropping a bomb described in connection on the trapezoidal plug socket, processed on the trapezoidal plug socket
There is the trapezoidal inserting groove to match with the trapezoidal grafting block, the front end of the trapezoidal plug socket has the second protrusion, described
It is machined with locking slot corresponding with the position of mounting hole in second protrusion, is fixedly connected with below the carry base
For playing the block of position-limiting action after the trapezoidal plug socket is inserted into the trapezoidal grafting block.
9. the long-range jettison device of unmanned plane carry hand-throw type grenade according to claim 8, pinking bullet, feature exist
In the spring retaining mechanism includes spring locking plug and pull ring, and the pull ring is fixedly connected on the spring locking plug
Top, the bottom of the spring locking plug passes through the mounting hole and is caught in the locking slot.
Priority Applications (1)
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CN201811069760.2A CN108928489B (en) | 2018-09-13 | 2018-09-13 | Remote throwing device for carrying hand throwing grenade and knocking grenade by unmanned aerial vehicle |
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CN201811069760.2A CN108928489B (en) | 2018-09-13 | 2018-09-13 | Remote throwing device for carrying hand throwing grenade and knocking grenade by unmanned aerial vehicle |
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CN108928489B CN108928489B (en) | 2023-07-14 |
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CN111114786A (en) * | 2020-01-14 | 2020-05-08 | 吉林省翼启飞科技有限公司 | Grenade and grenade throwing device |
RU2733904C1 (en) * | 2019-07-02 | 2020-10-08 | Федеральное государственное казенное военное образовательное учреждение высшего образования "ВОЕННАЯ АКАДЕМИЯ МАТЕРИАЛЬНО-ТЕХНИЧЕСКОГО ОБЕСПЕЧЕНИЯ имени генерала армии А.В. Хрулева" Министерства обороны Российской Федерации | Suspension for delivery of ammunition mounted on drone and method of use thereof |
CN111824421A (en) * | 2020-06-15 | 2020-10-27 | 成都大学 | A anti-riot bullet shooting mechanism and bullet shooting device for unmanned aerial vehicle |
CN112027089A (en) * | 2020-08-21 | 2020-12-04 | 成都智巡科技有限责任公司 | Unmanned aerial vehicle device of throwing ammunition |
CN113184190A (en) * | 2021-06-11 | 2021-07-30 | 北京亿舱科技有限公司 | Automatic grenade throwing device carried by unmanned aerial vehicle |
CN113247262A (en) * | 2021-07-05 | 2021-08-13 | 天津天羿科技有限公司 | Multipurpose aircraft |
CN113804068A (en) * | 2021-10-25 | 2021-12-17 | 中国人民武装警察部队工程大学 | Device capable of remotely controlling detonation of torpedoes of various types and detonation method |
RU2815127C1 (en) * | 2023-03-28 | 2024-03-11 | Анатолий Михайлович Криштоп | Hybrid reconnaissance and strike unmanned aerial vehicle (hrsuav), device for counteracting projectiles of surface-to-air missile systems with thermal guidance heads (dcpsamstgh) for hrsuav and method of operation of hrsuav with dcpsamstgh |
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