CN206511136U - A kind of assisted unmanned plane launcher - Google Patents
A kind of assisted unmanned plane launcher Download PDFInfo
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- CN206511136U CN206511136U CN201621393764.2U CN201621393764U CN206511136U CN 206511136 U CN206511136 U CN 206511136U CN 201621393764 U CN201621393764 U CN 201621393764U CN 206511136 U CN206511136 U CN 206511136U
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- bearing
- sliding rail
- unmanned plane
- rail rack
- pitching
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Abstract
The utility model discloses a kind of assisted unmanned plane launcher, belong to field of aerospace technology.Including：Mounting seat, sliding rail rack component, installation baffle plate, blocking device and pitching lowering or hoisting gear；Mounting seat is made up of the bikini cylinder load-bearing frame, the second bearing and two the first bearings of steel-pipe welding, and load-bearing frame is by the second bearing and the first seat supports on ground or mounting surface；Sliding rail rack component is made up of sliding rail rack, slide rail, stopping means；The upper end that sliding rail rack one end is provided with the first bearing with load-bearing frame is hinged, and the bottom that the other end is provided with the second bearing by pitching lowering or hoisting gear and load-bearing frame is hinged, and sliding rail rack component can adjust its luffing angle by pitching lowering or hoisting gear；The tail end that baffle plate is fixed on sliding rail rack component is installed, blocking device is fixed on the lower section of sliding rail rack component, and unmanned plane is fixed on by its rear slider on the stopping means of sliding rail rack component, and is locked by the blocking device.
Description
Technical field
The utility model belongs to field of aerospace technology, and in particular to a kind of assisted unmanned plane launcher.
Background technology
The radiation pattern of current unmanned plane can be divided into：Rolling start, catapult-assisted take-off, rocket assist transmitting, hand throw transmitting, sky
It is middle to deliver and take off vertically；
In rocket assist emission process, the kinetic energy that unmanned plane takes off comes from rocket booster produced by the burning of fuel
Energy.Rocket assist transmitting mode have the advantage that for whole emitter take it is local smaller, cost is relatively low, by
It is smaller to external influence, can be disposed with faster speed etc.；Unmanned plane rocket assist launch mode, due to technology
Maturation, using maneuverability, the limitation in non-emissive place, thus countries in the world application all than wide.
Unmanned plane flies to disengaging guide rail from along guide rail process when launching is the first stage taken off, and studies this stage
The research to whole unmanned plane emission process of radiation pattern and emission parameter have great significance.
Utility model content
The purpose of this utility model：In order to solve the above problems, the utility model proposes a kind of assisted unmanned plane hair
Frame is penetrated, its radiation pattern is largely consumed in the rolling start stage to launching occasion without particular/special requirement, and avoiding Fuel On Board.
The technical solution of the utility model：A kind of assisted unmanned plane launcher, including：Mounting seat, sliding rail rack group
Part, installation baffle plate, blocking device and pitching lowering or hoisting gear；
The mounting seat by steel-pipe welding bikini cylinder load-bearing frame, the second bearing and two the first bearings
Composition, the load-bearing frame is by second bearing and first seat supports on ground or mounting surface；
The sliding rail rack component is made up of sliding rail rack, slide rail and stopping means；
The upper end that described sliding rail rack one end is provided with the first bearing with the load-bearing frame is hinged, and the other end passes through described
The bottom that pitching lowering or hoisting gear is provided with the second bearing with the load-bearing frame is hinged, and the sliding rail rack component passes through pitching liter
Falling unit can adjust its luffing angle；
Described to install the tail end that baffle plate is fixed on the sliding rail rack component, the blocking device is fixed on the slide rail branch
The lower section of frame component, unmanned plane is fixed on by its rear slider on the stopping means of sliding rail rack component, and passes through the locking
Device is locked.
Preferably, first bearing and second bearing are provided with disk and first bearing is provided with leveling spiral shell
Bar.
Preferably, the pitching lowering or hoisting gear is made up of handwheel, bevel gear and T-shaped screw rod, and the handwheel passes through bevel gear
It is connected with the T-shaped screw rod.
Preferably, the blocking device adjusts spiral shell by latch hook, pedestal, pull bar, handle, spring, the first rocking arm, the second rocking arm
Mother's composition；
The spring is arranged on pull bar, and one end of the pull bar is connected through pedestal with handle, the handle and described
Adjusting nut is provided between pedestal；The other end of the pull bar is connected by the first rocking arm with latch hook, and the latch hook activity is even
It is connected on the pedestal, first rocking arm and pull bar are arranged on the pedestal by the second rocking arm.
Preferably, described pull bar one end is provided with boss, and the spring is arranged between the boss and the pedestal.
Preferably, the unmanned plane rear slider is provided with stopper slot, and the stopper slot coordinates with the latch hook.
Preferably, the slide rail is made using rectangle steel square tube section, and the stopping means is arranged on inside the slide rail
And the slide rail bottom coordinates fluting with the latch hook.
Technique effect of the present utility model：The utility model can effectively solve high-speed unmanned aerial vehicle take off landing place limitation
Problem, improves the sinking speed that takes off, unmanned plane is rapidly entered high-speed flight state.
Brief description of the drawings
Fig. 1 is a kind of structure composition schematic diagram of a preferred embodiment of boosting unmanned plane launcher of the utility model；
Fig. 2 is the first seat structure schematic diagram of embodiment illustrated in fig. 1；
Fig. 3 is the pitching lifting device structure schematic diagram of embodiment illustrated in fig. 1；
Fig. 4 is the blocking device structural representation of embodiment illustrated in fig. 1；
Fig. 5 is the top view of the blocking device of embodiment illustrated in fig. 1；
Fig. 6 is in the lock state schematic diagram for the rear slider of embodiment illustrated in fig. 1.
Wherein, 1- mounting seats, 2- sliding rail rack components, 3- installation baffle plates, 4- blocking devices, 5- pitching lowering or hoisting gears,
6- rear sliders, 11- load-bearing frames, the bearings of 12- second, the bearings of 13- first, 14- disks, 15- linkage levelling screws, 21- slide rail branch
Frame, 22- slide rails, 23- stopping means, 41- latch hooks, 42- pedestals, 43- pull bars, 44- handles, 45- springs, the rocking arms of 46- first,
The rocking arms of 47- second, 48- adjusting nuts, 51- handwheels, 52- bevel gears, 53-T type screw rods.
Embodiment
To make the purpose, technical scheme and advantage of the utility model implementation clearer, below in conjunction with the utility model
Accompanying drawing in embodiment, the technical scheme in the utility model embodiment is further described in more detail.In the accompanying drawings, from beginning
Same or similar element or element with same or like function are represented to same or similar label eventually.Described reality
It is a part of embodiment of the utility model to apply example, rather than whole embodiments.The embodiment described below with reference to accompanying drawing
It is exemplary, it is intended to for explaining the utility model, and it is not intended that to limitation of the present utility model.It is new based on this practicality
Embodiment in type, the every other implementation that those of ordinary skill in the art are obtained under the premise of creative work is not made
Example, belongs to the scope of the utility model protection.Embodiment of the present utility model is described in detail below in conjunction with the accompanying drawings.
In description of the present utility model, it is to be understood that term " " center ", " longitudinal direction ", " transverse direction ", "front", "rear",
The orientation or position relationship of the instruction such as "left", "right", " vertical ", " level ", " top ", " bottom " " interior ", " outer " is based on accompanying drawing institutes
The orientation or position relationship shown, is for only for ease of description the utility model and simplifies description, rather than indicate or imply and be signified
Device or element must have specific orientation, with specific azimuth configuration and operation, therefore it is not intended that to this practicality
The limitation of novel protected scope.
Embodiment of the present utility model is described in detail below in conjunction with the accompanying drawings, Fig. 1 is referred to Fig. 6；
A kind of assisted unmanned plane launcher, including：Mounting seat 1, sliding rail rack component 2, installation baffle plate 3, locking dress
Put 4 and pitching lowering or hoisting gear 5；
Mounting seat 1 is by the bikini cylinder load-bearing frame 11 of steel-pipe welding, the second bearing 12 and two first
Seat 13 is constituted, the first bearing 13 and the second bearing 12 is provided with disk 14 and the first bearing 13 is provided with linkage levelling screw 15, load
Framework 11 is supported on ground or mounting surface by the disk 14 of the second bearing 12 and the first bearing 13；In view of launcher
Fixed surface evenness is installed bad, the second bearing 12 is designed as uncontrollable stationary structure, and 2 are symmetrically arranged
First bearing 13 adjusts launcher rearward height to meet the fixed Level-adjusting of launcher installation by linkage levelling screw 15
It is required that.
Sliding rail rack component 2 is made up of sliding rail rack 21, slide rail 22, stopping means 23；Sliding rail rack component 2 uses section
Frame structure is welded into for rectangle steel square tube section, the stopping means 23 of the rear end of sliding rail rack 21 is fixed on the medial surface of slide rail 22
On, the stopping means 23 of the front end of sliding rail rack 21 is arranged on the front elevational sectional of slide rail 22, the one end of sliding rail rack 21 and load frame
One end that frame 11 is provided with the first bearing 13 is hinged, and the other end is provided with second by pitching lowering or hoisting gear 5 and load-bearing frame 11
The journal stirrup of the bottom of bearing 12 is hinged, under the effect of pitching lowering or hoisting gear 5, and sliding rail rack component 2 is overall will be around the second bearing
The axis rotation of 12 two, top journal stirrup, realizes the adjustment of the angle of departure.
The level of launcher and the conversion of emission state realize that pitching lowering or hoisting gear 5 is by hand by pitching lowering or hoisting gear 5
Wheel 51, bevel gear 52 and T-shaped screw rod 53 are constituted, and handwheel 51 is connected by bevel gear 52 with T-shaped screw rod 53；The pitching lowering or hoisting gear
5 by manually operating handwheel 51, and the combination of driving bevel gear 52 and T-shaped screw rod 53 realizes that rectilinear path is adjusted, the actuator travel
The angle of departure can be met to adjust between 0~20 °.
The effect of blocking device 4 is that unmanned plane is reliably latched in into launcher when unmanned plane turbojet engine works
On.The blocking force design of single blocking device is slightly larger than 2 times of unmanned vehicle engine maximum thrust, you can safety interlocking nobody
Machine.After rocket firing, blocking device can be unlocked smoothly.Blocking device 4 uses the unidirectional blocking mechanism pattern of hinge type, closes
Locking device is by latch hook 41, pedestal 42, pull bar 43, handle 44, spring 45, the first Rocker arm 46, the second Rocker arm 47 and adjusting nut 48
Composition；
The one end of pull bar 43 is provided with boss, and spring 45 is arranged between boss and pedestal 42, and one end of pull bar 43 passes through base
Seat 42 is connected with handle 44, and adjusting nut 48 is provided between handle 44 and pedestal 42；The other end of pull bar 43 shakes by first
Arm 46 is connected with latch hook 41, and latch hook 41 is movably connected on pedestal 42, and the first Rocker arm 46 and pull bar 43 are pacified by the second Rocker arm 47
On pedestal 42, by the installation site of adjusting nut 48, so that the pretightning force of spring 45 is adjusted, the pretension of general spring 45
Power size is arranged between 500N-5000N.
Rocket launcher is fixed on the tail end of sliding rail rack component 2 by installing baffle plate 3, and blocking device is fixed on slide rail branch
The lower section of frame component 2, stopping means 23 is arranged on the inside of slide rail 22 and the bottom of slide rail 22 coordinates after fluting, unmanned plane with latch hook 41
Sliding block 6 is provided with stopper slot, and stopper slot coordinates with latch hook 41, and unmanned plane is fixed on sliding rail rack component by its rear slider 6
On stopping means 23, and locked by blocking device.
When unmanned plane need to be installed to launcher, load unmanned plane from the front of slide rail 22, unmanned plane is transported backward along slide rail 22
It is dynamic, the anterior inclined-plane of the latch hook 41 of blocking mechanism is depressed by rear slider 6, latch hook 41 enters the bottom surface stopper slot of rear slider 6, locking
The stopping means 23 of device blocks unmanned plane and moved further back, now as blocking.Now blocking device by nobody
Machine is latched on slide rail 2 securely.After rocket firing, when being more than blocking force along slide rail direction thrust, latch hook 41 rotates
And by hinge by spring-compressed, blocking mechanism is opened, and unmanned plane is skidded off along slide rail.
Unmanned plane in blocking need to only be closed if necessary to be removed from launcher from slide rail rear portion pull handle 44
The latch hook 41 of locking device is expansible, and unmanned plane can overstep the limit along the forward slip of slide rail 2.
It is last it is to be noted that：Above example is only limited to illustrate the technical solution of the utility model, rather than to it
System.Although the utility model is described in detail with reference to the foregoing embodiments, one of ordinary skill in the art should manage
Solution：It can still be modified to the technical scheme described in foregoing embodiments, or which part technical characteristic is entered
Row equivalent substitution；And these modifications or replacement, the essence of appropriate technical solution is departed from each embodiment of the utility model
The spirit and scope of technical scheme.
Claims (7)
1. a kind of assisted unmanned plane launcher, it is characterised in that including：Mounting seat (1), sliding rail rack component (2), installation
Baffle plate (3), blocking device (4) and pitching lowering or hoisting gear (5)；
The mounting seat (1) is by the bikini cylinder load-bearing frame (11) of steel-pipe welding, the second bearing (12) and two
First bearing (13) is constituted, and the load-bearing frame (11) is supported in by second bearing (12) and first bearing (13)
On ground or mounting surface；
The sliding rail rack component (2) is made up of sliding rail rack (21), slide rail (22), stopping means (23)；
The upper end that described sliding rail rack (21) one end is provided with the first bearing (13) with the load-bearing frame (11) is hinged, the other end
The bottom for being provided with the second bearing (12) with the load-bearing frame (11) by the pitching lowering or hoisting gear (5) is hinged, the cunning
Rail bracket component (2) can adjust its luffing angle by pitching lowering or hoisting gear (5)；
Described to install the tail end that baffle plate (3) is fixed on the sliding rail rack component (2), the blocking device (4) is fixed on described
The lower section of sliding rail rack component (2), unmanned plane is fixed on the stopping means of sliding rail rack component (23) by its rear slider, and
Locked by the blocking device (4).
2. a kind of assisted unmanned plane launcher according to claim 1, it is characterised in that：First bearing (13) and
Second bearing (12) is provided with disk (14) and first bearing (13) is provided with linkage levelling screw (15).
3. a kind of assisted unmanned plane launcher according to claim 1, it is characterised in that：The pitching lowering or hoisting gear
(5) be made up of handwheel (51), bevel gear (52) and T-shaped screw rod (53), the handwheel (51) by bevel gear (52) with it is described T-shaped
Screw rod (53) is connected.
4. a kind of assisted unmanned plane launcher according to claim 1, it is characterised in that：The blocking device (4) by
Latch hook (41), pedestal (42), pull bar (43), handle (44), spring (45), the first rocking arm (46), the second rocking arm (47) and regulation
Nut (48) is constituted；
The spring (45) is arranged on pull bar (43), and one end of the pull bar (43) passes through pedestal (42) and handle (44) phase
Even, adjusting nut (48) is provided between the handle (44) and the pedestal (42)；The other end of the pull bar (43) passes through
First rocking arm (46) is connected with latch hook (41), and the latch hook (41) is movably connected on the pedestal (42), first rocking arm
(46) and pull bar (43) by the second rocking arm (47) be arranged on the pedestal (42) on.
5. a kind of assisted unmanned plane launcher according to claim 4, it is characterised in that：Described pull bar (43) one end is set
Boss is equipped with, the spring (45) is arranged between the boss and the pedestal (42).
6. a kind of assisted unmanned plane launcher according to claim 4, it is characterised in that：The unmanned plane rear slider is set
Stopper slot is equipped with, the stopper slot coordinates with the latch hook (41).
7. a kind of assisted unmanned plane launcher according to claim 4, it is characterised in that：The slide rail (22) uses square
Shape steel square tube section makes, and the stopping means (23) is arranged on the slide rail (22) inside and slide rail (22) bottom and institute
State latch hook (41) and coordinate fluting.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621393764.2U CN206511136U (en) | 2016-12-19 | 2016-12-19 | A kind of assisted unmanned plane launcher |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621393764.2U CN206511136U (en) | 2016-12-19 | 2016-12-19 | A kind of assisted unmanned plane launcher |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206511136U true CN206511136U (en) | 2017-09-22 |
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ID=59863054
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621393764.2U Active CN206511136U (en) | 2016-12-19 | 2016-12-19 | A kind of assisted unmanned plane launcher |
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| Country | Link |
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| CN (1) | CN206511136U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109850175A (en) * | 2019-03-22 | 2019-06-07 | 绵阳富莱特航空科技有限公司 | A kind of novel emission frame structure |
| CN112644732A (en) * | 2021-01-05 | 2021-04-13 | 徐艳 | Vehicle-mounted multi-rotor unmanned aerial vehicle take-off and landing platform |
| CN113844670A (en) * | 2021-11-09 | 2021-12-28 | 北京航空航天大学 | Disconnect-type folding oil moves duct aircraft and starts platform |
| CN114074765A (en) * | 2020-08-21 | 2022-02-22 | 海鹰航空通用装备有限责任公司 | Interlocking type separating mechanism of box type launching unmanned aerial vehicle and box type launching system |
| CN114894033A (en) * | 2022-04-15 | 2022-08-12 | 中国航空工业集团公司沈阳飞机设计研究所 | Constant overload catapult |
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2016
- 2016-12-19 CN CN201621393764.2U patent/CN206511136U/en active Active
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109850175A (en) * | 2019-03-22 | 2019-06-07 | 绵阳富莱特航空科技有限公司 | A kind of novel emission frame structure |
| CN109850175B (en) * | 2019-03-22 | 2024-03-12 | 绵阳富莱特航空科技有限公司 | Novel transmitting frame structure |
| CN114074765A (en) * | 2020-08-21 | 2022-02-22 | 海鹰航空通用装备有限责任公司 | Interlocking type separating mechanism of box type launching unmanned aerial vehicle and box type launching system |
| CN112644732A (en) * | 2021-01-05 | 2021-04-13 | 徐艳 | Vehicle-mounted multi-rotor unmanned aerial vehicle take-off and landing platform |
| CN113844670A (en) * | 2021-11-09 | 2021-12-28 | 北京航空航天大学 | Disconnect-type folding oil moves duct aircraft and starts platform |
| CN113844670B (en) * | 2021-11-09 | 2023-07-14 | 北京航空航天大学 | Separated foldable oil-driven ducted aircraft starting platform |
| CN114894033A (en) * | 2022-04-15 | 2022-08-12 | 中国航空工业集团公司沈阳飞机设计研究所 | Constant overload catapult |
| CN114894033B (en) * | 2022-04-15 | 2023-05-16 | 中国航空工业集团公司沈阳飞机设计研究所 | Constant overload projectile device |
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