CN205770199U - A kind of SUAV catapult-launching gear - Google Patents
A kind of SUAV catapult-launching gear Download PDFInfo
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- CN205770199U CN205770199U CN201620743192.XU CN201620743192U CN205770199U CN 205770199 U CN205770199 U CN 205770199U CN 201620743192 U CN201620743192 U CN 201620743192U CN 205770199 U CN205770199 U CN 205770199U
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- support component
- props
- wing
- locking
- catapult
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Abstract
The utility model discloses a kind of SUAV catapult-launching gear, comprising: body props up support component, described body props up support component for supporting the body of unmanned plane and installing other parts；Wing props up support component, and described wing props up rear portion one end of support component propping up support component with described body and is connected, and wing props up support component for supporting the wing of unmanned plane；Locking device, described locking device is arranged on described body and props up the front portion of support component, for locking the ejecting hook of unmanned plane before take-off；Ejection switch, described ejection switch is for controlling the folding condition of described locking device；Level indicator, described level indicator is arranged on described body and props up the upper surface of support component.This utility model SUAV catapult-launching gear carries convenient, simple to operation so that unmanned plane launcher reliability is higher.In addition function is more various, convenient uses in Mini-Unmanned Aerial Vehicles, have lightweight, volume is little, advantages of simple structure and simple.
Description
Technical field
This utility model belongs to unmanned plane lift-off technology field, particularly relates to a kind of SUAV catapult-launching gear.
Background technology
Unmanned plane at present taking photo by plane, agricultural, plant protection, auto heterodyne, express transportation, disaster relief, observation wild animal, monitoring pass
Catch an illness, survey and draw, news report, electric inspection process, the disaster relief, movies-making etc. field are the most increasingly widely applied.By
The highest in the cost of unmanned plane, user and businessman are intended to unmanned plane and less accident occur.
Unmanned plane has an accident and is mainly to occur at takeoff phase, carries out rising of unmanned plane by support launcher
Fly, the launching success rate of unmanned plane can well be improved.Ejection mechanism utilizes what system stored energy in advance quickly to discharge reality
Now the moment launching object is accelerated, be widely used in modern military and general industry, such as catapult-assisted take-off, the guided missile of aircraft carrier
Ejection launch, ejection escape seat, vehicle impact testing etc..The Main Function of shot support is that aircraft accelerates to critical speed
Degree, is that aircraft is obtained in that enough initial velocity break away from the launching apparatus of gravity flight.Catapult-launching gear has many types, has steam
Launch, rubber band launches, electromagnetic launch and rocket-assisted ejection etc..But existing ejection mechanism structure is complicated, price is held high
Expensive, it is difficult to be applicable to middle-size and small-size unmanned plane.
Utility model content
The purpose of this utility model is to provide a kind of SUAV catapult-launching gear, to solve existing ejection mechanism structure
Complicated, expensive, it is difficult to the problem being applicable to middle-size and small-size unmanned plane.
To achieve these goals, this utility model provides a kind of SUAV catapult-launching gear, comprising:
Body props up support component, and described body props up support component for supporting the body of unmanned plane and installing other parts；
Wing props up support component, and described wing props up rear portion one end of support component propping up support component with described body and is connected, wing
Prop up support component for supporting the wing of unmanned plane；
Locking device, described locking device is arranged on described body and props up the front portion of support component, for locking nothing before take-off
Man-machine ejecting hook；
Ejection switch, described ejection switch is for controlling the folding condition of described locking device；
Level indicator, described level indicator is arranged on described body and props up the upper surface of support component.
This utility model SUAV as above catapult-launching gear, further, described wing props up support component and body
Propping up and be articulated and connected between support component, wing props up support component and is folded up when not in use.
This utility model SUAV as above catapult-launching gear, further, described wing props up support component and includes folding
Folded bar and wing bracing frame；Described wing bracing frame is arranged on folding rod；Folding rod and body prop up hinged company between support component
Connect.
This utility model SUAV as above catapult-launching gear, further, described locking device includes locking rack,
Locking pivot pin and return spring；Locking rack is arranged on body and props up the forward position of support component, and locking rack is provided with and launches for receiving
The groove of hook；Locking bearing pin is arranged on locking rack, with at groove location locking ejecting hook or release ejecting hook；Return
Spring is used for making locking bearing pin return；Described ejection switch includes control handle and power transmission steel wire rope；Described power transmission steel wire rope is even
It is connected between control handle and locking bearing pin.
This utility model SUAV as above catapult-launching gear, further, described control handle is arranged on wing
Prop up on the folding rod of support component, be positioned at the top of wing bracing frame.
This utility model SUAV as above catapult-launching gear, further, also includes pressure transducer, display
And power supply, described power supply is pressure transducer and monitor power supply, and the pressure value information that described pressure transducer senses passes
Pass display, display show in real time；The locking rack of described locking device is connected to body by slide rail and props up support component
Forward position；Locking rack afterbody is provided with dowel steel, and pulling force is passed to pressure transducer by dowel steel.
The beneficial effects of the utility model are:
This utility model SUAV catapult-launching gear carries convenient, simple to operation, for unfamiliar use
Family equally accomplishes that left-hand seat i.e. can so that unmanned plane launcher reliability is higher, increases the stability in ejection process.This external work
Can be more various, convenient use in Mini-Unmanned Aerial Vehicles, have lightweight, volume is little, advantages of simple structure and simple.
Accompanying drawing explanation
By the detailed description made in conjunction with the following drawings, of the present utility model above-mentioned and/or other aspects and advantage will
Becoming more apparent upon and be easier to understand, these accompanying drawings the most schematically, are not limiting as this utility model, wherein:
Fig. 1 is the first view of the SUAV catapult-launching gear of a kind of embodiment of this utility model；
Fig. 2 is the second view of the SUAV catapult-launching gear of a kind of embodiment of this utility model；
Fig. 3 is the three-view diagram of the SUAV catapult-launching gear of a kind of embodiment of this utility model；
Fig. 4 is the 4th view of the SUAV catapult-launching gear of a kind of embodiment of this utility model；
Fig. 5 is that the wing of SUAV catapult-launching gear supports modular support wing view；
Fig. 6 is that the body of SUAV catapult-launching gear supports modular support fuselage state schematic diagram；
Fig. 7 is locking device and the pressure transducer assembly relation schematic diagram of SUAV catapult-launching gear.
In accompanying drawing, the list of parts representated by each label is as follows:
1, body props up support component, 2, wing prop up support component, 21, folding rod, 22, wing bracing frame, 3, locking device, 31,
Locking rack, 32, locking pivot pin, 33, return spring, 34, power transmission steel wire rope, 35, for accommodating the groove of ejecting hook, 36, sliding
Rail, 37, dowel steel, 4, ejection switch, 5, level indicator, 6, pressure transducer, 7, display, 8, power supply, 9, the body of unmanned plane,
10, the wing of unmanned plane, 11, ejecting hook, 100, SUAV catapult-launching gear.
Detailed description of the invention
Hereinafter, the embodiment of SUAV catapult-launching gear of the present utility model is described with reference to the accompanying drawings.
The embodiment recorded at this is specific detailed description of the invention of the present utility model, is used for illustrating of the present utility model
Design, is all explanatory and exemplary, should not be construed as this utility model embodiment and the limit of this utility model scope
System.In addition to the embodiment recorded at this, those skilled in the art can also be public based on the application claims and description institute
The content opened uses other technical scheme obvious, and these technical schemes include using doing the embodiment recorded at this
Go out the technical scheme of any obvious substitutions and modifications.
The accompanying drawing of this specification is schematic diagram, aids in illustrating design of the present utility model, it is schematically indicated each several part
Shape and mutual relation thereof.Note that the structure of each parts for the ease of clearly showing this utility model embodiment, respectively
Do not draw according to identical ratio between accompanying drawing.Identical reference marker is used for representing identical part.
Fig. 1 illustrates the SUAV catapult-launching gear 100 of a kind of embodiment of this utility model, comprising:
Body props up support component 1, and described body props up support component 1 for supporting the body 9 of unmanned plane and installing other parts；
In the embodiment show in figure 1, body props up support component and includes upper plate and lower plate, is connected by pillar between upper plate and lower plate.?
Forming the cavity identical with strut height between upper plate and lower plate, described cavity is easily installed other parts, additionally, this knot
Structure can reduce the overall weight of launching cradle.
Wing props up support component 2, and described wing props up rear portion one end of support component 2 propping up support component 1 with described body and is connected, machine
The wing props up support component 2 for supporting the wing 10 of unmanned plane；
Locking device 3, described locking device 3 is arranged on described body and props up the front portion of support component 1, for locking before take-off
The ejecting hook 11 of unmanned plane；
Ejection switch 4, described ejection switch is for controlling the folding condition of described locking device 3；
Level indicator 5, as in figure 2 it is shown, described level indicator 5 is arranged on described body props up the upper surface of support component 1.Level indicator
Effect is to adjust the inclination angle that unmanned plane takes off, and beneficially unmanned plane takes off smoothly.
This utility model SUAV catapult-launching gear carries convenient, simple to operation, for unfamiliar use
Family equally accomplishes that left-hand seat i.e. can；Using both hands hand-held launching cradle mode, emission process is relatively reliable, reduces the accident launched
Rate；In addition function is more various, can be as launching the launching cradle of unmanned plane, again can be as reclaiming the reel that launch rubber band, side
Just in Mini-Unmanned Aerial Vehicles use, have lightweight, volume is little, advantages of simple structure and simple.
In the SUAV catapult-launching gear of this utility model above-described embodiment, do not using for the ease of catapult-launching gear
Time portability, can improve further below, described wing props up support component 2 and body props up hinged company between support component 1
Connecing, wing props up support component 2 and is folded up when not in use.As it is shown in figure 1, described wing props up support component 2 includes folding rod 21
With wing bracing frame 22；Described wing bracing frame 22 is arranged on folding rod 21；Folding rod 21 and body prop up and cut with scissors between support component 1
Connect in succession.
In the SUAV catapult-launching gear of this utility model above-described embodiment, as it is shown in fig. 7, described locking device 3
Including locking rack 31, locking pivot pin 32 and return spring 33；Locking rack 31 is arranged on body and props up the forward position of support component 1, lock
Tight frame 31 is provided with the groove 35 for accommodating ejecting hook；Locking bearing pin 32 is arranged on locking rack 31, is existed by locking bearing pin
The mobile realization locking ejecting hook 11 of groove 35 position or release ejecting hook 11；Return spring 33 is used for making locking bearing pin 32
Return, in the embodiment show in figure 7, return spring is arranged on the afterbody of locking bearing pin, provides one to the left to locking bearing pin
To returning elastic；Described ejection switch includes control handle 4 and power transmission steel wire rope 34；Described power transmission steel wire rope 34 is connected to control
Between handle 4 processed and locking bearing pin 32.As shown in Figure 1 and Figure 4, described control handle peace 4 is contained in wing and props up the folding of support component 2
On bar 21, it is positioned at the top of wing bracing frame 22.
In the SUAV catapult-launching gear of this utility model above-described embodiment, the elastic force that unmanned plane takes off required needs
Being greater than a certain fixed value, but this elastic force numerical value is difficult to grasp by the personal experience of operator, the success rate taken off is relatively low.
In order to improve the success rate that unmanned aerial vehicle ejecting takes off, improvement further to above-described embodiment, as shown in Fig. 3, Fig. 4 and Fig. 7, small-sized
Unmanned aerial vehicle ejecting device also includes pressure transducer 6, display 7 and power supply 8, and described power supply 8 is pressure transducer 6 and display
7 power supplies, the pressure value information that described pressure transducer 6 senses passes to display 7, display 7 shows in real time；Described
The locking rack 31 of locking device 3 is connected to body by slide rail 36 and props up the forward position of support component 1；Locking rack 36 afterbody is provided with biography
Power bar 37, pulling force is passed to pressure transducer 6 by dowel steel 37.
The use process of this utility model above-mentioned SUAV catapult-launching gear is as follows:
Step 1, the unmanned plane being provided with ejecting hook installs rear (Fig. 5 and Fig. 6) in place with catapult-launching gear, by rubber band
One end is fixed, and the ejecting hook of unmanned plane is fixed and is locked in locking device, then pulls launching cradle afterburning to rubber band,
Rubber band is enable to provide enough energy so that unmanned plane reaches critical velocity and takes off to unmanned plane；
Step 2, hand-held launching cradle, control the unmanned plane take-off angle of attack by level indicator；
Step 3, when release, is opened locking device by ejection switch, the ejecting hook of unmanned plane and locking device
Unclamp, discharge unmanned plane；
Step 4, launches rubber band and drives unmanned plane to arrive the flight speed required for aircraft, launches rubber band disengaging simultaneously and launches
Hook, unmanned plane continues flight by self power, completes the takeoff maneuver of unmanned plane.
For the SUAV takeoff method of this utility model above-described embodiment, pressure transducer is installed utilizing and shows
When showing the SUAV catapult-launching gear of device, after pulling launching cradle to rubber band reinforcing, the pulling force shown in real time by display
Numerical value determines whether to pull and puts in place.
For the SUAV takeoff method of this utility model above-described embodiment, complete after unmanned aerial vehicle ejecting takes off,
Also include supporting wing the step that member collapses is packed up.
Each technical characteristic of above-mentioned disclosure is not limited to disclosed and further feature combination, and those skilled in the art are also
Other combination between each technical characteristic can be carried out according to the purpose of utility model, be as the criterion realizing the purpose of this utility model.
Claims (6)
1. a SUAV catapult-launching gear, it is characterised in that including:
Body props up support component, and described body props up support component for supporting the body of unmanned plane and installing other parts；
Wing props up support component, and described wing props up rear portion one end of support component propping up support component with described body and is connected, and wing supports
Assembly is for supporting the wing of unmanned plane；
Locking device, described locking device is arranged on described body and props up the front portion of support component, for locking unmanned plane before take-off
Ejecting hook；
Ejection switch, described ejection switch is for controlling the folding condition of described locking device；
Level indicator, described level indicator is arranged on described body and props up the upper surface of support component.
SUAV catapult-launching gear the most according to claim 1, it is characterised in that described wing props up support component and body
Propping up and be articulated and connected between support component, wing props up support component and is folded up when not in use.
SUAV catapult-launching gear the most according to claim 1, it is characterised in that described wing props up support component and includes folding
Folded bar and wing bracing frame；Described wing bracing frame is arranged on folding rod；Folding rod and body prop up hinged company between support component
Connect.
SUAV catapult-launching gear the most according to claim 3, it is characterised in that described locking device includes locking
Frame, locking pivot pin and return spring；Locking rack is arranged on body and props up the forward position of support component, and locking rack is provided with for accommodating bullet
Penetrate the groove of hook；Locking bearing pin is arranged on locking rack, with at groove location locking ejecting hook or release ejecting hook；Return
Position spring is used for making locking bearing pin return；Described ejection switch includes control handle and power transmission steel wire rope；Described power transmission steel wire rope
It is connected between control handle and locking bearing pin.
SUAV catapult-launching gear the most according to claim 4, it is characterised in that described control handle is arranged on wing
Prop up on the folding rod of support component, be positioned at the top of wing bracing frame.
SUAV catapult-launching gear the most according to claim 1, it is characterised in that also include pressure transducer, display
Device and power supply, described power supply is pressure transducer and monitor power supply, the pressure value information that described pressure transducer senses
Pass to display, display show in real time；The locking rack of described locking device is connected to body by slide rail and props up support component
Forward position；Locking rack afterbody is provided with dowel steel, and pulling force is passed to pressure transducer by dowel steel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620743192.XU CN205770199U (en) | 2016-07-15 | 2016-07-15 | A kind of SUAV catapult-launching gear |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620743192.XU CN205770199U (en) | 2016-07-15 | 2016-07-15 | A kind of SUAV catapult-launching gear |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205770199U true CN205770199U (en) | 2016-12-07 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620743192.XU Withdrawn - After Issue CN205770199U (en) | 2016-07-15 | 2016-07-15 | A kind of SUAV catapult-launching gear |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205770199U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106114890A (en) * | 2016-07-15 | 2016-11-16 | 天峋（常州）智能科技有限公司 | A kind of SUAV catapult-launching gear and unmanned plane takeoff method |
| WO2019079931A1 (en) * | 2017-10-23 | 2019-05-02 | 大连理工大学 | Small underwater launcher capable of floating on water for unmanned aerial vehicle |
-
2016
- 2016-07-15 CN CN201620743192.XU patent/CN205770199U/en not_active Withdrawn - After Issue
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106114890A (en) * | 2016-07-15 | 2016-11-16 | 天峋（常州）智能科技有限公司 | A kind of SUAV catapult-launching gear and unmanned plane takeoff method |
| CN106114890B (en) * | 2016-07-15 | 2019-04-02 | 天峋（常州）智能科技有限公司 | A kind of small drone catapult-launching gear and unmanned plane takeoff method |
| WO2019079931A1 (en) * | 2017-10-23 | 2019-05-02 | 大连理工大学 | Small underwater launcher capable of floating on water for unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20180930 Address after: 214400 3 creative street, 8 Binjiang West Road, Jiangyin, Jiangsu. Patentee after: Jiangyin Tian Xun Technology Development Co., Ltd. Address before: 213000 west of Jiangsu science and technology center, A, 18, Changwu Road, Wujin, Changzhou. Patentee before: Day I (Changzhou) Technology Co. Ltd. |
|
| TR01 | Transfer of patent right | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20161207 Effective date of abandoning: 20190402 |
|
| AV01 | Patent right actively abandoned |