CN207523957U - A kind of intermediate range unmanned aerial vehicle ejecting frame - Google Patents
A kind of intermediate range unmanned aerial vehicle ejecting frame Download PDFInfo
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- CN207523957U CN207523957U CN201721267552.4U CN201721267552U CN207523957U CN 207523957 U CN207523957 U CN 207523957U CN 201721267552 U CN201721267552 U CN 201721267552U CN 207523957 U CN207523957 U CN 207523957U
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- aerial vehicle
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Abstract
The utility model discloses a kind of intermediate range unmanned aerial vehicle ejecting framves, including a kind of intermediate range unmanned aerial vehicle ejecting frame, including ejection frame body and controller, the ejection frame body is internally provided with damping filling plate, the lower end of the ejection frame body is equipped with absorption type supporting leg, the both sides of the absorption type supporting leg are equipped with damping spring, the upper end of the ejection frame body is equipped with hydraulic pressure lifting device, the upper end of the hydraulic pressure lifting device is equipped with emitter, the upper end of the emitter is equipped with brute spring, and the outer surface of the emitter is equipped with handle slideway.A kind of intermediate range unmanned aerial vehicle ejecting frame described in the utility model; equipped with absorption type supporting leg, damping spring and angle demodulator; the placement for enabling to launcher is more firm; and it can effectively reduce the impact force generated when unmanned plane takes off; play certain protective effect in itself to equipment; the take-off angle of unmanned plane can be adjusted, different operating situation is applicable in, brings better prospect of the application.
Description
Technical field
The utility model is related to launching cradle apparatus field, more particularly to a kind of intermediate range unmanned aerial vehicle ejecting frame.
Background technology
The unmanned aerial vehicle ejecting mode of taking off is a kind of advanced unmanned plane radiation pattern occurred in the world in recent years, with commonly using
Rato mode compare, have many advantages, such as that good property safe and out of sight, good economy performance and adaptability are good, will not generate light,
The signals such as sound, heat and smog, convenient for the hidden of take-off venue, there is no the storage, transport and problem of management of fire control equipment, and often
The expense that consumable supplies and support ensure during secondary progress unmanned plane transmitting is relatively low, in addition in a certain range by adjusting accumulation of energy
Device the blowing pressure and precharge pressure can be adapted to the requirement of different unmanned plane take-off weights and takeoff speed, Gas fluid pressure bullet
It penetrates launching apparatus to be mountable in carrier vehicle, be shifted convenient for maneuver warfare and transport, therefore device has good maneuverability again
Property.
Existing unmanned aerial vehicle ejecting frame when in use there are certain drawbacks, when placing not enough put down by traditional launching cradle
Surely so that after take off, launching cradle can generate inclination to unmanned plane, and the damping effect of traditional launching cradle is poor, and unmanned plane is taking off
When can generate huge impact force, impact force can cause equipment in itself certain damage, can not adjust the angle that unmanned plane takes off
Degree brings certain adverse effect, for this purpose, it is proposed that a kind of intermediate range unmanned aerial vehicle ejecting frame to the ejection of taking off of unmanned plane.
Utility model content
The main purpose of the utility model is that providing a kind of intermediate range unmanned aerial vehicle ejecting frame, background technology can be effectively solved
The problems in.
To achieve the above object, the technical solution that the utility model is taken is：
A kind of intermediate range unmanned aerial vehicle ejecting frame, including ejection frame body and controller, the ejection frame body is internally provided with
Plate is filled in damping, and the lower end of the ejection frame body is equipped with absorption type supporting leg, and the both sides of the absorption type supporting leg are equipped with
Damping spring, the upper end of the ejection frame body are equipped with hydraulic pressure lifting device, and the upper end of the hydraulic pressure lifting device is equipped with emitter,
The upper end of the emitter is equipped with brute spring, and the outer surface of the emitter is equipped with handle slideway, the brute spring
One end be equipped with ejection fixator, one end of the handle slideway is equipped with handle, and one end of the emitter is equipped with angle tune
Save device, the side of the angle demodulator is equipped with supporting rack, and support frame as described above is fixedly connected with controller, the controller it is interior
Surface is equipped with liquid crystal display, and the lower section of the liquid crystal display is equipped with button, and the side of the damping spring is equipped with electricity
Pond module, the outer surface of the battery module are equipped with charge port.
Preferably, the absorption type supporting leg is fixedly connected with damping spring with ejection frame body, the absorption type branch
The quantity of support leg is two groups, and the quantity of the damping spring is four groups.
Preferably, the emitter is connected by angle demodulator with launching cradle subject activity.
Preferably, the brute spring is fixedly connected with ejection fixator.
Preferably, the liquid crystal display is fixedly connected with button with controller.
Compared with prior art, the utility model has the advantages that：The unmanned aerial vehicle ejecting frame, in the bottom of device
Be provided with absorption type supporting leg, absorption type supporting leg can ground and device in itself between generate adsorption capacity so that device
The phenomenon that placing and more consolidate, will not generating inclination, damping spring, traditional launching cradle are equipped in the both sides of absorption type supporting leg
Damping effect it is poor, unmanned plane can generate huge impact force when taking off, and impact force can cause equipment in itself certain
Damage, damping spring can be very good to offset the impact force that unmanned plane is generated when taking off, and play the role of protection to equipment,
Angle demodulator is equipped in the side of launching cradle, traditional launching cradle can not adjust the angle that unmanned plane takes off so that unmanned plane rises
Winged mode is more single, and angle demodulator can change the take-off angle of unmanned plane, adapts to the various environment that take off, passes through controller
The departure time and the take-off angle of unmanned plane can be controlled, whole device is simple, easy to operate, the effect of angle adjustment and damping
It is more preferable relative to traditional approach.
Description of the drawings
Fig. 1 is a kind of overall structure diagram of intermediate range unmanned aerial vehicle ejecting frame of the utility model.
Fig. 2 is a kind of partial view of intermediate range unmanned aerial vehicle ejecting frame of the utility model.
In figure：1st, battery module；2nd, charge port；3rd, absorption type supporting leg；4th, damping spring；5th, frame body is launched；6th, subtract
Shake filling plate；7th, supporting rack；8th, controller；9th, angle demodulator；10th, fixator is launched；11st, handle；12nd, brute spring；13、
Handle slideway；14th, emitter；15th, hydraulic pressure lifting device；16th, liquid crystal display；17th, button.
Specific embodiment
To be easy to understand technical means, creative features, achievable purpose and effectiveness of the utility model, below
With reference to specific embodiment, the utility model is expanded on further.
As shown in Figs. 1-2, a kind of intermediate range unmanned aerial vehicle ejecting frame, including ejection frame body 5 and controller 8, the launching cradle
Main body 5 is internally provided with damping filling plate 6, and the lower end of the ejection frame body 5 is equipped with absorption type supporting leg 3, the absorption type
The both sides of supporting leg 3 are equipped with damping spring 4, and the upper end of the ejection frame body 5 is equipped with hydraulic pressure lifting device 15, the hydraulic pressure liter
The upper end for dropping device 15 is equipped with emitter 14, and the upper end of the emitter 14 is equipped with brute spring 12, the emitter 14
Outer surface be equipped with handle slideway 13, one end of the brute spring 12 is equipped with ejection fixator 10, the handle slideway 13
One end is equipped with handle 11, and one end of the emitter 14 is equipped with angle demodulator 9, and the side of the angle demodulator 9 is equipped with
Supporting rack 7, support frame as described above 7 are fixedly connected with controller 8, and the inner surface of the controller 8 is equipped with liquid crystal display 16, described
The lower section of liquid crystal display 16 is equipped with button 17, and the side of the damping spring 4 is equipped with battery module 1, the battery mould
The outer surface of block 1 is equipped with charge port 2.
Wherein, the absorption type supporting leg 3 is fixedly connected with damping spring 4 with ejection frame body 5, the absorption type branch
The quantity of support leg 3 is two groups, and the quantity of the damping spring 4 is four groups.
Wherein, the emitter 14 is flexibly connected by angle demodulator 9 and ejection frame body 5.
Wherein, the brute spring 12 is fixedly connected with ejection fixator 10.
Wherein, the liquid crystal display 16 is fixedly connected with button 17 with controller 8.It should be noted that this practicality
Novel is a kind of intermediate range unmanned aerial vehicle ejecting frame, when in use, by battery module 1, has the function of to store electricity, can cause
Equipment has the function of outdoor study, and power supply is accessed by charge port 2, can be equipment charge, by absorption type supporting leg 3,
Can ground and device in itself between generate adsorption capacity so that the placement of device is more firm, can be with by damping spring 4
The impact force that unmanned plane is generated when taking off is offset well, plays the role of protection to equipment, and plate 6 is filled by damping,
The weight of ejection frame body 5 can be reduced, there is good resiliency so that equipment is easy to carry, by supporting rack 7, to control
Device 8 processed plays the role of support, by controller 8, can control the angle of launching cradle and the departure time of unmanned plane, pass through
Angle demodulator 9, the adjustable angle taken off by launching fixator 10, can play the role of unmanned plane fixed, pass through
Pull handle 11 can generate thrust required when unmanned plane takes off, and by brute spring 12, can go out unmanned aerial vehicle ejecting
It goes, by emitter 14, placement can be played the role of before take off to unmanned plane, it, can be with by hydraulic pressure lifting device 15
The height of emitter 14 is adjusted, the height where unmanned plane and the angle taken off can be shown by liquid crystal display 16, is led to
Pressing keys 17 are crossed, controller 8 can be manipulated, it is more practical.A kind of intermediate range unmanned aerial vehicle ejecting frame described in the utility model, if
There are absorption type supporting leg 3, damping spring 4 and angle demodulator 9, the placement for enabling to launcher is more firm, and can be effective
The impact force generated when unmanned plane takes off is reduced, certain protective effect is played in itself to equipment, unmanned plane can be adjusted
Take-off angle is applicable in different operating situation, brings better prospect of the application.
The basic principle of the utility model and main feature and the advantages of the utility model has been shown and described above.One's own profession
The technical staff of industry is it should be appreciated that the present utility model is not limited to the above embodiments, described in above embodiments and description
Only illustrate the principle of the utility model, on the premise of not departing from the spirit and scope of the utility model, the utility model is also
Various changes and modifications are had, these various changes and improvements fall within the scope of the claimed invention.The utility model
Claimed range is defined by the appending claims and its equivalent thereof.
Claims (5)
1. a kind of intermediate range unmanned aerial vehicle ejecting frame, including ejection frame body (5) and controller (8), it is characterised in that：The launching cradle
Main body (5) is internally provided with damping filling plate (6), and the lower end of the ejection frame body (5) is equipped with absorption type supporting leg (3), institute
The both sides for stating absorption type supporting leg (3) are equipped with damping spring (4), and the upper end of the ejection frame body (5) is equipped with hydraulic lifting
Device (15), the upper end of the hydraulic pressure lifting device (15) are equipped with emitter (14), and the upper end of the emitter (14) is equipped with by force
Power spring (12), the outer surface of the emitter (14) are equipped with handle slideway (13), and one end of the brute spring (12) is set
There is ejection fixator (10), one end of the handle slideway (13) is equipped with handle (11), and one end of the emitter (14) is set
Angled adjuster (9), the side of the angle demodulator (9) are equipped with supporting rack (7), support frame as described above (7) and controller (8)
It is fixedly connected, the inner surface of the controller (8) is equipped with liquid crystal display (16), and the lower section of the liquid crystal display (16) is equipped with
Button (17), the side of the damping spring (4) are equipped with battery module (1), and the outer surface of the battery module (1) is equipped with
Charge port (2).
2. a kind of intermediate range unmanned aerial vehicle ejecting frame according to claim 1, it is characterised in that：The absorption type supporting leg (3)
It is fixedly connected with damping spring (4) with ejection frame body (5), the quantity of the absorption type supporting leg (3) is two groups, described to subtract
The quantity for shaking spring (4) is four groups.
3. a kind of intermediate range unmanned aerial vehicle ejecting frame according to claim 1, it is characterised in that：The emitter (14) passes through
Angle demodulator (9) and ejection frame body (5) are flexibly connected.
4. a kind of intermediate range unmanned aerial vehicle ejecting frame according to claim 1, it is characterised in that：The brute spring (12) and bullet
Fixator (10) is penetrated to be fixedly connected.
5. a kind of intermediate range unmanned aerial vehicle ejecting frame according to claim 1, it is characterised in that：The liquid crystal display (16) and
Button (17) is fixedly connected with controller (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721267552.4U CN207523957U (en) | 2017-09-28 | 2017-09-28 | A kind of intermediate range unmanned aerial vehicle ejecting frame |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721267552.4U CN207523957U (en) | 2017-09-28 | 2017-09-28 | A kind of intermediate range unmanned aerial vehicle ejecting frame |
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| Publication Number | Publication Date |
|---|---|
| CN207523957U true CN207523957U (en) | 2018-06-22 |
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ID=62569800
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721267552.4U Active CN207523957U (en) | 2017-09-28 | 2017-09-28 | A kind of intermediate range unmanned aerial vehicle ejecting frame |
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| CN (1) | CN207523957U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109094809A (en) * | 2018-09-07 | 2018-12-28 | 佛山皖和新能源科技有限公司 | A kind of transmitting of fixed-wing unmanned plane Electromagnetic Launching sliding rail and its launching technique |
| CN114800417A (en) * | 2022-06-08 | 2022-07-29 | 国网河北省电力有限公司元氏县供电分公司 | Intelligent maintenance tool case is used in power supply |
-
2017
- 2017-09-28 CN CN201721267552.4U patent/CN207523957U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109094809A (en) * | 2018-09-07 | 2018-12-28 | 佛山皖和新能源科技有限公司 | A kind of transmitting of fixed-wing unmanned plane Electromagnetic Launching sliding rail and its launching technique |
| CN114800417A (en) * | 2022-06-08 | 2022-07-29 | 国网河北省电力有限公司元氏县供电分公司 | Intelligent maintenance tool case is used in power supply |
| CN114800417B (en) * | 2022-06-08 | 2023-09-26 | 国网河北省电力有限公司元氏县供电分公司 | Intelligent maintenance tool case for power supply |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20190507 Address after: 710000 Xi'an International Port Area, Shaanxi Province Patentee after: Xi'an Jizhi Aviation Technology Co., Ltd. Address before: No. 19, Zone C, 1st Floor, No. 31 Taiwanese Pioneering Garden, No. 2 Jinjing Road, Beigao Town, Pingtan Comprehensive Experimental Zone, Fuzhou City, Fujian Province Patentee before: Pingtan Haichuang Newell Technology Co. Ltd. |