CN203763852U - Model aircraft safety paraglider - Google Patents
Model aircraft safety paraglider Download PDFInfo
- Publication number
- CN203763852U CN203763852U CN201420166147.3U CN201420166147U CN203763852U CN 203763852 U CN203763852 U CN 203763852U CN 201420166147 U CN201420166147 U CN 201420166147U CN 203763852 U CN203763852 U CN 203763852U
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- CN
- China
- Prior art keywords
- umbrella
- paraglider
- aeromodelling aerocraft
- safe
- safe umbrella
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
The utility model provides a model aircraft safety paraglider, and relates to an aircraft protecting device, in particular to a remote control model aircraft with the safety paraglider. The model aircraft safety paraglider comprises a model aircraft and the safety paraglider. The safety paraglider is fixedly connected to the model aircraft through a wire. An paraglider releasing device is further included, one end of the paraglider releasing device is fixedly connected with the model aircraft, the other end of the paraglider releasing device is in detachable connection with the model aircraft, and the safety paraglider can be overlaid on the lower portion of the paraglider releasing device in a detachable mode. According to the model aircraft safety paraglider, a paraglider is detachably arranged on the lower portion of the paraglider releasing body, once mechanical breakdown happens, the paraglider releasing device enables the paraglider to be quickly released, under the mutual action of the paraglider and air, the model aircraft can be protected, and equipment damaged caused by hard landing of the model aircraft and the ground is avoided. The model aircraft safety paraglider is simple in connecting mechanism, and high in practicability.
Description
Technical field
The utility model relates to a kind of aircraft protective device, particularly a kind of telecontrolled model aircraft that is loaded with safe umbrella.
Background technology
In daily life, common remote-controlled model aircraft and other similar aircraft are generally all very worthy, when aircraft on high in when flight, different from the automobile of ground run, once generation mechanical breakdown, aeromodelling aerocraft and ground form hard landing, centesimal fault, often caused remote-controlled model aircraft and aircraft absolutely to damage, if carried the aircraft of research equipment, once the not only aircraft that breaks down can crash, also can cause the damage of research equipment, will bring larger economic loss, make us very much unfortunate.
Summary of the invention
The utility model is intended to propose a kind of in telecontrolled aircraft when there was a mechanical failure, the aeromodelling aerocraft safe umbrella that can avoid telecontrolled aircraft to crash and damage.
Aeromodelling aerocraft safe umbrella described in the utility model, comprise aeromodelling aerocraft and safe umbrella, described safe umbrella is connected on aeromodelling aerocraft by line, also include a umbrella body releasing device, this umbrella body releasing device one end and aeromodelling aerocraft are connected, the other end is connected with aeromodelling aerocraft releasable, safe umbrella removable be laminated on umbrella body releasing device bottom.
Preferably, described umbrella body releasing device comprises steering wheel, rocking arm and fixed band, steering wheel is fixedly installed on aeromodelling aerocraft; rocking arm is arranged on steering wheel; and be movably connected with steering wheel; one end of fixed band is fixedly installed on aeromodelling aerocraft, and the other end is articulated on rocking arm, safe umbrella removable be laminated on fixed band bottom.
Preferably, the bottom of described umbrella body releasing device is also provided with one for placing the cabin body of safe umbrella, and it is inner that safe umbrella is stacked in cabin body, and fixed band, through the upper surface of cabin body, is enclosed in cabin body by safe umbrella inner.
Or preferably, described fixed band is spacing elastic cord.
Or further preferably, on described steering wheel, also induction connects a remote controller.
Or still more preferably, described remote controller is connected by electromagnetic wave or microwave with steering wheel.
Preferably, described aeromodelling aerocraft is the oil machine engine power model of an airplane or the methanol engine model of an airplane or the battery power model of an airplane.
Preferably, the described oil machine engine power model of an airplane is the petrol engine model of an airplane.
Preferably, described safe umbrella is paraglider or airborne safe balloon.
Aeromodelling aerocraft safe umbrella described in the utility model; safe umbrella removable is arranged on to umbrella body releasing device bottom; once generation mechanical breakdown, umbrella body releasing device can discharge safe umbrella rapidly, under the interaction of safe umbrella and air; can play a protective role to aeromodelling aerocraft; the device damage of avoiding the hard landing between itself and ground to cause, the utility model bindiny mechanism is simple, can suitability for industrialized production; and can bring huge economic benefit, practical.
Accompanying drawing explanation
Fig. 1 is syndeton schematic diagram of the present utility model.
Fig. 2 is the use state reference map of embodiment 1.
Fig. 3 is the use state reference map of embodiment 3.
1-aeromodelling aerocraft in figure; 2-safe umbrella; 3-steering wheel; 4-rocking arm; 5-fixed band.
The specific embodiment
Embodiment 1.
Aeromodelling aerocraft safe umbrella described in the utility model, comprise aeromodelling aerocraft 1 and safe umbrella 2, described safe umbrella 2 is connected on aeromodelling aerocraft 1 by line, steering wheel 3 is fixedly installed on aeromodelling aerocraft 1, and Rocker arm 4 is arranged on steering wheel 3, and is movably connected with steering wheel 3, one end of fixed band 5 is fixedly installed on aeromodelling aerocraft, the other end is articulated on Rocker arm 4, and safe umbrella 2 can be folded neat rear concora crush in fixed band 5 bottoms, and remote controller is connected with steering wheel 3 inductions by electromagnetic wave.Fixed band 5 described in the utility model is spacing elastic cord; Described aeromodelling aerocraft 1 is the oil machine engine power model of an airplane or the methanol engine model of an airplane or the battery power model of an airplane; The described oil machine engine power model of an airplane is the petrol engine model of an airplane.
During use, safe umbrella 2 is folded to neat rear concora crush in fixed band 5 bottoms, one end of fixed band 5 is fixing aboard, the other end is articulated on Rocker arm 4, when aircraft is when there was a mechanical failure, user promptly controls steering wheel 3, make it drive Rocker arm 4 to rotate, when Rocker arm 4 rotates, fixed band 5 can skid off Rocker arm 4 gradually along with the swing of Rocker arm 4, and finally depart from Rocker arm 4, now safe umbrella 2 opens under the effect of air, and with air generation relative motion, slow down the decrease speed of aeromodelling aerocraft 1, avoided the hard landing between aeromodelling aerocraft 1 and ground, prevented the badly damaged of aeromodelling aerocraft 1.
Embodiment 2.
The present embodiment is substantially the same manner as Example 1, difference is that the present embodiment is also provided with one for placing the cabin body of safe umbrella 2 on described aeromodelling aerocraft 1, safe umbrella 2 is folded and is placed on body inside, cabin, fixed band 5 is through the upper surface of cabin body, and it is inner that safe umbrella 2 is enclosed in to cabin body, effectively avoided aeromodelling aerocraft 1 in flight course, the destruction that air produces safe umbrella 2, safeguard the integrality of safe umbrella 2, further promoted the security performance of aeromodelling aerocraft 1.
Embodiment 3.
The present embodiment and embodiment 1 or 2 are basic identical, difference is that safe umbrella 2 is special safety umbrella described in the present embodiment, described special safety umbrella, and its bottom is a large main chute, main chute top is provided with an extraction parachute, 1/10th sizes that the size of this extraction parachute is main chute.When there is machinery in aeromodelling aerocraft 1, user promptly controls steering wheel 3, make it drive Rocker arm 4 to rotate, when Rocker arm 4 rotates, fixed band 5 can skid off Rocker arm 4 gradually along with the swing of Rocker arm 4, and finally depart from Rocker arm 4, now extraction parachute flies up after inflating under the effect of air, pulls out main chute, and main chute is opened after naturally inflating, now safe umbrella is fully opened, for aeromodelling aerocraft 1 provides safety guarantee.
Claims (9)
1. aeromodelling aerocraft safe umbrella, comprise aeromodelling aerocraft (1) and safe umbrella (2), described safe umbrella (2) is connected on aeromodelling aerocraft (1) by line, it is characterized in that: also include a umbrella body releasing device, this umbrella body releasing device one end and aeromodelling aerocraft (1) are connected, the other end is connected with aeromodelling aerocraft (1) releasable, safe umbrella (2) removable be laminated on umbrella body releasing device bottom.
2. aeromodelling aerocraft safe umbrella as claimed in claim 1; it is characterized in that: described umbrella body releasing device comprises steering wheel (3), rocking arm (4) and fixed band (5); steering wheel (3) is fixedly installed on aeromodelling aerocraft (1); rocking arm (4) is arranged on steering wheel (3); and be movably connected with steering wheel (3); one end of fixed band (5) is fixedly installed on aeromodelling aerocraft (1); it is upper that the other end is articulated in rocking arm (4), umbrella (2) removable be laminated on fixed band (5) bottom.
3. aeromodelling aerocraft safe umbrella as claimed in claim 2, it is characterized in that: the bottom of described umbrella body releasing device is also provided with one for placing the cabin body of safe umbrella (2), safe umbrella (2) can laminate in cabin body inner, fixed band (5), through the upper surface of cabin body, is enclosed in cabin body by safe umbrella (2) inner.
4. aeromodelling aerocraft safe umbrella as claimed in claim 2 or claim 3, is characterized in that: described fixed band (5) is spacing elastic cord.
5. aeromodelling aerocraft safe umbrella as claimed in claim 5, is characterized in that: on described steering wheel (3), also induction connects a remote controller.
6. aeromodelling aerocraft safe umbrella as claimed in claim 6, is characterized in that: described remote controller is connected by electromagnetic wave or microwave with steering wheel (3).
7. aeromodelling aerocraft safe umbrella as claimed in claim 1, is characterized in that: described aeromodelling aerocraft (1) is the oil machine engine power model of an airplane or the methanol engine model of an airplane or the battery power model of an airplane.
8. aeromodelling aerocraft safe umbrella as claimed in claim 7, is characterized in that: the described oil machine engine power model of an airplane is the petrol engine model of an airplane.
9. aeromodelling aerocraft safe umbrella as claimed in claim 1, is characterized in that: described safe umbrella is paraglider or special safety umbrella or airborne safe balloon.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420166147.3U CN203763852U (en) | 2014-04-08 | 2014-04-08 | Model aircraft safety paraglider |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420166147.3U CN203763852U (en) | 2014-04-08 | 2014-04-08 | Model aircraft safety paraglider |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203763852U true CN203763852U (en) | 2014-08-13 |
Family
ID=51281102
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420166147.3U Expired - Fee Related CN203763852U (en) | 2014-04-08 | 2014-04-08 | Model aircraft safety paraglider |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203763852U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106251736A (en) * | 2016-09-30 | 2016-12-21 | 襄阳宏伟航空器有限责任公司 | A kind of paragliding VR simulator |
| CN108313313A (en) * | 2018-01-26 | 2018-07-24 | 重庆邮电大学 | Unmanned plane failure response system |
| CN110312657A (en) * | 2017-03-01 | 2019-10-08 | Rps航空航天技术股份有限公司 | A kind of aircraft equipped with assisting in flying component |
-
2014
- 2014-04-08 CN CN201420166147.3U patent/CN203763852U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106251736A (en) * | 2016-09-30 | 2016-12-21 | 襄阳宏伟航空器有限责任公司 | A kind of paragliding VR simulator |
| CN110312657A (en) * | 2017-03-01 | 2019-10-08 | Rps航空航天技术股份有限公司 | A kind of aircraft equipped with assisting in flying component |
| CN108313313A (en) * | 2018-01-26 | 2018-07-24 | 重庆邮电大学 | Unmanned plane failure response system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20140813 Termination date: 20160408 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |