CN202642096U - Small-scale unmanned aerial vehicle, as well as onboard arresting gear, ground arresting gear and arresting system thereof - Google Patents
Small-scale unmanned aerial vehicle, as well as onboard arresting gear, ground arresting gear and arresting system thereof Download PDFInfo
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- CN202642096U CN202642096U CN 201220138320 CN201220138320U CN202642096U CN 202642096 U CN202642096 U CN 202642096U CN 201220138320 CN201220138320 CN 201220138320 CN 201220138320 U CN201220138320 U CN 201220138320U CN 202642096 U CN202642096 U CN 202642096U
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Abstract
The utility model relates to a small-scale unmanned aerial vehicle, as well as an onboard arresting gear, a ground arresting gear and an arresting system thereof. The onboard arresting gear comprises an arresting hook and a release unit; one end of the arresting hook is used for being rotatablely connected to a fuselage main body of the small-scale unmanned aerial vehicle; the other end of the arresting hook is used for being connected with the release unit; and the release unit is fixed on a fuselage of the small-scale unmanned aerial vehicle and is used for fixing or releasing the arresting hook according to a received external control signal. According to the utility model, the landing recovery can be implemented during landing without a taxiway; and the small-scale unmanned aerial vehicle, as well as the onboard arresting gear, the ground arresting gear and the arresting system thereof has simple structure and is convenient to operate.
Description
Technical field
The application relates to arresting gear on SUAV (small unmanned aerial vehicle) and the machine thereof, ground arresting gear and arresting system.
Background technology
The miniature self-service abbreviation " SUAV (small unmanned aerial vehicle) " that drives an airplane is to utilize radio robot and not manned aircraft that the process controller provided for oneself is handled.Without driving compartment, but the equipment such as autopilot, process controller are installed on the machine.On ground, the naval vessels or machine tool command and control station personnel by equipment such as radars, to its follow the tracks of, location, remote control, remote measurement and digital communication.Can under radio telecommand, as conventional airplane, take off or launch with booster rocket, also can take aerial input flight to by machine tool.During recovery, the available mode automatic Landing the same with the conventional airplane landing mission also can be by remote control with parachute or block recovery.But repetitiousness uses repeatedly.Be widely used in aerial reconnaissance, supervision, communication, antisubmarine, electro countermeasure etc.
Existing SUAV (small unmanned aerial vehicle) is blocked recovery system and has been made a lot of effort and trial for solving SUAV (small unmanned aerial vehicle) safe landing problem.US Patent the 7th, 143, No. 976 (US7143976B2) stated a kind of SUAV (small unmanned aerial vehicle) ventral that is connected to, and blocks bar landing recovery system by what multiple fastener formed, is fit to SUAV (small unmanned aerial vehicle) and blocks recovery in the regional safety of limited space.US Patent the 7th, 219, No. 856 (US7219856B2) stated that then a kind of automatic release blocks the ground recovery apparatus of rope, can be used for reclaiming the SUAV (small unmanned aerial vehicle) that arrester hook places ventral.
But these systems and device for the SUAV (small unmanned aerial vehicle) of blocking low speed, on the machine or ground installation seem too complicated.And the airborne device complexity can cause SUAV (small unmanned aerial vehicle) weight to increase, and airworthiness descends; The surface facility complexity has then increased equipment cost and has reduced the portability of equipment.
The utility model content
Provide hereinafter about brief overview of the present utility model, in order to basic comprehension about some aspect of the present utility model is provided.Should be appreciated that this general introduction is not about exhaustive general introduction of the present utility model.It is not that intention is determined key of the present utility model or pith, neither be intended to limit scope of the present utility model.Its purpose only is that the form of simplifying provides some concept, with this as the in greater detail preorder of discussing after a while.
A main purpose of the present utility model is to provide arresting gear on a kind of SUAV (small unmanned aerial vehicle) and the machine thereof, ground arresting gear and arresting system.
According to an aspect of the present utility model, arresting gear on a kind of SUAV (small unmanned aerial vehicle) machine comprises: arrester hook and release gear; One end of described arrester hook is used for being rotationally attached to SUAV (small unmanned aerial vehicle) fuselage main body, and the other end is used for being connected with described release gear; Described release gear is fixed on the described SUAV (small unmanned aerial vehicle) fuselage, is used for fixing or discharging described arrester hook according to the external control signal that receives.
Further, the described arrester hook in the arresting gear comprises the neck of hook and hook body on the SUAV (small unmanned aerial vehicle) machine;
The described neck of hook is elongated rod-shaped, and described hook is as circular-arc greater than 180 ° of central angle;
Described arrester hook rotatably be connected to the ventral of described SUAV (small unmanned aerial vehicle) away from an end of hook body.
Further, the length of the described arrester hook in the arresting gear is no more than the length of described SUAV (small unmanned aerial vehicle) on the SUAV (small unmanned aerial vehicle) machine.
Further, the described arrester hook in the arresting gear is positioned at the symmetrical plane of described SUAV (small unmanned aerial vehicle) on the SUAV (small unmanned aerial vehicle) machine;
Described arrester hook is movably connected at the center of gravity place of described SUAV (small unmanned aerial vehicle).
Further, the end away from the hook body of the described arrester hook in the arresting gear passes through the single degree of freedom chain connection at the ventral of described SUAV (small unmanned aerial vehicle) on the SUAV (small unmanned aerial vehicle) machine.
According on the other hand of the present utility model, a kind of SUAV (small unmanned aerial vehicle) ground arresting gear comprises: two supports placing perpendicular to ground, and be connected to elastic threads between described two supports; Described elastic threads is used for providing the power of blocking of SUAV (small unmanned aerial vehicle) flight.
Further, the described elastic threads in the arresting gear of SUAV (small unmanned aerial vehicle) ground is parallel to ground, and described elastic threads is not less than the length of described SUAV (small unmanned aerial vehicle) apart from the height on ground.
According on the other hand of the present utility model, a kind of SUAV (small unmanned aerial vehicle) arresting system comprises:
Arresting gear and SUAV (small unmanned aerial vehicle) ground arresting gear on the SUAV (small unmanned aerial vehicle) machine.
According on the other hand of the present utility model, a kind of SUAV (small unmanned aerial vehicle) comprises the SUAV (small unmanned aerial vehicle) fuselage, also comprises arresting gear on the SUAV (small unmanned aerial vehicle) machine.
According on the other hand of the present utility model, a kind of SUAV (small unmanned aerial vehicle) is blocked recovery system and is comprised SUAV (small unmanned aerial vehicle) ground arresting gear and SUAV (small unmanned aerial vehicle).
Adopt arresting gear on SUAV (small unmanned aerial vehicle) of the present utility model and the machine thereof, ground arresting gear and arresting system, can under the condition of the landing that does not possess plane track, realize landing and reclaim, and simple in structure, easy to operate.
Description of drawings
With reference to below in conjunction with the explanation of accompanying drawing to the utility model embodiment, can understand more easily above and other purpose of the present utility model, characteristics and advantage.Parts in the accompanying drawing are just in order to illustrate principle of the present utility model.In the accompanying drawings, same or similar technical characterictic or parts will adopt identical or similar Reference numeral to represent.
Fig. 1 is the constructional drawing that SUAV (small unmanned aerial vehicle) of the present utility model is blocked a kind of embodiment of arresting gear on the machine in the regenerative apparatus;
Fig. 2 is the constructional drawing that SUAV (small unmanned aerial vehicle) of the present utility model is blocked a kind of embodiment of the ground arresting gear in the regenerative apparatus;
Fig. 3-Fig. 6 is the scheme drawing that SUAV (small unmanned aerial vehicle) of the present utility model is blocked the regenerative apparatus working process;
Wherein:
1---arrester hook;
2---the single degree of freedom hinge;
3---release gear;
4---elastic threads;
5---support.
The specific embodiment
Embodiment of the present utility model is described with reference to the accompanying drawings.The element of describing in an accompanying drawing of the present utility model or a kind of embodiment and feature can combine with element and the feature shown in one or more other accompanying drawing or the embodiment.Should be noted that for purpose clearly, omitted in accompanying drawing and the explanation and the utility model expression and description irrelevant, parts known to persons of ordinary skill in the art and processing.SUAV (small unmanned aerial vehicle) of the present utility model is blocked regenerative apparatus and is comprised arresting gear and ground arresting gear on the machine.
Referring to shown in Figure 1, block the constructional drawing of a kind of embodiment of arresting gear on the machine in the regenerative apparatus for SUAV (small unmanned aerial vehicle).Arresting gear comprises arrester hook 1 and release gear 3 on the machine.One end of arrester hook is rotationally attached to the fuselage of SUAV (small unmanned aerial vehicle).Release gear 3 is fixed on the SUAV (small unmanned aerial vehicle), by control setup, for example, remote controller control release gear 3 fixing or release arrester hooks 1.
As a kind of embodiment, the described arrester hook 1 that SUAV (small unmanned aerial vehicle) is blocked in the regenerative apparatus comprises the neck of hook and hook body.The neck of hook is elongated rod-shaped, and hook is as circular-arc greater than 180 ° of central angle, and for example the hook body can be the circular arc of 5/8 part of a circle.
As a kind of preferred version, SUAV (small unmanned aerial vehicle) is blocked in the regenerative apparatus, arrester hook 1 rotatably be connected to the ventral of SUAV (small unmanned aerial vehicle) away from an end of hook body, for example the end away from the hook body of arrester hook 1 rotatably is connected to the center of gravity place of SUAV (small unmanned aerial vehicle).Rotatably connection herein can be the connection of arbitrarily rotatable mode well-known to those skilled in the art, for example adopts single degree of freedom hinge 2 to connect.
As a kind of preferred version, the length that SUAV (small unmanned aerial vehicle) is blocked the arrester hook 1 of regenerative apparatus is no more than the length of SUAV (small unmanned aerial vehicle), and arrester hook 1 is positioned at the symmetrical plane of SUAV (small unmanned aerial vehicle).
Referring to shown in Figure 2, block the constructional drawing of a kind of embodiment of the ground arresting gear in the regenerative apparatus for SUAV (small unmanned aerial vehicle).This ground arresting gear comprises two supports 5 placing perpendicular to ground and is connected to two elastic threads 4 between the support.
As a kind of preferred version, the elastic threads 4 that SUAV (small unmanned aerial vehicle) is blocked in the regenerative apparatus is parallel to ground, and elastic threads 4 is not less than the length of SUAV (small unmanned aerial vehicle) apart from the height on ground.
3-is shown in Figure 6 referring to accompanying drawing, blocks the scheme drawing of regenerative apparatus working process for SUAV (small unmanned aerial vehicle) of the present utility model.
Referring to shown in Figure 3, SUAV (small unmanned aerial vehicle) enters decline passway, flies to towards the direction of ground arresting gear.In this process, can control release gear 3 by control setup and discharge arrester hook 1, so that an end of arrester hook 1 is because action of gravitation decline.
Referring to shown in Figure 4, SUAV (small unmanned aerial vehicle) continues to descend, until the hook body of arrester hook 1 hooks the elastic threads 4 in the arresting gear of ground.Referring to shown in Figure 5, because of effect of inertia, SUAV (small unmanned aerial vehicle) will continue forward flight, yet because the hook body of arrester hook 1 has hooked the elastic threads 4 in the arresting gear of ground, this SUAV (small unmanned aerial vehicle) will be slowed down gradually, until stop at last (referring to shown in Figure 6).So far, SUAV (small unmanned aerial vehicle) has been finished the overall process of its landing by blocking regenerative apparatus.
In a kind of concrete embodiment, adopting quality is 0.55 kilogram unmanned plane, long 0.8 meter of this unmanned aerial vehicle body, 1 meter of the span, flying speed be about 20 kms/hour.Arrester hook on the machine is made by steel wire, is about 0.7 meter, and releasing mechanism is formed by the transformation of the way of electronic telecontrol steering wheel.The rope that blocks in the ground installation has adopted the elasticity luggage rope, blocks rope support and is made by steel pipe, and 2.5 meters of height block the top that rope ties up to support.In the reality test, block regenerative apparatus the experiment unmanned plane has been obtained the extraordinary effect of blocking.In many experiments, as long as any part of arrester hook touches and blocks rope, unmanned plane just can be by safety, nondestructively block, successful implementation recovery.
Adopt arresting gear on SUAV (small unmanned aerial vehicle) of the present utility model and the machine thereof, ground arresting gear and arresting system, do not need a plurality of snap closes during recovery, single arrester hook can be finished the work smoothly.In addition, owing to block rope good elasticity is arranged, when SUAV (small unmanned aerial vehicle) reclaims, need not after rope is blocked in the SUAV (small unmanned aerial vehicle) contact, to discharge the ropes that block more and slow down for SUAV (small unmanned aerial vehicle).Can under the condition of the landing that does not possess plane track, realize the ground recovery of SUAV (small unmanned aerial vehicle), and simple in structure, easy to operate.
The above is described in detail embodiments more of the present utility model.To understand such as those of ordinary skill in the art, whole or any steps or the parts of method and apparatus of the present utility model, can be in the network of any computing equipment (comprising treater, storage medium etc.) or computing equipment, realized with hardware, firmware, software or their combination, this is that those of ordinary skills use their basic programming skill just can realize in the situation of understanding content of the present utility model, does not therefore need to specify at this.
In addition, it is evident that, when relating to possible peripheral operation in the superincumbent explanation, will use undoubtedly any display equipment and any input equipment, corresponding interface and the control program that link to each other with any computing equipment.Generally speaking, the hardware of the various operations in the related hardware in computing machine, computer system or the computer network, software and the realization preceding method of the present utility model, firmware, software or their combination namely consist of equipment of the present utility model and each constituent elements thereof.
Therefore, based on above-mentioned understanding, the purpose of this utility model can also be by realizing in any program of messaging device operation or batch processing.Described messaging device can be known common apparatus.Therefore, the purpose of this utility model also can be only by providing the program product that comprises the program code of realizing described method or equipment to realize.That is to say that such program product also consists of the utility model, and storage or the medium that transmits such program product also consist of the utility model.Obviously, described storage or transmission medium can be well known by persons skilled in the art, and therefore storage or the transmission medium of any type that perhaps develops in the future also there is no need at this various storages or transmission medium to be enumerated one by one.
In equipment of the present utility model and method, obviously, after can decomposing, make up and/or decompose, each parts or each step reconfigure.These decomposition and/or reconfigure and to be considered as equivalents of the present utility model.The step that also it is pointed out that the above-mentioned series of processes of execution can naturally a/s order be carried out in chronological order, but does not need necessarily to carry out according to time sequence.Some step can walk abreast or carry out independently of one another.Simultaneously, in the above in the description to the utility model specific embodiment, can in one or more other embodiment, use in identical or similar mode for the feature that a kind of embodiment is described and/or illustrated, combined with the feature in other embodiment, or the feature in alternative other embodiment.
Should emphasize that term " comprises/comprise " existence that refers to feature, key element, step or assembly when this paper uses, but not get rid of the existence of one or more further feature, key element, step or assembly or additional.
Although described the utility model and advantage thereof in detail, be to be understood that and in the situation that does not exceed the spirit and scope of the present utility model that limited by appended claim, can carry out various changes, alternative and conversion.And the application's scope is not limited only to the specific embodiment of the described process of specification sheets, equipment, means, method and step.The one of ordinary skilled in the art will readily appreciate that from disclosure of the present utility model, according to the utility model can use carry out with the essentially identical function of corresponding embodiment described herein or obtain result essentially identical with it, existing and want exploited process, equipment, means, method or step future.Therefore, appended claim is intended to comprise such process, equipment, means, method or step in their scope.
Claims (9)
1. arresting gear on the SUAV (small unmanned aerial vehicle) machine is characterized in that, comprising: arrester hook and release gear; One end of described arrester hook is used for being rotationally attached to SUAV (small unmanned aerial vehicle) fuselage main body, and the other end is used for being connected with described release gear; Described release gear is fixed on the described SUAV (small unmanned aerial vehicle) fuselage, is used for fixing or discharging described arrester hook according to the external control signal that receives.
2. arresting gear on the SUAV (small unmanned aerial vehicle) machine according to claim 1, it is characterized in that: described arrester hook comprises the neck of hook and hook body;
The described neck of hook is elongated rod-shaped, and described hook is as circular-arc greater than 180 ° of central angle;
Described arrester hook rotatably be connected to the ventral of described SUAV (small unmanned aerial vehicle) away from an end of hook body.
3. arresting gear on the SUAV (small unmanned aerial vehicle) machine according to claim 1 is characterized in that:
The length of described arrester hook is no more than the length of described SUAV (small unmanned aerial vehicle).
4. arresting gear on the SUAV (small unmanned aerial vehicle) machine according to claim 1, it is characterized in that: described arrester hook is positioned at the symmetrical plane of described SUAV (small unmanned aerial vehicle);
Described arrester hook is movably connected at the center of gravity place of described SUAV (small unmanned aerial vehicle).
5. arresting gear on the SUAV (small unmanned aerial vehicle) machine according to claim 1 is characterized in that: described arrester hook away from an end of hook body by the ventral of single degree of freedom chain connection in described SUAV (small unmanned aerial vehicle).
6. a SUAV (small unmanned aerial vehicle) ground arresting gear is characterized in that, comprising: two supports placing perpendicular to ground, and be connected to elastic threads between described two supports; Described elastic threads is used for providing the power of blocking of SUAV (small unmanned aerial vehicle) flight.
7. SUAV (small unmanned aerial vehicle) according to claim 6 ground arresting gear, it is characterized in that: described elastic threads is parallel to ground, and described elastic threads is not less than the length of described SUAV (small unmanned aerial vehicle) apart from the height on ground.
8. a SUAV (small unmanned aerial vehicle) arresting system is characterized in that, comprising:
Such as arresting gear on the described SUAV (small unmanned aerial vehicle) machine of claim 1-5 any one; And,
Such as claim 6 or 7 described SUAV (small unmanned aerial vehicle) ground arresting gears.
9. a SUAV (small unmanned aerial vehicle) comprises the SUAV (small unmanned aerial vehicle) fuselage, it is characterized in that, also comprises such as arresting gear on the described SUAV (small unmanned aerial vehicle) machine of claim 1-5 any one.
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| Application Number | Priority Date | Filing Date | Title |
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| CN 201220138320 CN202642096U (en) | 2012-04-01 | 2012-04-01 | Small-scale unmanned aerial vehicle, as well as onboard arresting gear, ground arresting gear and arresting system thereof |
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| Application Number | Priority Date | Filing Date | Title |
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| CN 201220138320 CN202642096U (en) | 2012-04-01 | 2012-04-01 | Small-scale unmanned aerial vehicle, as well as onboard arresting gear, ground arresting gear and arresting system thereof |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN104670516A (en) * | 2015-02-15 | 2015-06-03 | 南京理工大学 | Rapid taking-off and landing device of air vehicle |
| CN107226215A (en) * | 2017-05-22 | 2017-10-03 | 成都飞机工业（集团）有限责任公司 | The rotary cross bar of unmanned plane blocks recovery system and recovery method |
| CN107571988A (en) * | 2017-09-06 | 2018-01-12 | 哈尔滨工业大学 | A kind of double hook device for recovery of being breasted the tape for unmanned plane |
| CN108382589A (en) * | 2018-02-05 | 2018-08-10 | 中国航空工业集团公司成都飞机设计研究所 | A kind of pair of overall aerodynamic arrangement for sending out unmanned plane and its short take-off and landing method |
| CN109398684A (en) * | 2018-11-21 | 2019-03-01 | 西安爱生无人机技术有限公司 | A kind of unmanned plane blocks hook mechanism |
| CN109625305A (en) * | 2018-12-04 | 2019-04-16 | 青岛启航弹射科技有限公司 | A kind of unmanned plane recyclable device |
| CN109747851A (en) * | 2017-11-07 | 2019-05-14 | 中国科学院沈阳自动化研究所 | A kind of small-sized fixed-wing unmanned plane recovery system |
| CN110049919A (en) * | 2016-12-13 | 2019-07-23 | 英西图公司 | The air-launched of unmanned vehicle and/or recycling and relevant system and method |
| CN110816822A (en) * | 2019-12-06 | 2020-02-21 | 西安爱生技术集团公司 | Be used for unmanned aerial vehicle to block hook band pulley hook head structure |
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2012
- 2012-04-01 CN CN 201220138320 patent/CN202642096U/en not_active Expired - Fee Related
Cited By (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104670516B (en) * | 2015-02-15 | 2016-07-06 | 南京理工大学 | The quick lifting gear of aircraft |
| CN104670516A (en) * | 2015-02-15 | 2015-06-03 | 南京理工大学 | Rapid taking-off and landing device of air vehicle |
| CN110049919A (en) * | 2016-12-13 | 2019-07-23 | 英西图公司 | The air-launched of unmanned vehicle and/or recycling and relevant system and method |
| CN110049919B (en) * | 2016-12-13 | 2023-12-01 | 英西图公司 | Airborne missions and/or recovery of unmanned aerial vehicle and related systems and methods |
| CN107226215B (en) * | 2017-05-22 | 2023-08-04 | 成都飞机工业（集团）有限责任公司 | Unmanned aerial vehicle rotary cross bar arresting recovery system and recovery method |
| CN107226215A (en) * | 2017-05-22 | 2017-10-03 | 成都飞机工业（集团）有限责任公司 | The rotary cross bar of unmanned plane blocks recovery system and recovery method |
| CN107571988A (en) * | 2017-09-06 | 2018-01-12 | 哈尔滨工业大学 | A kind of double hook device for recovery of being breasted the tape for unmanned plane |
| CN109747851A (en) * | 2017-11-07 | 2019-05-14 | 中国科学院沈阳自动化研究所 | A kind of small-sized fixed-wing unmanned plane recovery system |
| CN109747851B (en) * | 2017-11-07 | 2021-06-01 | 中国科学院沈阳自动化研究所 | Small-size fixed wing unmanned aerial vehicle recovery system |
| CN108382589A (en) * | 2018-02-05 | 2018-08-10 | 中国航空工业集团公司成都飞机设计研究所 | A kind of pair of overall aerodynamic arrangement for sending out unmanned plane and its short take-off and landing method |
| CN109398684A (en) * | 2018-11-21 | 2019-03-01 | 西安爱生无人机技术有限公司 | A kind of unmanned plane blocks hook mechanism |
| CN109398684B (en) * | 2018-11-21 | 2024-03-22 | 西安爱生无人机技术有限公司 | Unmanned aerial vehicle arresting hook mechanism |
| CN109625305A (en) * | 2018-12-04 | 2019-04-16 | 青岛启航弹射科技有限公司 | A kind of unmanned plane recyclable device |
| WO2020156587A1 (en) | 2018-12-04 | 2020-08-06 | 青岛启航弹射科技有限公司 | Unmanned aerial vehicle recovery apparatus |
| CN109625305B (en) * | 2018-12-04 | 2024-02-13 | 青岛启航弹射科技有限公司 | Unmanned aerial vehicle recovery unit |
| CN110816822A (en) * | 2019-12-06 | 2020-02-21 | 西安爱生技术集团公司 | Be used for unmanned aerial vehicle to block hook band pulley hook head structure |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130102 Termination date: 20160401 |