CN202686760U - Free gliding system with safety protection device - Google Patents

Free gliding system with safety protection device Download PDF

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Publication number
CN202686760U
CN202686760U CN 201220291735 CN201220291735U CN202686760U CN 202686760 U CN202686760 U CN 202686760U CN 201220291735 CN201220291735 CN 201220291735 CN 201220291735 U CN201220291735 U CN 201220291735U CN 202686760 U CN202686760 U CN 202686760U
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safety
cableway
cable
support tower
guard
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CN 201220291735
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Chinese (zh)
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谭大刚
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Abstract

The utility model relates to a free gliding system with a safety protection device, which is characterized in that a flight path rope way is spanned between an upper-end support tower and a lower-end support tower, wherein the safety protection device capable of sliding along with the flight path rope way is arranged on the flight path rope way; a safety cable capable of automatic shrinkage is arranged on the safety protection device; a suspension type hang glider is hung at the lower end of the safety cable; and a launching platform is arranged in front of the upper-end support tower.

Description

Free glide system with safety guard
Technical field
The utility model belongs to expands the sports events field, particularly relates to a kind of glide system with safety guard.
Background technology
In human-powered flight's motion, unpowered gliding flight is owing to can realize human dream of freely circling in the air as bird by self strength since ancient times aloft, do not produce again the environmental pollutions such as noise and exhaust emission awing fully, so become immediately a top manpower apparatus work after certainly carrying out.Produce huge noise and discharging waste gas contaminated environment, make the surrounding population sidelong glance compare with various ground, aerial, water surface motorcycling, become stark contrast.One of extreme sport that human-powered flight motion or the present age are the most Eco-Fashion, from mid-term in last century along with at the hang gliding equipment constantly along improving airworthiness, the progress of lightweight and portability direction, the flight of the hang gliding wing is in fashion in the whole world.(the utility model people's last invention " hang gliding wing Manpower driver and ground surface simulated training rack thereof " is (ZL200710010928.8) supporting with hang gliding, drive all-wing aircraft so that motorless hang gliding becomes manpower, more increase the airworthiness of human-powered flight's motion.) still, although existing hang gliding requires and improves the aspects such as airworthiness and safety that at reduction apparatus bulking value cost and flight weather con dition very much progress has been arranged, because gliding flight must carrying out at certain altitude in the air, for the participant of each gliding flight beginner particularly, flight safety is a most worrying problem all the time.Inherently safe in the study flight course is worried, is that the flight of restriction hang gliding can't obtain as bungee jumping, surfing, and rock-climbing waits the topmost factor of the such Popularization of extreme sport.See that the protection that rock climbing person student or contestant have the assistant to control the security insurance rope prevents that unexpected tenesmus is injured; people look forward to also learning taking off of human-powered flight under the protection of security insurance rope for the people who begins to learn hang gliding flight naturally; the skill of controlling and land, and can freely circle in the air.Because the hang gliding sporting flying is being taken off; up-and-down movement as rock-climbing is not only arranged in flight and the landing mission; also simultaneously with the forward sporting flying of suitable speed, can not have the assistant with identical speed follow-up and control safety cable protect aircraft and sportsman when meeting accident not with collision on the ground.If create a kind of energy and sporting flying advanced in unison and the safety cable apparatus system that can bump with flying height self-align restriction aircraft and ground, then the popular primary stage of learning the human-powered flight just can be removed and be feared to free the trouble and worry of safety misadventure of falling.Can also there be so far in the world such human-powered flight's protection equipment to occur.
The beginning of this century, so-called " cableway hang gliding " appearred in the U.S., and outdoor activity projects such as " children's cableway hang glidings " also appears in Germany.Its equipment is introduced as A level extreme sport equipment recommendation by the many tourist attractions of China, is known as " flying over the earth as bird ", also attracts to many youthful participations and numerous spectators' concern.But the very fast discovery of participant and viewer, this what is called " flight apparatus " that the simple and crude profile of hang gliding arranged only is fixed on the decoration under the conventional steel wire cableway parsing davit in fact.Although the downslide process also stimulates and basic guarantee safety very much, to tie up position be roughly to become the level to whole what is called " flight " process except being hung, and its impression and conventional steel cableway be slippery not to have essential distinction, but experiences far from each other with the motion of hang gliding flight.Even if people carry out up to a hundred times " flight " exercise at this " cableway hang gliding ", the participant still can't grasp taking off of hang gliding, controls flight and landing skill.So this existing " cableway hang gliding " can not learn in order to satisfy the beginner demand of the safety assurance of real hang gliding or other man-power aircraft tool airmanships fully although technique device has solved sports safety own.
Based on above-mentioned viewpoint; the applicant has initiated the imagination of carrying out the human-powered flight under safety guard-safeguard in 2010; on the technical development basis that the simulated training rack cableway follows up in last invention " hang gliding wing Manpower driver and ground surface simulated training rack thereof "; add the longest spacing safety cable capstan winch technology of self-constriction; in the gliding flight process, do not need the assistant to participate in; do not consume any energy; solve to advantages of simple the human-powered flight and begun to learn the training stage to the technical barrier that aircraft and aviator are equipped with the safety cable that certainly follows up, invented the utility model " the free glide of band safety guard-safeguard system ".
Summary of the invention
Goal of the invention: the utility model provides a kind of free glide system with safety guard, its objective is that solving glides and expand in the sports events in safety, need personnel to control, glide problem that aspects such as consuming the energy in degree of freedom and the aviator's glide process exists.
Technical scheme:
A kind of free glide system with safety guard, it is characterized in that: between high-end support tower and low side support tower, set up the flight path cableway, being provided with on the flight path cableway can be along the safety guard of flight path cableway sliding, safety guard is provided with the safety cable that can automatically shrink, and the hang gliding wing is hung in the lower end of safety cable; The place ahead that is positioned at high-end support tower is provided with the platform that takes off.
Be arranged with circulating trailing cable in parallel with the flight path cableway between high-end support tower and the low side support tower; Be provided with driving runner and runner on the top of high-end support tower and low side support tower, the circulation trailing cable is enclosed ring and is enclosed between driving runner and the runner, drives runner and is connected with motor and driving device.
Described safety guard is comprised of suspension bracket, cableway wirerope assembly pulley, safety cable capstan wheel and rectification outer cover; The the first cableway wirerope assembly pulley and the second cableway wirerope pulley block frame that are installed in front and back end, suspension bracket top are located on the flight path cableway; Safety cable capstan wheel with built-in clockwork spring is installed on the center shaft at suspension bracket middle part; Safety cable one end that can automatically shrink is fixed and is wrapped on the safety cable capstan wheel, and the other end passes the fork guard that is installed in the suspension bracket lower end and can pull out, but is connected with the reinsurance hook by the safety hook seat; But the reinsurance hook is connected with the hang gliding wing; Also be respectively equipped with wirerope rectification outer cover, pulley rectification outer cover, safety lock capstan wheel rectification outer cover and safety hook rectification outer cover on the safety guard.
Be provided with little hook at the circulation trailing cable, an end of additional connecting strand hangs on the little hook, and the link that the other end passes on the safety guard adds on the protection link that hangs over hang gliding.
The relevant position of safety cable root is fixed with a spacing pillar, can frame when maximum spacing elongation of safety cable be fixed on the fork guard on the suspension bracket.
Advantageous effect:
The characteristics that the utility model has utilized the minimal friction of the omnidistance weight capacity of wire cableway and cableway pulley to roll fast and to advance and substantially mate with hang gliding gliding flight speed at wire cableway flexibly connect cableway pulley and the hang gliding wing with the self-constriction safety cable.Control in the overall process of gliding flight participating in the aviator, do not consume any energy, for hang gliding and aviator thereof provide straight line path flight omnidistance safety guard-safeguard.Fender guard is being when omnidistance flight realizes unexpected protection; because this device is little at the wirerope coefficient of rolling friction; fender guard is in inclined cableway glides; the potential energy dress of device is changed to kinetic energy and can also offers help to the glide of aircraft, and the pulling force of safety cable can not cause resistance increment to cause on the contrary the pulling force that advances to aircraft.Need to particularly point out, be all cableway and use, the utility model has essential distinction with existing " cableway hang gliding ".Be that cableway wirerope of the present utility model and assembly pulley (are implemented protection situation or aircraft and flown to its maximum gliding distance but do not arrive the flight path cableway terminal point) not bear hang gliding and aviator's total force except the aircraft accidental falling occurs in the normal flight process; only bear the own weight loading of fender guard (only for the former below 1/10th); so the sag of chain of wirerope, day-to-day operation assembly pulley Rolling wear and cableway design and construction cost and ropeway operation maintenance cost etc. all are significantly less than existing " cableway hang gliding ".For example the apparatus of existing " cableway hang gliding " slides each two wirerope of cableway up-downgoing, also need to be equipped with control telecommunication connection and trailing cable, sliding downwards and following apparatus is retracted the reciprocal process of eminence takeoff point all needs with electric capstan power driven and control.And flight path cableway of the present utility model only needs a load-bearing wirerope, is freely gliding by high-end in the low side flight course, and circulation trailing cable and hang gliding break away from fully, do not need to consume any driving electric power.
So; application of the present utility model; not only can solve vast hang gliding airhog looks forward to learning taking off of hang gliding flight for the stage of begining to learn under the protection of security insurance rope; the skill of controlling and land; carry out the wonderful dream of freely circling in the air; exempt the safety worries of sporting flying person in begining to learn flight training; greatly enlarge the audient's who participates in this motion scope and number; can also guarantee when guaranteeing personal security that expensive flight equipment is not subjected to contingency generation loss; greatly improve the service efficiency of trial ground and hang gliding equipment, the economic benefit that increases must substantially exceed the input of cableway and fender guard construction.
The utility model supporting after the repacking hang gliding wing is extractd, as the take a flight test application in navigation channel of the safety of the various Manpower-drivens flight equipment of taking a flight test, can exempt the middle various losses that may have an accident and bring of taking a flight test of Manpower-driven flight equipment, be conducive to promote the research and development just of Manpower-driven aircraft.(each aircraft contestant can pull out a distance calculating aerial flight distance to safety cable by takeoff point fully if use in the safety performance contest place as various intention man-power aircrafts, under hanging, maximum safety cable length slides into the safe landing of cableway mid point), can avoid present high platform human-powered flight to match the restriction that to hold the water surface (thereby also must be summer), avoid aviator and equipment to suffer water soaking, saved wrecker and equipment expense.Can realize that the contestant flies several times and get the highest achievement, spectators can more closely watch from every side, increase the appreciative value of contest, the mass participation so that this type of contest is more convenient for.
The utility model is expanded sports events equipment as the novel popular Eco-Fashion leisure limit and is used, and must be subject to its real flight experience young man's favor, becomes the most widely application.Compare with existing " cableway hang gliding " project, with its exclusive independent intellectual property right and low manufacturing expense, more energy-conserving and environment-protective reach lower operation and maintenance cost, more real flight impression, more airmanship knowledge intension etc. advantage, more fashion obtains wider popularization in the whole country and adopts, and becomes the popular platform that China popularizes the hang gliding sporting flying.
Description of drawings:
Fig. 1 is keystone configuration scheme drawing of the present utility model;
Fig. 2 is pylon top, the utility model left side structure for amplifying scheme drawing;
Fig. 3 is pylon top, the utility model right side structure for amplifying scheme drawing;
Fig. 4 is the utility model safety guard structural representation;
Fig. 5 is the local structure for amplifying scheme drawing of safety cable Fig. 4 when all pulling out;
Fig. 6 is that the utility model flight path cableway sets up scheme drawing;
Fig. 7 is that the utility model circulation trailing cable is carried additionally the mode structural representation.
Mark 1 among the figure: flight path cableway, 2: suspension bracket, 3: the first cableway wirerope assembly pulleys; 4: the second cableway wirerope assembly pulleys, 5: built-in clockwork spring, 6: the safety cable capstan wheel; 7: safety cable, 8: but the reinsurance hook, 9: wirerope rectification outer cover; 10: pulley rectification outer cover, 11: safety lock capstan wheel rectification outer cover, 12: safety hook rectification outer cover; 13: center shaft, 14: spacing pillar, 15: the safety hook seat; 16: fork guard, 17: link, 18: high-end support tower; 19: low side support tower, 20: the first anchoring devices, 21: the second anchoring devices; 22: circulating trailing cable; 23: motor and driving device, 24: the platform that takes off, 25: the hang gliding wing; 26: mobile jib; 27: protection link, 28: drive runner, 29: runner; 30: little hook, 31: additional connecting strand.
The specific embodiment:Below in conjunction with accompanying drawing the utility model is described further:
Represented among Fig. 1 that the free glide of the utility model band safety guard-safeguard system forms overall picture, represented that respectively height support tower top is detailed in two ringlet E, F among the figure, represented with Fig. 2,3 respectively.This system forms and comprises: the flight path cableway 1 that is supported by high-end support tower 18 and low side support tower 19 reaches the circulating trailing cable 22 parallel with cableway; the safety guard that moves on the cableway; be positioned at the platform 24 that takes off before the high-end pylon, be hung on safety guard safety cable lower end through four major parts such as the repacking hang gliding wing 25 grades.The circulation trailing cable 22 of high-end support tower 18 and low side support tower 19 a little higher than wireropes, being closed-loop is enclosed between driving runner 28 and the runner 29, the axle that drives runner 28 and runner 29 is separately fixed on high-end support tower 18 and the low side support tower 19, by being fixed on motor and driving device 23 on the high-end support tower 18, driving runner 28.
Fig. 4 has described to remove safety guard structure behind the rectification outer cover (dotted portion among the figure), internal state when Fig. 5 represents that safety cable is pulled out fully, as shown in Figure 4.Safety guard is by suspension bracket 2; be installed in the first cableway wirerope assembly pulley 3 and the second cableway wirerope assembly pulley 4 of suspension bracket 2 front and back ends; be installed in the safety cable capstan wheel 6 with built-in clockwork spring 5 at suspension bracket 2 middle parts; automatically shrinking safety cable 7 one ends fixes and is wrapped on the safety cable capstan wheel 6; the other end pass fork guard 16 pull out connecting safety hook seat 15 and can be free reinsurance hook 8; wirerope rectification outer cover 9; pulley rectification outer cover 10; safety lock capstan wheel rectification outer cover 11, and safety hook rectification outer cover 12 parts such as grade form.
The first cableway wirerope assembly pulley 3 and the second cableway wirerope assembly pulley 4 all each freely hang oneself heavy pulley and lower lock-bit pulley combination form.The cableway wirerope passes between top sheave and lower sheave when installing operation.
The mounting means of noting built-in clockwork spring 5 is: its interior end is fixed on the center shaft 13 of safety cable capstan wheel 6, and fixedly on safety cable capstan wheel 6 cards, when self-constriction safety cable 7 is pulled out fully, built-in clockwork spring 5 is complete tight condition to an outer end.Loosening of built-in clockwork spring 5 can drive the 7 winding withdrawals of safety cable capstan wheel 6 turning handle safety cables when turning round.Another key feature of safety cable 7 mounting structures is: when self-constriction safety cable 7 is pulled out fully; the spacing pillar 14 meeting framves that safety cable 7 root relevant positions are fixed are on the fork guard 16 that is fixed on the suspension bracket 2, and realization safety cable 7 fender guard when the spacing elongation of maximum can be born the safe bearing load of regulation.In order to reduce the suffered air resistance of safety guard when the quick roll-sliding of cableway wirerope; have wirerope pulley rectification outer cover 9 and pulley rectification outer cover 10 to be installed in respectively the outside of the first cableway wirerope assembly pulley 3 and the second cableway wirerope assembly pulley 4, safety lock capstan wheel rectification outer cover 11 is installed in safety cable capstan wheel 6 outsides.And safety hook rectification outer cover 12 can be along sliding on the safety cable 7, but after reinsurance hook 8 hangs up properly with aircraft top suspension ring, but slide reinsurance hook 8 is covered with aircraft top suspension ring again.For the free left/right rotation of realizing aircraft in the flight course in addition 180 degree turn back, but be installed in the reinsurance hook 8 in the safety cable free end safety hook seat 15, related safety hook rectification outer cover 11 and the man-power aircraft hung can rotate freely as horizontal 360-degree take safety cable as the longitudinal axis in safety hook seat 15 together.Suspension bracket 2 is provided with the link 17 of side opening osculum towards the high-end end of cableway.
Fender guard adopts light material as far as possible under the wear-resistant prerequisite of proof strength, reduce the weight of fender guard, with minimizing advance friction drag and inertia.For example all fairings all adopt light plastic.
The platform 24 that takes off is located at high-end support tower 18 fronts of inclination wire cableway on the ground of low side support tower 19 1 sides, have the passage ladder from ground sensible table top, table top is provided with guardrail except all the other each edges towards the edge that takes off of low side pylon.
The hang gliding wing 25 adopts existing High Performance commodity, through having installed protection link 27 additional at its mobile jib 26 hang gliding center-of-gravitys position, supports the use after the repacking.
In Fig. 6, provide heeling path cableway and set up landform requirement schematic side view, amplified the vertical direction ratio among the figure for expression makes things convenient for.Heavy line represents wire cableway among Fig. 6, and dotted line represents typical flight path (aircraft and aviator's barycenter trajectory), and the A of Fig. 6 typical case flight path, B and C represent that respectively gliding ability is high, the hang gliding flight result who neutralizes low.Wherein the back segment of B and C is all hung downslide at safety guard and is walked to flight path cableway terminal point after safety cable is pulled out fully.The penumbra line represents typical ground (comprise and taking off and landing platform), for seeing clearly, the relative vertical scale of horizontal proportion has been shortened.Only show in the accompanying drawing to build on wire cableway and the ground on level land and the relative height requirement of the landing platform that takes off, wirerope two ends design antenna height required support tower and anchor mechanism all adopt the universal design Specification Design to make and installation.If high-end pylon builds on the higher landform of relative low side, then take off platform and high-end pylon attach structure change.The utility model adopts conventional wire cableway, only need to set up a wirerope, and wire cableway is being projected as straight line from overlooking ground.Flight path cableway 1 is the inclination wire cableway that is erected between high-end support tower 18 and the low side support tower 19, there are respectively the first anchoring device 20 and the second anchoring device 21 in cableway wirerope two with its tension and are fixed in ground, on the ground between high-end support tower 18 and the low side support tower 19 or the water surface any obstacle must not be arranged.Flight path cableway 1 is characterised in that: the wirerope weight capacity is greater than the safe bearing load (be aircraft weight add aviator's body weight take advantage of 1.5 to 2 times of safety factors) of regulation on the complete trails of flight path cableway 1; And flight path cableway 1 wirerope antenna height; the cooperation result of loadintensity and landform; must guarantee the initial segment (on launching platform) and landing runway end on being positioned at the cableway takeoff runway, whole flight path wirerope 1 all the other everywhere overhead (water surface) of cableway wirerope highly (hang the safe bearing load sag of chain actual measurement of regulation by fender guard at this place) all greater than fender guard safety cable 7 maximum spacing pull out length add hang gliding together with hang and participate in glide personnel height.
Heeling shown in Figure 6 path flight cableway scheme can be built on the level land, also can utilize the construction of nature inclination landform, to reduce the building height of wirerope support tower and the platform that takes off.In the middle of the flight path water surface can be arranged.Can lengthen flight path (keep the cableway ramp rate, adapt with employing hang gliding glide ratio) on increase takeoff point height basis.According to present hang gliding airworthiness level, present embodiment can specifically adopt 150 meters wirerope flight paths of 15 meters elevation drops of platform and pick-up point cableway that takes off according to accompanying drawing 3.
In Fig. 7, circulating trailing cable 22 is closed-loop and is enclosed between driving runner 28, the runner 29, the axle that drives runner 28, runner 29 is separately fixed on high-end support tower 18 and the low side support tower 19, circulating trailing cable 22 comes and goes two all a little higher than wire cablewaies 1 and parallel with it, drive runner 28 by motor-driven and install 23 driving unidirectional rotation, so that the trailing cable of close wire cableway 1 is by being moved to high extreme direction by low side.Two symmetric position is respectively with 4 little hooks 30 on the circulating trailing cable 22; when retracting cableway to the fender guard that is in the cableway low side when high-end together with hang gliding 25; first hang gliding is transferred to head towards high-end cableway direction; (fender guard is motionless); hang up an end of additional connecting strand 31 at one of little hook 30 of circulation trailing cable 22; additional connecting strand 31 passes that link 17 another terminations then add on the protection link 27 that hangs over hang gliding 25 on the fender guard, needs safety hook rectification outer cover 12 along sliding to expose protection ring 27 on the safety cable for this reason.By starter motor realize fender guard together with hang gliding by low side to high-end transmission, additional connecting strand 31 make safety cable 7 suitable retraction fender guards can promoting hang gliding 25 in high-end drawing.When fender guard be pulled together with hang gliding 25 cableway high-end after; motor stops; the staff can be additional connecting strand 31 from little hook 30; link 17 and 27 disengagements of protection link are taken off; so that fender guard and hang gliding 25 break away from fully with circulating trailing cable 22; simultaneously hang gliding is transferred to head towards the low extreme direction of cableway, finish the person of letting on and handle hang gliding from the platform that takes off to the omnidistance preparation of under safety guard-safeguard, freely gliding of low side landing point.
Essential characteristic of the present utility model is, the design and construction of flight path cableway and the landing platform that takes off is when satisfying customer requirements and suiting measures to local conditions according to site topography, and the most important technical requirements that all must satisfy behind the safety guard in the outfit is: the wirerope weight capacity is greater than the safe bearing load of regulation (be hang gliding weight add typical participant person's body weight take advantage of 1.5 to 2 times of safety factors) on the complete trails of flight path cableway; And flight path cableway wirerope antenna height; the cooperation result of loadintensity and landform; must guarantee terminal two places of the initial segment (at the launching platform face) on being positioned at the cableway takeoff runway and landing runway, whole flight path wirerope all the other everywhere the terrain clearance of cableway wirerope (hanging the safe bearing load sag of chain actual measurement of regulation at this place by fender guard) all add that greater than the maximum spacing length of pulling out of fender guard safety cable aircraft together with hanging aviator highly.The result that cooperates of landing runway height and this section cableway height; hang the hang gliding actual verification after pulling out fully with the safety guard safety cable at the terminal wirerope of landing runway, hang gliding is mixed can normally walk about on ground after typical body weight personnel uprightly hang and is advisable.

Claims (5)

1. free glide system with safety guard, it is characterized in that: between high-end support tower (18) and low side support tower (19), set up flight path cableway (1), being provided with on the flight path cableway (1) can be along the safety guard of flight path cableway (1) slip, safety guard is provided with the safety cable (7) that can automatically shrink, and the hang gliding wing (25) is hung in the lower end of safety cable (7); The place ahead that is positioned at high-end support tower (18) is provided with the platform that takes off (24).
2. the free glide system with safety guard according to claim 1 is characterized in that: be arranged with circulating trailing cable (22) in parallel with flight path cableway (1) between high-end support tower (18) and the low side support tower (19); Be provided with driving runner (28) and runner (29) on the top of high-end support tower (18) and low side support tower (19), circulation trailing cable (22) is enclosed ring and is enclosed between driving runner (28) and the runner (29), drives runner (28) and is connected with motor and driving device (23).
3. the free glide system with safety guard according to claim 1, it is characterized in that: described safety guard is comprised of suspension bracket (2), cableway wirerope assembly pulley, safety cable capstan wheel (6) and rectification outer cover; The the first cableway wirerope assembly pulley (3) and the second cableway wirerope assembly pulley (4) that are installed in suspension bracket (2) front and back end, top are erected on the flight path cableway (1); Safety cable capstan wheel (6) with built-in clockwork spring (5) is installed on the center shaft (13) at suspension bracket (2) middle part; Safety cable (7) one ends that can automatically shrink are fixed and are wrapped on the safety cable capstan wheel (6), and the other end passes the fork guard (16) that is installed in suspension bracket (2) lower end and can pull out, by safety hook seat (15) but be connected with reinsurance hook (8); But reinsurance hook (8) is connected with the hang gliding wing (25); Also be respectively equipped with wirerope rectification outer cover (9), pulley rectification outer cover (10), safety lock capstan wheel rectification outer cover (11) and safety hook rectification outer cover (12) on the safety guard.
4. the free glide system with safety guard according to claim 1; it is characterized in that: be provided with little hook (30) at circulation trailing cable (22); one end of additional connecting strand (31) hangs on the little hook (30), and the link (17) that the other end passes on the safety guard adds on the protection link (27) that hangs over hang gliding (25).
5. the free glide system with safety guard according to claim 1; it is characterized in that: the relevant position of safety cable (7) root is fixed with a spacing pillar (14), can frame when maximum spacing elongation of safety cable (7) be fixed on the fork guard (16) on the suspension bracket (2).
CN 201220291735 2012-06-20 2012-06-20 Free gliding system with safety protection device Expired - Fee Related CN202686760U (en)

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CN107261508A (en) * 2017-08-17 2017-10-20 镇江市丹徒区硕源材料科技有限公司 A kind of entertainment systems
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CN107380438A (en) * 2017-08-17 2017-11-24 镇江市丹徒区硕源材料科技有限公司 A kind of bungee jumping aircraft and its application
CN107380437A (en) * 2017-08-17 2017-11-24 佛山市领卓科技有限公司 One kind amusement aircraft and its application
CN107298183A (en) * 2017-08-17 2017-10-27 佛山市领卓科技有限公司 A kind of rod failure aircraft and its application
CN108583887A (en) * 2017-08-17 2018-09-28 佛山市领卓科技有限公司 A kind of amusement aircraft and its application
CN108568116A (en) * 2017-08-17 2018-09-25 镇江市丹徒区硕源材料科技有限公司 A kind of entertainment systems
CN108553917A (en) * 2017-08-17 2018-09-21 镇江市丹徒区硕源材料科技有限公司 A kind of bungee jumping aircraft and its application
CN107672798A (en) * 2017-10-04 2018-02-09 佛山市领卓科技有限公司 A kind of Electric aircraft
CN107776887A (en) * 2017-11-23 2018-03-09 成都天空营地科技有限公司 A kind of flight experience/elementary training aerodone
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