CN102020017A - Hollow inflatable wing type paraglider - Google Patents
Hollow inflatable wing type paraglider Download PDFInfo
- Publication number
- CN102020017A CN102020017A CN2009100188109A CN200910018810A CN102020017A CN 102020017 A CN102020017 A CN 102020017A CN 2009100188109 A CN2009100188109 A CN 2009100188109A CN 200910018810 A CN200910018810 A CN 200910018810A CN 102020017 A CN102020017 A CN 102020017A
- Authority
- CN
- China
- Prior art keywords
- molding
- paraglider
- spacing
- moulding
- spacer film
- Prior art date
- 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.)
- Pending
Links
Images
Landscapes
- Emergency Lowering Means (AREA)
Abstract
The invention discloses a hollow inflatable wing type paraglider, which belongs to the technical field of manufacturing of sports equipment. The paraglider consists of molding and spacing membranes, an upper wing surface, a lower wing surface, ventilation holes, a charging connector and lanyards, wherein a plurality of molding and spacing membranes which are transversely arranged at equal intervals are connected between the upper wing surface and the lower wing surface; all the internally arranged molding and spacing membranes are provided with the ventilation holes; the outermost molding and spacing membrane is provided with the charging connector; and the lanyards are fixed at a front end point and a rear end point on a straight line in which the lower wing surface is tangential to each molding and spacing membrane. When the paraglider is used, the paraglider is opened, and is aerated by the charging connector; after the space of each molding and spacing membrane is filled with gas, the entire paraglider has an airplane wing shape due to the molding and positioning action of the molding and spacing membranes, so the windward lifting power and the gliding capacity can be improved; and the paraglider has the advantages of rational design, simple structure, convenience of use and the like.
Description
Technical field
The present invention relates to a kind of hollow inflation all-wing aircraft type gliding parachute, belong to technical field of manufacture of sports.
Background technology
Gliding parachute originated from 1984, be by France a collection ofly have deep love for parachuting, a kind of sporting flying of aircrew's invention of hang gliding, very popular in states such as American-European and Japan at present, also popular in China mainland and Taiwan.
Gliding parachute itself has no any power, and why it can fly, and shows after canopy is full of air (flying wing) the special shape, entirely by aviator's control, in conjunction with planting specific character (aerodynamic force) flight in the atmosphere.The parachute of traditional type, promptly general parachute can only produce the decline resistance aloft, does not have lift, and gliding parachute aloft can generation speed and lift in the flight course, and its speed and lift are bigger than its resistance far away.Because textural, gliding parachute canopy endothecium structure is provided with air bag, and before not being full of air, gliding parachute does not have the corner angle of essence, in case inner bladder is full of air, corner angle will appear in the forward position of gliding parachute.Like this, when gliding parachute flies aloft relative air-flow is drawn away mobilely up and down respectively by aerofoil, resistance is parallel with the other side's wind-force, and weight combines with wing top air, and gliding parachute generation speed is advanced.
Polytype sports type gliding parachute is arranged in the prior art, but exist mostly airworthiness not good, lack when flying down with the wind defective or deficiency such as due lift, the pretty good gliding parachute of various aspects of performance is certainly also arranged, but because of its complex structure, cost is high can't popularize.
Summary of the invention
The present invention is directed to the deficiencies in the prior art, provide a kind of simple in structure, cost is low, easy to use, hollow inflation all-wing aircraft type gliding parachute with aircraft airfoil section.
The objective of the invention is to be achieved through the following technical solutions:
A kind of hollow inflation all-wing aircraft type gliding parachute is by moulding spacer film, top airfoil, lower aerofoil, air extractor vent, charging connector and umbrella rope are formed, wherein, between last lower aerofoil, be connected with some equidistant transversely arranged moulding spacer films, be equipped with air extractor vent on the moulding spacer film of internal arrangement, outermost moulding spacer film is provided with charging connector, on the tangent straight line of lower aerofoil and per pass moulding spacer film, be fixed with the umbrella rope on the position of rear and front end point.
The spacer film parts that described moulding spacer film is a kind of aircraft wing moulding, transversely arranged being fixed between the lower aerofoil forms and arranges also the aerofoil modeling structure of ventilation mutually separately.
When the present invention uses, open gliding parachute, and by charging connector to wherein the inflation, be full of the space of each moulding spacer film when gas after, because the moulding positioning action of moulding spacer film, the whole umbrella wing presents the moulding as the aircraft wing, during glide, the sportsman is fixed on the gliding parachute bottom by the umbrella rope, then from the hilltop or eminence be fit to take-off place and take off, in the landing process, present aircraft wing moulding moulding spacer film 1 and can increase lift down with the wind, promote the glide ability, make farther that the sportsman glides, operation control is more accurate.
It should be noted that since the present invention for cost-cutting, structure is simpler, there is no essential or safety equipments such as flying suit, cover band, safety cap, gloves, footwear, eyes protector, instrument on it, when the sportsman uses, should carry these must or safety equipment.For safety, preferably carry auxiliary parachute or urgent umbrella, because doing that thermal current spirals or during high flight, running into some extraordinary circumstances sometimes; The size dimension of auxiliary parachute that carries or urgent umbrella should be selected suitable dimensions according to everyone body weight difference.
The present invention is simple in structure, and cost of manufacture is lower, and it is fine to use effect, is highly suitable for common fan, is convenient to popularize, and then makes this motion more popular.The present invention has reasonable in design, simple in structure, easy to use, low cost and other advantages.
Description of drawings
Fig. 1 is a structural representation of the present invention.
Wherein: 1, moulding spacer film, 2, top airfoil, 3, lower aerofoil, 4, air extractor vent, 5, charging connector, 6, the umbrella rope.
The specific embodiment
The present invention is further illustrated below in conjunction with accompanying drawing:
A kind of hollow inflation all-wing aircraft type gliding parachute, form by moulding spacer film 1, top airfoil 2, lower aerofoil 3, air extractor vent 4, charging connector 5 and umbrella rope 6, as shown in Figure 1, wherein, between top airfoil 2 and lower aerofoil 3, be connected with some equidistant transversely arranged moulding spacer films 1, be equipped with air extractor vent 4 on the moulding spacer film 1 of internal arrangement, outermost moulding spacer film 1 is provided with charging connector 5, on the tangent straight line of lower aerofoil 3 and per pass moulding spacer film 1, be fixed with umbrella rope 6 on the position of rear and front end point.
During use, open gliding parachute, in moulding spacer film 1, charge into air by charging connector 5, be full of the space of each moulding spacer film 1 when gas after, just present wing shapes, because the moulding positioning action of moulding spacer film 1, the whole umbrella wing presents the moulding as the aircraft wing.
During glide, be ready to essential or safety equipments such as flying suit, cover band, safety cap, gloves, footwear, eyes protector, instrument, the sportsman is fixed on the gliding parachute bottom by the umbrella rope, then from the hilltop or eminence be fit to take-off place and take off, in the landing process, presenting aircraft wing moulding moulding spacer film 1 can increase lift down with the wind, promotes the glide ability, make farther that the sportsman glides, operation control is more accurate.
Claims (2)
1. hollow inflation all-wing aircraft type gliding parachute, it is characterized in that: form by moulding spacer film, top airfoil, lower aerofoil, air extractor vent, charging connector and umbrella rope, wherein, between top airfoil, lower aerofoil, be connected with some equidistant transversely arranged moulding spacer films, be equipped with air extractor vent on the moulding spacer film of internal arrangement, outermost moulding spacer film is provided with charging connector, on the tangent straight line of lower aerofoil and per pass moulding spacer film, is fixed with the umbrella rope on the position of rear and front end point.
2. a kind of hollow inflation all-wing aircraft type gliding parachute according to claim 1, it is characterized in that, the spacer film parts that described moulding spacer film is a kind of aircraft wing moulding, transversely arranged being fixed between top airfoil, the lower aerofoil forms and arranges also the aerofoil modeling structure of ventilation mutually separately.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009100188109A CN102020017A (en) | 2009-09-11 | 2009-09-11 | Hollow inflatable wing type paraglider |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2009100188109A CN102020017A (en) | 2009-09-11 | 2009-09-11 | Hollow inflatable wing type paraglider |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN102020017A true CN102020017A (en) | 2011-04-20 |
Family
ID=43861888
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2009100188109A Pending CN102020017A (en) | 2009-09-11 | 2009-09-11 | Hollow inflatable wing type paraglider |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN102020017A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102897320A (en) * | 2012-10-20 | 2013-01-30 | 向言李 | Paraglider capable of being folded and unfolded automatically |
| CN109018337A (en) * | 2018-06-27 | 2018-12-18 | 深圳市百川融创科技有限公司 | Automatically the ram air parachute of umbrella and recycling has been manipulated |
-
2009
- 2009-09-11 CN CN2009100188109A patent/CN102020017A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102897320A (en) * | 2012-10-20 | 2013-01-30 | 向言李 | Paraglider capable of being folded and unfolded automatically |
| CN102897320B (en) * | 2012-10-20 | 2016-03-30 | 向言李 | A kind of self-jacked gliding parachute |
| CN109018337A (en) * | 2018-06-27 | 2018-12-18 | 深圳市百川融创科技有限公司 | Automatically the ram air parachute of umbrella and recycling has been manipulated |
| CN109018337B (en) * | 2018-06-27 | 2023-12-01 | 深圳市百川融创科技有限公司 | Automatic control plays punching press parafoil of umbrella and recovery |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN104925243B (en) | A kind of variable inflated type buoyance lift integration stratospheric airship of span | |
| CN209382267U (en) | A kind of combined type vertically taking off and landing flyer | |
| CN207417149U (en) | A kind of double lift culvert vertical take-off and landing aircrafts based on tilting duct | |
| CN106864744A (en) | A kind of co-axial rotor variant vertically taking off and landing flyer | |
| CN106184741A (en) | A kind of flying wing type ducted fan VUAV | |
| CN106005396A (en) | Combined jet-flow control device for helicopter rotor blade and control method of combined jet-flow control device | |
| CN105857579A (en) | Propeller airplane | |
| CN109760832A (en) | A kind of VTOL fixed-wing unmanned vehicle | |
| CN104964610B (en) | A kind of unmanned target drone of waverider-derived | |
| CN205686600U (en) | The aircraft that a kind of dirigible is combined with many rotors | |
| CN102020017A (en) | Hollow inflatable wing type paraglider | |
| CN201494626U (en) | Hollow inflatable wing-type paraglider | |
| CN206087302U (en) | All -wing aircraft formula ducted fan VTOL unmanned aerial vehicle | |
| CN209209028U (en) | One kind is verted three rotor VTOL all-wing aircraft of type | |
| CN203094446U (en) | Parawing system for wheel type parawing | |
| CN209650530U (en) | A kind of rotatable Multi Role Aircraft wing structure | |
| CN105329447A (en) | Front air chamber automatically-forming punched parafoil | |
| CN203975214U (en) | A kind of system of wafing that flies of utilizing natural wind motion | |
| CN207417148U (en) | A kind of single lift culvert vertical take-off and landing aircraft based on tilting duct | |
| CN201334118Y (en) | Double-layered parachute | |
| CN206087332U (en) | Flight slide convenient to take off and land | |
| CN205221123U (en) | Automatic punching press parafoil that takes shape of leading edge air chamber | |
| CN205418070U (en) | Class triangle overall arrangement high altitude screw | |
| CN206125407U (en) | Miniature ducted fan aircraft | |
| CN205867488U (en) | Novel open air is let flight motion fly away and is equipped |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20110420 |