CN204275498U - A kind of software kite - Google Patents
A kind of software kite Download PDFInfo
- Publication number
- CN204275498U CN204275498U CN201420785644.1U CN201420785644U CN204275498U CN 204275498 U CN204275498 U CN 204275498U CN 201420785644 U CN201420785644 U CN 201420785644U CN 204275498 U CN204275498 U CN 204275498U
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- kite
- software
- ventilating duct
- air
- fin
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Abstract
The utility model discloses a kind of software kite, comprise main body, main body comprises front and the back side, and the back side is provided with at least three ventilating ducts be arranged side by side, and be provided with ventilation slot between two adjacent ventilating ducts, every bar ventilating duct comprises an air inlet and air outlet.The utility model adopts technique scheme, when there is skewness after kite flying, can overcome kite skewness by control and regulation rope; The setting in balance cabin can make flight of kites more stable; The spacing of the fin on two adjacent ventilating ducts is H, and the length of payment to a porter is 1.5H, can reduce the quantity of payment to a porter like this, makes lift larger, can be applicable to three grades and let fly away with apparatus for lower wind; When the setting of air bag makes kite flying, for improving the lift of kite, when regaining kite, kite is slowly declined, the convenient setting point controlling kite simultaneously; The setting in two lateral balance cabins can make flight of kites more stable.
Description
Technical field
The utility model relates to a kind of kite, relates to a kind of software kite specifically.
Background technology
Since the wooden kite of black Zhai Faming, the material of kite and manufacture craft experienced by Improvement and perfection repeatedly.Due to wooden kite heavier-weight, in order to alleviate the weight of kite, people change the material of kite into bamboo by timber.From Tang of Sui, due to the prosperity of paper-making industry, beginning paper using among the people papers kite, and then further mitigates kite weight, improves the manufacture craft of kite.Experience constantly perfect in several thousand, although the weight saving of kite, the manufacture craft of kite improves, due to the existence of skeleton, and the shortcomings such as weight is still light not, and still there is complex manufacturing technology, not portable.
At present, market there is the software kite of lighter in weight, the appearance of software kite, considerably improved the manufacture craft of kite, but, by the restriction of its structure, software kite is when letting fly away, and stability is bad, and suffered buoyancy is less, so the volume of software kite is mostly less, can not the ornament such as suspended weights is comparatively large, length is longer silk ribbon at the afterbody of kite, so the length of software kite is mostly shorter.
Number of patent application be 201020263461.5 utility model patent disclose a kind of no-skeleton kite, not only alleviate the weight of kite, improve the stability of kite, improve the buoyancy of kite to a certain extent simultaneously.But above-mentioned software kite stability can't reach requirement, after repeatedly letting fly away, the shape in air channel there will be distortion due to traction action all simultaneously, there will be skewness, be inconvenient to regulate after deflection after kite flying.In addition, let fly away when the kite of said structure is applicable to more than 3 grades wind-force, let difficulty fly away with during apparatus for lower wind for 3 grades, be difficult to meet people and let requirement fly away under different occasion.
Summary of the invention
It is better that the technical problems to be solved in the utility model is to provide a kind of stability, occurs skewness
Rear convenient adjustment, lift is larger, can be applicable to three grades of software kites let fly away with apparatus for lower wind.
For solving the problem, the utility model is by the following technical solutions: a kind of software kite, comprise main body, main body comprises front and the back side, the back side is provided with at least three ventilating ducts be arranged side by side, be provided with ventilation slot between two adjacent ventilating ducts, every bar ventilating duct comprises an air inlet and air outlet.
Below further improvement of the utility model:
The front of main body is provided with two air bags, and air bag is arranged on the position near air opening end, and position corresponding with each air bag in main body offers the air holes be communicated with air bag.
Further improvement:
Air inlet on ventilating duct outside being positioned in ventilating duct or air outlet are provided with quantity-adjustable size
Adjusting device.
Further improvement:
Air inlet on ventilating duct outside being positioned in ventilating duct and air outlet are all provided with quantity-adjustable size
Adjusting device.
Further improvement:
Described adjusting device is two adjusting ropes, and the degree fastened by controlling two adjusting ropes controls the size of intake or air output.
Further improvement:
On the ventilating duct in outside, be respectively equipped with a balance cabin in some ventilating ducts, balance cabin is arranged on the position near air inlet, and described balance cabin is communicated with ventilating duct.
Further improvement:
Every bar ventilating duct is provided with fin, every bar fin is connected with a payment to a porter.
Further improvement:
The quantity of described fin is 1, and fin is arranged along the length direction of every bar ventilating duct, and the fin one_to_one corresponding on each bar ventilating duct is arranged
Further improvement:
Vertical range between fin on two adjacent ventilating ducts is H, and the length being connected to the payment to a porter on fin is 1.5H.
Further improvement:
The cross-sectional area of described air inlet is greater than the cross-sectional area of air outlet, and the cross section of described air inlet is pentagon, and the cross section of described air outlet is triangle.
The utility model adopts technique scheme, when there is skewness after kite flying, can overcome kite skewness by control and regulation rope; The setting in balance cabin can make flight of kites more stable; The spacing of the fin on two adjacent ventilating ducts is H, and the length of payment to a porter is 1.5H, can reduce the quantity of payment to a porter like this, makes lift larger, can be applicable to three grades and let fly away with apparatus for lower wind; When the setting of air bag makes kite flying, for improving the lift of kite, when regaining kite, kite is slowly declined, the convenient setting point controlling kite simultaneously; The setting in two lateral balance cabins can make flight of kites more stable.
Below in conjunction with accompanying drawing, the technical solution of the utility model is described further.
Accompanying drawing explanation
Accompanying drawing 1 is the structural representation of the utility model embodiment;
Accompanying drawing 2 is the left view of accompanying drawing 1;
Accompanying drawing 3 is A-A sectional view in accompanying drawing 2;
Accompanying drawing 4 is the upward view of accompanying drawing 1.
In figure: 1-main body; 2-ventilating duct; 3-ventilation slot; 4-fin; 5-payment to a porter; 6-adjusting rope; 7-balances cabin; 8-through hole; 9-air bag; 10-air holes; 101-front; The 102-back side; 201-air inlet; 202-air outlet.
Detailed description of the invention
Embodiment, as shown in Figure 1, Figure 2, Figure 3 shows, a kind of software kite, comprise main body 1, main body 1 is single or multiple lift cloth, and main body 1 comprises front 101 and the back side 102, and the back side 102 of described main body 1 is provided with the ventilating duct 2 that at least 3 employing clothes be arranged side by side surround, be arranged in parallel between each bar ventilating duct 2, between two adjacent ventilating ducts 2, be provided with ventilation slot 3.
Ventilating duct 2 comprises air inlet 201 and air outlet 202, and gas passes into air outlet 202 by air inlet 201 and discharges.
The cross-sectional area of described air inlet 201 is greater than the cross-sectional area of air outlet 202, described air inlet 201
Cross section be pentagon, the cross section of described air outlet 202 is triangle.
The air inlet 201 being positioned at the ventilating duct 2 of both sides in many ventilating ducts 2 is provided with adjusting air inlet mouth 201
The adjusting device of intake size.
Improve as one, described adjusting device is arranged on the air outlet 202 of the ventilating duct 2 being positioned at both sides in many ventilating ducts 2, for adjusting air port 202 air output size.
Improve as one, the air outlet 202 being positioned at the ventilating duct 2 of both sides in many ventilating ducts 2 and air inlet 201 are all provided with adjusting device.
Described adjusting device is two adjusting ropes 6, the degree fastened by controlling two adjusting ropes 6 controls the size of intake or air output, when two adjusting ropes 6 are fastened, and the sidewall of adjusting rope 6 tractive air outlet 202 or air inlet 201, make sidewall close to each other, and then reduce air intake or air output.
As described in Figure 4, when kite deflection to the right after letting fly away, fasten the adjusting rope 6 at air outlet 202 place, left side, air outlet 202 is diminished or the adjusting rope 6 at air inlet 201 place makes air inlet 201 diminish on the right side of fastening, the problem of deflection on the right side of kite can be solved; When kite deflection to the left after letting fly away, fasten right side air outlet 202 place adjusting rope 6, make right side air outlet 202 diminish or fastens left side air inlet 201 place adjusting rope 6 make on the left of air inlet 201 diminish, the problem of deflection on the left of kite can be solved.
On the ventilating duct 2 in outside, a balance cabin 7 is respectively equipped with in many ventilating ducts 2, balance cabin 7 is arranged on the position near air inlet 201, described balance cabin 7 is communicated with by through hole 8 with air channel 2 all, when letting fly away, gas is entered in balance cabin 7 by air channel 2 via through holes 8 all, and the setting in two lateral balance cabins 7 can make flight of kites more stable.
Every bar ventilating duct 2 is provided with two or more fin 4, and fin 4 is arranged along the length direction of every bar ventilating duct 2, and the fin 4 on each bar ventilating duct 2 is arranged with one_to_one corresponding, every bar fin 4 is connected with a payment to a porter 5.
Improve as one, every bar ventilating duct 2 is provided with a fin 4, fin 4 is arranged along the length direction of every bar ventilating duct 2, fin 4 one_to_one corresponding on each bar ventilating duct 2 is arranged, and every bar fin 4 is connected with a payment to a porter 5, the vertical range between the fin 4 on two adjacent ventilating ducts 2 is H, the length of payment to a porter 5 is 1.5H, the quantity of payment to a porter can be reduced like this, make lift larger, three grades can be applicable to and let fly away with apparatus for lower wind.
The front 101 of described main body 1 is provided with two air bags 9, air bag 9 is arranged on air outlet 202 end near ventilating duct 2, position corresponding with each air bag 9 in main body 1 offers the air holes 10 be communicated with air bag 9, gas can enter into air bag 9 by air holes 10, the setting of air bag 9 makes the lift improving kite during kite flying, when regaining kite, kite is slowly declined, the convenient setting point controlling kite simultaneously.
Claims (10)
1. a software kite, comprise main body (1), main body (1) comprises front (101) and the back side (102), the back side (102) is provided with at least three ventilating ducts be arranged side by side (2), be provided with ventilation slot (3) between two adjacent ventilating ducts (2), every bar ventilating duct (2) comprises an air inlet (201) and air outlet (202).
2. a kind of software kite according to claim 1, it is characterized in that: the front (101) of main body (1) is provided with two air bags (9), air bag (9) is arranged on the position of holding near air outlet (202), and the upper position corresponding with each air bag (9) of main body (1) offers the air holes (10) be communicated with air bag (9).
3. a kind of software kite according to claim 1, is characterized in that: ventilating duct (2)
In be positioned at air inlet (201) on the ventilating duct (2) in outside or air outlet (202) is provided with the adjusting device of quantity-adjustable size.
4. a kind of software kite according to claim 1, is characterized in that: ventilating duct (2)
In be positioned on air inlet (201) on the ventilating duct (2) in outside and air outlet (202) and be all provided with the adjusting device of quantity-adjustable size.
5. a kind of software kite according to claim 3 or 4, is characterized in that: described adjusting device is two adjusting ropes (6), and the degree fastened by controlling two adjusting ropes (6) controls the size of intake or air output.
6. a kind of software kite according to claim 1, it is characterized in that: in some ventilating ducts (2), on the ventilating duct (2) in outside, be respectively equipped with balance cabin (7), balance cabin (7) is arranged on the position near air inlet (201), and described balance cabin (7) is communicated with ventilating duct (2).
7. a kind of software kite according to claim 1, is characterized in that: every bar ventilating duct (2) is provided with fin (4), every bar fin (4) is connected with a payment to a porter (5).
8. a kind of software kite according to claim 7, is characterized in that: the quantity of described fin (4) is 1, and fin (4) is arranged along the length direction of every bar ventilating duct (2), and fin (4) one_to_one corresponding on each bar ventilating duct (2) is arranged.
9. a kind of software kite according to claim 8, is characterized in that: between the fin (4) on two adjacent ventilating ducts (2), vertical range is H, and the length being connected to the payment to a porter (5) on fin (4) is 1.5H.
10. a kind of software kite according to claim 1, it is characterized in that: the cross-sectional area of described air inlet (201) is greater than the cross-sectional area of air outlet (202), the cross section of described air inlet (201) is pentagon, and the cross section of described air outlet (202) is triangle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420785644.1U CN204275498U (en) | 2014-12-15 | 2014-12-15 | A kind of software kite |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420785644.1U CN204275498U (en) | 2014-12-15 | 2014-12-15 | A kind of software kite |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204275498U true CN204275498U (en) | 2015-04-22 |
Family
ID=52858699
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420785644.1U Expired - Fee Related CN204275498U (en) | 2014-12-15 | 2014-12-15 | A kind of software kite |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204275498U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111717364A (en) * | 2020-07-01 | 2020-09-29 | 郝刚 | Soft aircraft and control method thereof |
| CN111806669A (en) * | 2020-07-20 | 2020-10-23 | 邓迪 | Captive balloon system suitable for small ship carries on |
-
2014
- 2014-12-15 CN CN201420785644.1U patent/CN204275498U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111717364A (en) * | 2020-07-01 | 2020-09-29 | 郝刚 | Soft aircraft and control method thereof |
| CN111806669A (en) * | 2020-07-20 | 2020-10-23 | 邓迪 | Captive balloon system suitable for small ship carries on |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150422 Termination date: 20181215 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |