US3335985A - Inflated kite - Google Patents
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- US3335985A US3335985A US475931A US47593165A US3335985A US 3335985 A US3335985 A US 3335985A US 475931 A US475931 A US 475931A US 47593165 A US47593165 A US 47593165A US 3335985 A US3335985 A US 3335985A
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- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H27/00—Toy aircraft; Other flying toys
- A63H27/08—Kites
- A63H27/085—Inflatable kites
Definitions
- This invention relates to a kite and, more particularly, relates to an inflated kite capable of serving multiple purposes.
- the kite is capable of flight in even a mild breeze and may be attractively decorated for the pleasure of youngsters.
- a fea ture of the invention is that the kite is reversible in the sense that either face of the kite may be presented to the breeze.
- the two faces of the kite may be of two different colors so that, in elfect, the color of the kite may be changed simply by shifting the string connection from one face of the kite to the other face.
- the invention affords several advantages as a device for use in emergencies at sea.
- the kite may be made of thin flexible plastic so that the kite in deflated state may be rolled into an exceedingly compact light-weight package.
- the inflated kite may serve as a lifesaver to keep a person afloat.
- the kite may be both radar-reflective and light-reflective to facilitate a search at sea.
- an inflated kite is ineflicient if it comprises multiple inflated compartments because the connections between the compartments function as hinges to permit the compartments to swing relative to each other to aerodynamically unfavorable angles relative to each other.
- the buckling may permit the envelope to assume inadvententup an unfavorable configuration.
- the invention is based on the further discovery of the cause of buckling of a single envelope. It has been found that if the tethering string is connected to the single envelope at two widely spaced points, the envelope will tend to buckle in one direction midway between the two points and if the string is connected only to a central region of the envelope the envelope will tend to buckle in the opposite direction but in either case buckling may be prevented by making the envelope of ample cross section in the central region where buckling tends to occur. A further finding is that buckling tends to occur in a region where there is an abrupt change in the cross section of the single envelope and therefore there should be a smooth transitional at any change in the cross section of the envelope.
- the invention is based on the discovery that a single non-buckling envelope with two opposite side alcoves making the envelope of a generally T-shaped configuration is inherently aerodynamically eflicient and Patented Aug. 15, 1967
- An important feature of the invention is that the kite may be produced at surprisingly low cost by simply bonding together two substantially coextensive thermoplastic flexible sheets of the general configuration of a triangle, one leg of the triangle being the top edge of the kite.
- the two sheets are heat bonded together around the periphery of the triangle and in addition the two sheets are bonded together along inwardly bowed lines on each side of the triangle, each bowed line extending from the region of. the outer end of the corresponding arm of the envelope towards the region of the lower end of the envelope. Only the central region defined by the two inwardly bowed bond lines is inflated to form the single T-shaped envelope, the two inwardly bowed lines together with the outer edges of the two sheets defining the two stabilizing side flaps.
- the upper edge of the triangular configuration of the two sheets is convex so that the upper edge of the inflated envelope is of convex cross section longitudinally of the edge; when the kite is inflated this upper edge of the kite is also of convex cross section laterally of the edge.
- the outward bowing of the upper edge and the inward curvature of the two inwardly bowed bond lines result in a tapered kite configuration, each arm of the T-shaped configuration tapering in cross section towards its outer end and the longitudinal portion of the T-shaped configuration tapering towards the lower end of the envelope.
- the outline of the kite as viewed in front elevation is an isosceles triangle with a convex base uppermost and the outline of the inflated envelope 26 is a second isosceles triangle with a convex base uppermost and coinciding with the base of the first triangle.
- the second triangle differs from the first in that the two sides of the triangle are curved inwardly relatively to the sides of the first triangle.
- Each of the two side flaps 22 of the kite is defined by two corresponding sides of the first and second triangles.
- the resultant kite is inherently stable because it presents a dihedral to the wind.
- the dihedral is created in part by the tapering cross section of the two arms of the T-shaped configuration, in part by the inherent bulbous character of the inflated envelope, and in further part by the two stabilizing flaps as they flex rearward in response to wind pressure.
- FIG. 1 is a side elevation of the kite in flight
- FIG. 2 is a perspective view from above of the kite in especially so if both of the two lateral arms taper towards their outer ends.
- the upper end or edge of the envelope must be of smoothly curved cross section to avoid any tendency to buckle and the transition from the two arms of the configuration must be smooth and relatively gradual.
- kitse are provided with flaps or webs on its opposite sides with each flap stretching from the region of the outer end of the corresponding lateral arm of the envelope to the region of the lower end of the envelope.
- the resultant kite is so stable that it may be flown at the end of a string that is connected solely to the central region of the envelope where the axis of the two arms intersects the longitudinal axis of the envelope.
- FIG. 3 is a plan view of the inflated kite
- FIG. 4 is a transverse section along the line 4-4 of FIG. 2;
- FIG. 5 is a longitudinal section of the envelope taken as indicated by the line 55 of FIG. 2;
- FIG. 6 is a transverse cross section taken along the line 6-6 of FIG. 2.
- FIG. 3 shows how two sheets of thin thermoplastic material of identical configuration may be positioned face to face as the first step of the fabrication of the kite. It can be seen that the two sheets are of the general configuration of a of a triangle, one side of the triangle being the upper edge of the kite. This upper edge of the two sheets, which is designated 10 in FIG. 3, is preferably concave or bowed outward and the other two legs of the triangle are preferably straight legs forming two converging straight side edges 12 of the kite.
- the two sheets are of the general configuration of a of a triangle, one side of the triangle being the upper edge of the kite.
- This upper edge of the two sheets, which is designated 10 in FIG. 3 is preferably concave or bowed outward and the other two legs of the triangle are preferably straight legs forming two converging straight side edges 12 of the kite.
- the two sheets are of the general configuration of a of a triangle, one side of the triangle being the upper edge of the kite.
- configuration of the two plastic sheets also includes a tab extension 14 at the lower vertex of the triangle.
- the next step in the fabrication of the kite is to bond the two sheets together around the entire periphery of the two sheets except across the end of the tab extension 14.
- the two sheets may be heat bonded by applying heat and pressure along the desired bond lines.
- the resultant heat-bonded seam extends along the outwardly curved upper edge 10 and along the two straight side edges 12 and additionally along the two sides of the tab extension 14.
- the bonding operation may be carried out in a flat press, or may be carried out by means of cooperating rolls, or may be carried out by hand by simply moving a heated element under pressure along the desired line of bonding.
- the next step is to bond the two sheets together in the same manner along two lines 15 that are bowed inwardly from the opposite sides of the assembly, each of the two lines merging with the peripheral bond line at a point 16 at the upper end of the triangle and at a second point 18 near the lower vertex of the triangle.
- kite comprising a single envelope, generally designated 20, flanked by two flexible flaps, each designated by the numeral 22.
- the peripheral edges of the two sheets need not be bonded together between the two points 16 and 18 on each side of the kite, but such bonding is preferred for mutual reinforcement of the two sheets.
- the envelope 20 is of generally T-shaped configuration with opposite lateral arms 24 and a longitudinal stem 25.
- the two arms 24 taper in cross section towards the lower end of the envelope.
- the upper edge of the kite is blunt, but smoothly curved. It may be further seen in FIGS. 2 and 3 that the upper edge of the kite is also concave longitudinally of the edge.
- the transverse cross section of the kite in the region of the two alcoves or arms 24 is generally oval tapering in thickness in opposite directions from a central region of maximum thickness.
- the longitudinal section of the kite tapers in both directions from a region of maximum thickness that is substantially closer to the upper end of the kite than to the lower end.
- the kite has a bulbous nose which extends across the full width of the upper end of the kite, the upper end of the kite being convex as viewed both in front elevation and in side elevation.
- each face of the envelope carries a small patch of cloth 28 bonded thereto for the purpose of attaching a string to the kite.
- Each cloth patch 28 may carry a short length of string 30 which may be tied to a second string of any desired length. If desired a single string may be employed which branches to various points of connection with the envelope but preferably if multiple points of connection are employed the multiple points are all in the same region as the intersection of the two axes of the envelope.
- the envelope may be inflated by inserting a tube temporarily into the tab 14 and then blowing into the tube while the tab material is held snugly around the tube. After the envelope is inflated that tab 14 may be folded onto itself or twisted and then secured by an encircling rubber band.
- a suitable tail 32 may comprise four ribbons of the same plastic material
- each ribbon being approximately 4 to one inch in width and approximately ten to twelve feet in length.
- two lengths of ribbon twenty to twenty-four feet long are folded to make the four ribbons.
- the tail 32 may be conveniently attached to the envelope 20 by means of a pair of small interlinked plastic rings 34.
- the tab 14 When the kite is inflated the tab 14 is folded to form a loop in engagement with one of the two rings 34 and then a rubber band 35 is placed around the folded tab so that the rubber band not only seals the tab against escape of air but also serves as means for mechanically connecting one of the rings 34 to the tab.
- the two folded ribbons of the plastic material may then be doubled back through the other of the two interlinked rings 34 and secured thereto by a second rubber band 36. It is to be understood that While the tab 14 provides an inlet port for inflating the envelope, other provisions for inflation may be made in other embodiments of the invention.
- kite is manufactured as a toy or recreational device it may be attractively decorated in any suitable manner.
- two sheets of plastic material of two different colors are used, for example red and green, so that the two faces of the kite are of contrasting colors.
- the apparent color of the kite that is the color of the flying kite as viewed from the ground, may be changed by simply changing the string connection from one face of the kite to the other.
- a sheet material will be selected that is radar reflective, for example a sheet material having a metal coating.
- the sheet material selected for this purpose has a bright metal coating to be not only radar reflective but also light ieflective so that the kite may be conspicuous by reflected ig t.
- kite is aer-odynamically stable.
- a kite comprising:
- said envelope tapering from the region of the alcoves towards the lower end of the kite as the kite is viewed both in front elevation and in side elevation,
- the upper end of the kite being formed by a bulbous nose of the envelope extending across the full width of the kite
- each of said webs is defined in part by a curved line at the juncture of said envelope and one of its alcoves.
- a kite as set forth in claim 1 in which the taper of the envelope towards the lower end of the kite and the taper of the two alcoves are continuous, the degree of taper being sufficient to make the envelope rigid when inflated.
- each of the Webs being defined by a side of the first triangle and a corresponding inwardly curved side of the second triangle.
- kite as set forth in claim 6 in which the envelope is of maximum cross section in a region substantially closer to the upper end of the kite than to the lower end;
- a kite as set forth in claim 6 which in flight has a center of pressure on its longitudinal axis substantially closer to the upper end of the kite than to the lower end and in which the envelope is rigid to maintain its shape when the kite is flown with a single string connected to the envelope at said center of pressure.
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Description
Aug. 15, 1967 A. b, NEAL 3,335,935
I INFLATED KITE Filed July 30, 1965 agf arwe f United States Patent 3,335,985 INFLATED KITE Albert D. Neal, 5509 Ocean Front Walk, Playa del Rey, Calif. 90291 Filed July 30, 1965, Ser. No. 475,931 Claims. (Cl. 244-453) This invention relates to a kite and, more particularly, relates to an inflated kite capable of serving multiple purposes.
As a toy or a recreational device, the kite is capable of flight in even a mild breeze and may be attractively decorated for the pleasure of youngsters. In this respect a fea ture of the invention is that the kite is reversible in the sense that either face of the kite may be presented to the breeze. The two faces of the kite may be of two different colors so that, in elfect, the color of the kite may be changed simply by shifting the string connection from one face of the kite to the other face.
The invention affords several advantages as a device for use in emergencies at sea. One advantage is that the kite may be made of thin flexible plastic so that the kite in deflated state may be rolled into an exceedingly compact light-weight package. Another advantage is that if necessary, the inflated kite may serve as a lifesaver to keep a person afloat. Still another advantage of special importance is that the kite may be both radar-reflective and light-reflective to facilitate a search at sea.
It has been found by actual test that an inflated kite is ineflicient if it comprises multiple inflated compartments because the connections between the compartments function as hinges to permit the compartments to swing relative to each other to aerodynamically unfavorable angles relative to each other. In the same manner if a kite is made of a single envelope to buckle intentionally, the buckling may permit the envelope to assume inadvententup an unfavorable configuration.
The invention is based on the further discovery of the cause of buckling of a single envelope. It has been found that if the tethering string is connected to the single envelope at two widely spaced points, the envelope will tend to buckle in one direction midway between the two points and if the string is connected only to a central region of the envelope the envelope will tend to buckle in the opposite direction but in either case buckling may be prevented by making the envelope of ample cross section in the central region where buckling tends to occur. A further finding is that buckling tends to occur in a region where there is an abrupt change in the cross section of the single envelope and therefore there should be a smooth transitional at any change in the cross section of the envelope.
Finally the invention is based on the discovery that a single non-buckling envelope with two opposite side alcoves making the envelope of a generally T-shaped configuration is inherently aerodynamically eflicient and Patented Aug. 15, 1967 An important feature of the invention is that the kite may be produced at surprisingly low cost by simply bonding together two substantially coextensive thermoplastic flexible sheets of the general configuration of a triangle, one leg of the triangle being the top edge of the kite. The two sheets are heat bonded together around the periphery of the triangle and in addition the two sheets are bonded together along inwardly bowed lines on each side of the triangle, each bowed line extending from the region of. the outer end of the corresponding arm of the envelope towards the region of the lower end of the envelope. Only the central region defined by the two inwardly bowed bond lines is inflated to form the single T-shaped envelope, the two inwardly bowed lines together with the outer edges of the two sheets defining the two stabilizing side flaps.
In the preferred practice of the invention the upper edge of the triangular configuration of the two sheets is convex so that the upper edge of the inflated envelope is of convex cross section longitudinally of the edge; when the kite is inflated this upper edge of the kite is also of convex cross section laterally of the edge. The outward bowing of the upper edge and the inward curvature of the two inwardly bowed bond lines result in a tapered kite configuration, each arm of the T-shaped configuration tapering in cross section towards its outer end and the longitudinal portion of the T-shaped configuration tapering towards the lower end of the envelope.
It can be seen in FIG. 3 that the outline of the kite as viewed in front elevation is an isosceles triangle with a convex base uppermost and the outline of the inflated envelope 26 is a second isosceles triangle with a convex base uppermost and coinciding with the base of the first triangle. The second triangle differs from the first in that the two sides of the triangle are curved inwardly relatively to the sides of the first triangle. Each of the two side flaps 22 of the kite is defined by two corresponding sides of the first and second triangles.
The resultant kite is inherently stable because it presents a dihedral to the wind. The dihedral is created in part by the tapering cross section of the two arms of the T-shaped configuration, in part by the inherent bulbous character of the inflated envelope, and in further part by the two stabilizing flaps as they flex rearward in response to wind pressure.
The features and advantages of the invention may be understood from the following detailed description and the accompanying drawing.
In the drawing, which is to be regarded as merely illustrative:
FIG. 1 is a side elevation of the kite in flight;
FIG. 2 is a perspective view from above of the kite in especially so if both of the two lateral arms taper towards their outer ends. The upper end or edge of the envelope must be of smoothly curved cross section to avoid any tendency to buckle and the transition from the two arms of the configuration must be smooth and relatively gradual.
A further discovery is that stability is increased if the kite is provided with flaps or webs on its opposite sides with each flap stretching from the region of the outer end of the corresponding lateral arm of the envelope to the region of the lower end of the envelope. The resultant kite is so stable that it may be flown at the end of a string that is connected solely to the central region of the envelope where the axis of the two arms intersects the longitudinal axis of the envelope.
FIG. 3 is a plan view of the inflated kite;
FIG. 4 is a transverse section along the line 4-4 of FIG. 2;
FIG. 5 is a longitudinal section of the envelope taken as indicated by the line 55 of FIG. 2; and
FIG. 6 is a transverse cross section taken along the line 6-6 of FIG. 2.
The construction of the kite may best be understood by first describing the method of fabrication. FIG. 3 shows how two sheets of thin thermoplastic material of identical configuration may be positioned face to face as the first step of the fabrication of the kite. It can be seen that the two sheets are of the general configuration of a of a triangle, one side of the triangle being the upper edge of the kite. This upper edge of the two sheets, which is designated 10 in FIG. 3, is preferably concave or bowed outward and the other two legs of the triangle are preferably straight legs forming two converging straight side edges 12 of the kite. Preferably, but not necessarily, the
configuration of the two plastic sheets also includes a tab extension 14 at the lower vertex of the triangle.
The next step in the fabrication of the kite is to bond the two sheets together around the entire periphery of the two sheets except across the end of the tab extension 14. For this purpose the two sheets may be heat bonded by applying heat and pressure along the desired bond lines. It is to be noted that the resultant heat-bonded seam extends along the outwardly curved upper edge 10 and along the two straight side edges 12 and additionally along the two sides of the tab extension 14. The bonding operation may be carried out in a flat press, or may be carried out by means of cooperating rolls, or may be carried out by hand by simply moving a heated element under pressure along the desired line of bonding.
The next step is to bond the two sheets together in the same manner along two lines 15 that are bowed inwardly from the opposite sides of the assembly, each of the two lines merging with the peripheral bond line at a point 16 at the upper end of the triangle and at a second point 18 near the lower vertex of the triangle.
The result of the fabrication procedure is a kite comprising a single envelope, generally designated 20, flanked by two flexible flaps, each designated by the numeral 22. Obviously, the peripheral edges of the two sheets need not be bonded together between the two points 16 and 18 on each side of the kite, but such bonding is preferred for mutual reinforcement of the two sheets. It can be seen in FIG. 3 that the envelope 20 is of generally T-shaped configuration with opposite lateral arms 24 and a longitudinal stem 25. It also can be seen that the two arms 24 taper in cross section towards the lower end of the envelope. As may be seen in FIG. the upper edge of the kite is blunt, but smoothly curved. It may be further seen in FIGS. 2 and 3 that the upper edge of the kite is also concave longitudinally of the edge.
It can be seen in FIG. 1 that the transverse cross section of the kite in the region of the two alcoves or arms 24 is generally oval tapering in thickness in opposite directions from a central region of maximum thickness. It can be seen in FIG. 5 that the longitudinal section of the kite tapers in both directions from a region of maximum thickness that is substantially closer to the upper end of the kite than to the lower end. It can be further seen in FIGS. 3 and 5 that the kite has a bulbous nose which extends across the full width of the upper end of the kite, the upper end of the kite being convex as viewed both in front elevation and in side elevation.
It may be noted by comparing the various views that the point of maximum thickness of the single envelope is in the region of the intersection of the longitudinal axis of the envelope with the transverse axis of the two arms 24. In the drawing a single string 26 is connected to the en velope in this region. Since the kite flies in a stable manner on the end of a single string, it is obvious that the center of pressure of the kite in flight is at the string connection. In the preferred practice of the invention, each face of the envelope carries a small patch of cloth 28 bonded thereto for the purpose of attaching a string to the kite. Each cloth patch 28 may carry a short length of string 30 which may be tied to a second string of any desired length. If desired a single string may be employed which branches to various points of connection with the envelope but preferably if multiple points of connection are employed the multiple points are all in the same region as the intersection of the two axes of the envelope.
The envelope may be inflated by inserting a tube temporarily into the tab 14 and then blowing into the tube while the tab material is held snugly around the tube. After the envelope is inflated that tab 14 may be folded onto itself or twisted and then secured by an encircling rubber band.
The kite will fly without a tail but flies with greater efiiciency and to greater height with a tail. A suitable tail 32 may comprise four ribbons of the same plastic material,
each ribbon being approximately 4 to one inch in width and approximately ten to twelve feet in length. In the preferred practice of the invention two lengths of ribbon twenty to twenty-four feet long are folded to make the four ribbons.
The tail 32 may be conveniently attached to the envelope 20 by means of a pair of small interlinked plastic rings 34. When the kite is inflated the tab 14 is folded to form a loop in engagement with one of the two rings 34 and then a rubber band 35 is placed around the folded tab so that the rubber band not only seals the tab against escape of air but also serves as means for mechanically connecting one of the rings 34 to the tab. The two folded ribbons of the plastic material may then be doubled back through the other of the two interlinked rings 34 and secured thereto by a second rubber band 36. It is to be understood that While the tab 14 provides an inlet port for inflating the envelope, other provisions for inflation may be made in other embodiments of the invention.
It the kite is manufactured as a toy or recreational device it may be attractively decorated in any suitable manner. Preferably two sheets of plastic material of two different colors are used, for example red and green, so that the two faces of the kite are of contrasting colors. The apparent color of the kite, that is the color of the flying kite as viewed from the ground, may be changed by simply changing the string connection from one face of the kite to the other.
If the kite is designed for emergency use at sea, a sheet material will be selected that is radar reflective, for example a sheet material having a metal coating. Preferably the sheet material selected for this purpose has a bright metal coating to be not only radar reflective but also light ieflective so that the kite may be conspicuous by reflected ig t.
The fact that the kite is aer-odynamically stable is demonstrated :by the stable manner in which the kite flies with only a single connection to the kite string. The stability results from the dihedral configuration.
My description in specific detail of the selected embodiment of the invention will suggest various changes, substitutions and other departures from my disclosure within the spirit and scope of the appended claims.
I claim:
1. A kite comprising:
a single elongated inflated envelope of flexible sheet material having two opposite side alcoves at the upper end of the kite,
said two alcoves tapering towards the sides of the kite as the kite is viewed both in front elevation and in end elevation,
said envelope tapering from the region of the alcoves towards the lower end of the kite as the kite is viewed both in front elevation and in side elevation,
the cross-sectional configuration of the envelope transversely of the kite -in the region of the two alcoves being generally oval with maximum thickness centrally of the cross section,
the upper end of the kite being formed by a bulbous nose of the envelope extending across the full width of the kite,
said upper end of the kite being convex as the kite is viewed in front elevation; and
flexible webs on each side of the envelope for stabilizing eifect when the kite is in flight, each web extending from the corresponding alcove of the envelope downward to the lower end portion of the envelope.
2. A kite as set forth in claim 1 in which each of said webs is defined in part by a curved line at the juncture of said envelope and one of its alcoves.
3. A kite as set forth in claim 1 in which said flexible webs on the two sides of the kite are the sole stabilizing webs of the kite.
4. A kite as set forth in claim 1 in which said envelope is symmetrical both relative to a longitudinal plane in the maximum Width dimension of the envelope and in a longitudinal plane perpendicular to the first mentioned plane.
5. A kite as set forth in claim 1 in which the taper of the envelope towards the lower end of the kite and the taper of the two alcoves are continuous, the degree of taper being sufficient to make the envelope rigid when inflated.
'6. A kite of sheet material of the outline in front elevation of a first isosceles triangle with its base end uppermost, said kite having a single inflated envelope of the general configuration in front elevation of a second isosceles triangle with its base end uppermost, said second triangle having inwardly curved opposite sides; and
two stabilizing webs on opposite sides of the kite, each of the Webs being defined by a side of the first triangle and a corresponding inwardly curved side of the second triangle.
7. A kite as set forth in claim 6 in which the uppermost bases of the two triangles coincide.
8. A kite as set forth in claim 7 in which the uppermost bases of the triangles are convex.
9. A kite as set forth in claim 6 in which the envelope is of maximum cross section in a region substantially closer to the upper end of the kite than to the lower end;
and in which the envelope tapers from said region in both longitudinal directions and both lateral directions.
10. A kite as set forth in claim 6 which in flight has a center of pressure on its longitudinal axis substantially closer to the upper end of the kite than to the lower end and in which the envelope is rigid to maintain its shape when the kite is flown with a single string connected to the envelope at said center of pressure.
References Cited UNITED STATES PATENTS 770,626 9/1904 Bell 244-153 2,486,158 10/ 1949 Haas 244-33 2,593,979 4/1952 Calhoun 244-154 3,086,737 4/1963 Hyman 244-153 3,093,354 6/1963 Pohl 244154 MILTON BUCHLER, Primary Examiner. P. E. SAUBERER, Assistant Examiner.
Claims (1)
1. A KITE COMPRISING: A SINGLE ELONGATED INFLATED ENVELOPE OF FLEXIBLE SHEET MATERIAL HAVING TWO OPPOSITE SIDE ALCOVERS AT THE UPPER END OF THE KITE, SAID TWO ALCOVES TAPERING TOWARDS THE SIDES OF THE KITE AS THE KITE IS VIEWED BOTH IN FRONT ELEVATION AND IN END ELEVATION, SAID ENVELOPE TAPERING FROM THE REGION OF THE ALCOVES TOWARDS THE LOWER END OF THE KITE AS THE KITE IS VIEWED BOTH IN FRONT ELEVATION AND IN SIDE ELEVATION, THE CROSS-SECTIONAL CONFIGURATION OF THE ENVELOPE TRANSVERSELY OF THE KITE IN THE REGION OF THE TWO ALCOVES BEING GENERALLY OVAL WITH MAXIMUM THICKNESS CENTRALLY OF THE CROSS SECTION,
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US475931A US3335985A (en) | 1965-07-30 | 1965-07-30 | Inflated kite |
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US475931A US3335985A (en) | 1965-07-30 | 1965-07-30 | Inflated kite |
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US3335985A true US3335985A (en) | 1967-08-15 |
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US475931A Expired - Lifetime US3335985A (en) | 1965-07-30 | 1965-07-30 | Inflated kite |
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Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
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US3480238A (en) * | 1967-02-27 | 1969-11-25 | Barish Ass Inc | Glide wing |
US3952975A (en) * | 1973-04-04 | 1976-04-27 | Vonco Products, Inc. | Inflatable kite |
US3980260A (en) * | 1973-04-04 | 1976-09-14 | Vonco Products, Inc. | Inflatable kite |
US4029273A (en) * | 1974-09-19 | 1977-06-14 | Christoffel Jr Julius M | Kite |
US4461438A (en) * | 1982-03-01 | 1984-07-24 | Team Winsor | Apparatus for controlling and storing a kite |
US5183224A (en) * | 1990-05-14 | 1993-02-02 | Harburg Rudy W | Self regulating pinwheel kite tail |
US5678784A (en) * | 1990-03-13 | 1997-10-21 | Vanguard Research, Inc. | Space vehicle and method |
US5762293A (en) * | 1997-05-14 | 1998-06-09 | Crosbie; Scott C. | Inflatable kite |
US6016998A (en) * | 1993-07-28 | 2000-01-25 | Allsopp; Gerald Alexander Richard | Kite stability and weight |
WO2005070758A1 (en) | 2004-01-26 | 2005-08-04 | Sjoeblom Hans | Location signalling device |
US20060157622A1 (en) * | 2005-01-19 | 2006-07-20 | David Johnston | Multi-purpose inflatable kite |
US20070161322A1 (en) * | 2006-01-10 | 2007-07-12 | Carmon Arie D | Multi-segment animation balloon |
US20100065676A1 (en) * | 2008-09-17 | 2010-03-18 | Kun Yuan Tong | Balloon kite |
CN104941202A (en) * | 2015-06-01 | 2015-09-30 | 励奇峰 | Single line dynamic kite |
US10807013B2 (en) * | 2017-12-20 | 2020-10-20 | Francis A. Alonso | Modified delta wing kite with inflatable fuselage |
US20210252418A1 (en) * | 2020-02-14 | 2021-08-19 | Thomas R. Pierce | Self-supporting inflatable kite system and method of use |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
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US770626A (en) * | 1904-09-20 | Aerial vehicle or other structure | ||
US2486158A (en) * | 1948-05-05 | 1949-10-25 | Haas Milford | Pneumatic kite |
US2593979A (en) * | 1952-01-11 | 1952-04-22 | Skycraft Mfg Corp | Tethered toy airplane |
US3086737A (en) * | 1961-04-24 | 1963-04-23 | Hyman Theodore | Inflatable kites |
US3093354A (en) * | 1961-10-10 | 1963-06-11 | Gen Mills Inc | Inflatable kite |
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1965
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US770626A (en) * | 1904-09-20 | Aerial vehicle or other structure | ||
US2486158A (en) * | 1948-05-05 | 1949-10-25 | Haas Milford | Pneumatic kite |
US2593979A (en) * | 1952-01-11 | 1952-04-22 | Skycraft Mfg Corp | Tethered toy airplane |
US3086737A (en) * | 1961-04-24 | 1963-04-23 | Hyman Theodore | Inflatable kites |
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Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3480238A (en) * | 1967-02-27 | 1969-11-25 | Barish Ass Inc | Glide wing |
US3952975A (en) * | 1973-04-04 | 1976-04-27 | Vonco Products, Inc. | Inflatable kite |
US3980260A (en) * | 1973-04-04 | 1976-09-14 | Vonco Products, Inc. | Inflatable kite |
US4029273A (en) * | 1974-09-19 | 1977-06-14 | Christoffel Jr Julius M | Kite |
US4461438A (en) * | 1982-03-01 | 1984-07-24 | Team Winsor | Apparatus for controlling and storing a kite |
US5678784A (en) * | 1990-03-13 | 1997-10-21 | Vanguard Research, Inc. | Space vehicle and method |
US5183224A (en) * | 1990-05-14 | 1993-02-02 | Harburg Rudy W | Self regulating pinwheel kite tail |
US6016998A (en) * | 1993-07-28 | 2000-01-25 | Allsopp; Gerald Alexander Richard | Kite stability and weight |
US5762293A (en) * | 1997-05-14 | 1998-06-09 | Crosbie; Scott C. | Inflatable kite |
US8534217B2 (en) | 2004-01-26 | 2013-09-17 | Hans Sjoblom | Location signaling device |
US20070284476A1 (en) * | 2004-01-26 | 2007-12-13 | Hans Sjoblom | Location Signaling Device |
US8356569B2 (en) | 2004-01-26 | 2013-01-22 | Hans Sjoblom | Location signaling device |
WO2005070758A1 (en) | 2004-01-26 | 2005-08-04 | Sjoeblom Hans | Location signalling device |
US20060157622A1 (en) * | 2005-01-19 | 2006-07-20 | David Johnston | Multi-purpose inflatable kite |
US20070161322A1 (en) * | 2006-01-10 | 2007-07-12 | Carmon Arie D | Multi-segment animation balloon |
US20100065676A1 (en) * | 2008-09-17 | 2010-03-18 | Kun Yuan Tong | Balloon kite |
CN104941202A (en) * | 2015-06-01 | 2015-09-30 | 励奇峰 | Single line dynamic kite |
CN104941202B (en) * | 2015-06-01 | 2018-07-13 | 励奇峰 | A kind of single line dynamic kite |
US10807013B2 (en) * | 2017-12-20 | 2020-10-20 | Francis A. Alonso | Modified delta wing kite with inflatable fuselage |
US20210252418A1 (en) * | 2020-02-14 | 2021-08-19 | Thomas R. Pierce | Self-supporting inflatable kite system and method of use |
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