EP0184777B1 - Avion jouet - Google Patents
Avion jouet Download PDFInfo
- Publication number
- EP0184777B1 EP0184777B1 EP85115477A EP85115477A EP0184777B1 EP 0184777 B1 EP0184777 B1 EP 0184777B1 EP 85115477 A EP85115477 A EP 85115477A EP 85115477 A EP85115477 A EP 85115477A EP 0184777 B1 EP0184777 B1 EP 0184777B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- frame
- flying device
- flying
- base
- elements
- 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.)
- Expired - Lifetime
Links
Images
Classifications
-
- 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
Definitions
- the invention relates to a kite-like toy flying device with a covering on a scaffold, which has a frame with side profiles running on both sides of an axis of symmetry, joined at one end to a point and at the other end by a base rod at a distance from one another.
- GB-A-6 598 (1909) describes a toy flying machine consisting of a triangular frame with transverse and longitudinal struts, which is partially covered and contains wing-like structures which run parallel to the covering and are firmly connected to this or the frame.
- This toy aircraft is equipped as a plane with a propeller that is connected to a rubber cord drive.
- Aircraft without a mechanical drive consist, for example, of a cross-shaped scaffold with a covering attached to it, the outer contours of which connect the ends of the scaffold.
- spatial flight boxes are known which, for example according to DE-U-77 34 838, are composed of several individual parts of the same shape.
- the side profiles are curved outwards from the tip to the base rod and the frame has coupling elements for connection to other parts of the frame, the coupling elements being a grid of the corner points of an equilateral triangle on the one hand and one on the other On the other hand, determine the point at which the side profiles are joined, opposite the baseline of the subsequent rectangles.
- the length of the sides of the rectangle starting from the base line corresponds to half the length of the base line or a multiple thereof.
- these requirements offer a single flight surface of favorable shape, which, on the other hand, can be assembled into a wide variety of shapes thanks to the grid described.
- the isosceles triangle allows the formation of a circle with six axes of symmetry. Each axis of symmetry passes through a tip of the isosceles triangle and is bisector of the opposite side, to which a rectangle of the type described can be connected.
- the frame should preferably run within the grid points determined by the coupling elements, which in turn are offered by cantilevered tabs or the like connecting elements.
- tabs or tubular cantilever elements each have at least one receiving opening for a pin or the like, so that several tabs can be connected with their mutually coaxially assigned receiving openings by a single pin.
- the pin is preferably designed as a spring sleeve, which receives an explosive pin in its axial bore; the explosive pin firmly pressed into the spring sleeve, the tabs penetrated by it are connected to one another in a force-locking manner.
- the scale made of cord for fastening a guide cord which is common in aircraft of the type mentioned at the outset, can - according to a further feature of the invention - be fastened to the spring sleeve or the detonating pin, which simplifies the adjustment of the control.
- the tabs which are preferably detachably connected to the frame.
- the tab is provided by a partial longitudinal slot with two integrally formed legs, which - adjacent to each other - are guided through the opening mentioned in the frame and the edges of which rest resiliently. Thanks to two spaced-apart locking lugs or the like on each of the two outer sides, the tongue is prevented from moving in its longitudinal direction.
- the aircraft according to the invention can be connected in a variety of configurations to other aircraft of the same design and in a particularly simple manner by means of the coupling elements described.
- Flight surfaces can be produced by arranging several of the described aircraft next to one another. However, individual aircraft or flight surfaces can also be joined together to form missiles by struts or the like.
- the use of the aircraft according to the invention is very diverse; The protection extends to a single aircraft as well as to the flight surfaces and missiles that can be manufactured with it.
- this tab is designed as a disk with at least two bores - preferably four bores.
- the disk is penetrated at a right angle by an approximately uniform other disk and forms a cross-shaped cross-section with it.
- the first disc of two is approximately uniform penetrated at right angles to other panes, with two panes each creating a cross-shaped cross section.
- a frame 10 for the production of the wing 11 of a toy aircraft consists of two side profiles 14, each starting from one end of a base rod 12 of length a of, for example, 300 mm and curved to a tip 13, and a cross rod 15 running parallel to the base rod 12.
- Tabs - namely a tip tab 18 and two end tabs 19 - protrude from the tip 13 as well as from the nodes of the base rod 12 with the side profiles 14, with plug-in holes 20, 21.
- the latter together with plug holes 22 from lateral expansion tabs 23 of the side profiles 14, determine a construction grid from radial lines R starting from a center point M and enclosing an angle w of 60 °, on which - at a distance 320 mm measuring - from the center point M or from the plug hole 20 the plug holes 22 lie on a construction circle K, with the radius r, (320 mm).
- These plug holes 21 also lie on a construction circle K 2 of radius r 2 around the center M and at a distance f of 120 mm from one another.
- the spreading tabs 23 each consist - as is particularly illustrated in FIG. 7 - of a plastic sheet of small thickness with a partial longitudinal slot 25 separating two sheet legs 24, which ends in a round hole 25 a .
- the thus limited elastic leaf legs 24 are brought together for fixing to the side profile 14 so that their laterally projecting end lugs 26 can be guided through a slot 28 of the side profile 14 (FIG. 4) until they engage behind the inner surface 29, an inner rib 29 of the side profile 14 .
- the frame 10 is provided as a scaffold for the wing 11 on both sides with a covering 31, which consists, for example, of foil sections welded to the sides to form a kind of pointed bag, the edge 32 of which is folded onto the surface 33 of the wing 11 and is releasably connected to this by adhesive tape 34.
- a covering 31 which consists, for example, of foil sections welded to the sides to form a kind of pointed bag, the edge 32 of which is folded onto the surface 33 of the wing 11 and is releasably connected to this by adhesive tape 34.
- a square extension frame 36 composed of four frame bars 37 or an equilateral triangular frame 38 can be connected to the end straps 19 by means of corner straps 39; whose plug holes 40 are at a distance f from one another, and a coupling pin can protrude at both ends into - not recognizable - bores in frame 10 and triangular or square frame 38 or 36 and additionally stabilize them.
- FIG. 7 also illustrates an explosive pin 44 a with an axial hole 61 through which one of the holding cords 60 for the aircraft 30 is guided.
- Stabilizing straps 45 are fixed to the respective rear tips 45 in the plane of the wing 11, for example in FIG. 13 by means of a coupling blade 55 which is shown in the enlarged longitudinal section in the left half of the figure and is similar to a blade-like plan. This is connected to a spring sleeve 42 of the type shown in FIG. 7, which extends through a plug-in hole 56 of a molded coupling tab, with a tip tab 18 in the manner described. A pair of slots 58 runs in the clutch plate 55, around the separating web 59 of which the stabilizing band 45 is placed holding.
- FIG. 10 The coupling of eight aircraft 30 to the device 30 c and their additional stiffening by additional struts 46 with unillustrated plug holes is shown in FIG. 10.
- the devices 30 d to 30 f are composed of several aircraft 30 over a large area, with FIGS. 11 to 13 curved additional struts 47 show.
- the aircraft 30 of the exemplary embodiments 50 a to 50 e lie one above the other, possibly with the interposition of spacer struts 51, which can be seen in principle in FIG. 21 and fixed on the tabs 18, 23. In this way, double, triple or multiple decks can be easily manufactured.
- four aircraft 30 a are arranged spatially to one another as a box and fixed with their tabs 18, 19, 23 in a spatial rod cage 52.
- T-pieces 70 made of plastic pipes can be used according to FIG. 24, which plug pins 71 of the frame parts - or their ends themselves - receive. At least one of those plastic pipes 72 is provided with a plug hole 21.
- the aircraft described are guided obliquely into the wind on a long cord 62 (FIG. 21) and are thereby buoyed.
- This cord 62 is optionally slidably connected to the holding cord 60, which - fixed at both ends - forms a so-called balance; thanks to this scale, the gliding angle of the aircraft can be adjusted.
- the plug pin 42 is inserted into an opening 21 n , which are provided in parallel collar corners 80 of a frame corner 81, which run on both sides of a pocket slot 82.
- a disk 93 is inserted with a bore 84; this is aligned with the openings 21 n and is penetrated by the pin 42.
- the disk 83 is provided with four bores 84 and can thus connect four frame corners 81 to one another (not shown).
- stop walls 85 can run between the bores 84.
- the disk 83 a of FIG. 27 is actually a disk cross made of two disks 83 of the type described which penetrate one another at right angles.
Landscapes
- Toys (AREA)
- Micromachines (AREA)
Claims (11)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT85115477T ATE57311T1 (de) | 1984-12-08 | 1985-12-05 | Spielzeugfluggeraet. |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3444818A DE3444818C1 (de) | 1984-12-08 | 1984-12-08 | Spielzeugfluggeraet |
DE3444818 | 1984-12-08 |
Publications (3)
Publication Number | Publication Date |
---|---|
EP0184777A2 EP0184777A2 (fr) | 1986-06-18 |
EP0184777A3 EP0184777A3 (en) | 1987-10-07 |
EP0184777B1 true EP0184777B1 (fr) | 1990-10-10 |
Family
ID=6252237
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP85115477A Expired - Lifetime EP0184777B1 (fr) | 1984-12-08 | 1985-12-05 | Avion jouet |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP0184777B1 (fr) |
AT (1) | ATE57311T1 (fr) |
DE (1) | DE3444818C1 (fr) |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB190906598A (en) * | 1909-03-19 | 1910-01-20 | Charles Ebenezer Richardson | Improvements in Toy Aerial Machines. |
US1092303A (en) * | 1913-11-17 | 1914-04-07 | John Stippick | Kite. |
DE1928425U (de) * | 1965-09-24 | 1965-12-02 | Schmohl Geb | Faltbarer drachen. |
FR1594767A (fr) * | 1968-10-30 | 1970-06-08 | ||
DE7029834U (de) * | 1970-08-07 | 1970-10-15 | Guenther Spielwaren | Drachen, insbesondere spielzeugdrachen. |
US3937426A (en) * | 1973-11-09 | 1976-02-10 | Synestructics, Inc. | Tetrahedral kite structure |
DE7606694U1 (de) * | 1976-03-05 | 1976-09-02 | Neckermann, Michael, 8702 Lengfeld | Zerlegbarer drachen |
-
1984
- 1984-12-08 DE DE3444818A patent/DE3444818C1/de not_active Expired
-
1985
- 1985-12-05 EP EP85115477A patent/EP0184777B1/fr not_active Expired - Lifetime
- 1985-12-05 AT AT85115477T patent/ATE57311T1/de not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
DE3444818C1 (de) | 1986-05-22 |
ATE57311T1 (de) | 1990-10-15 |
EP0184777A3 (en) | 1987-10-07 |
EP0184777A2 (fr) | 1986-06-18 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE60102851T2 (de) | Paneelanordnung und Verbindungsmittel | |
DE2150236B2 (de) | Einrichtung zum Verbinden eines Skelettpfostens und -querträgers aus Kastenprofilen | |
DE60202889T2 (de) | Ein spielzeugbaukasten | |
EP0274085B1 (fr) | Pince-papier en matière plastique | |
CH615629A5 (fr) | ||
DE2701905B2 (de) | Stranggepreßtes Bauelement zum Aufbau von Wänden, insbesondere von Kraftfahrzeugen | |
DE69821310T2 (de) | Spielzeugkonstruktionsset | |
EP0184777B1 (fr) | Avion jouet | |
DE2400177C3 (de) | Vorrichtung zum lösbaren Zusammenhalten eines Skistockpaares | |
DE2208509B2 (de) | Verbindungsglied | |
DE2924874A1 (de) | Flugzeugmodell | |
EP0143299A2 (fr) | Elément de protection de coins ou de bords | |
DE3125111C2 (de) | Gelenkkette für Stetigförderer | |
DE8534112U1 (de) | Spielzeugfluggerät | |
DE8531225U1 (de) | Tragnetz | |
DE3802738C2 (de) | Bauspielzeug | |
DE3142934C2 (de) | Stabelement für Bausysteme | |
DE2345162A1 (de) | Kreuzstueck fuer das stabkreuz eines faltdrachens | |
DE19502721C2 (de) | Räumleiter | |
DE2065276C3 (de) | Längsstrahlende Antenne mit einem Längsträger und darauf angeordneten Antenne nelementen | |
DE3519823A1 (de) | Stapelpalette mit eckpfosten | |
AT389926B (de) | Gleitkette | |
DE2941184A1 (de) | In einer stuetze angeordnete halterung zum stirnseitigen anschliessen von balken | |
DE2310081A1 (de) | Kontaktfederleiste | |
DE2710392A1 (de) | Traeger fuer spielmodelle |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
AK | Designated contracting states |
Kind code of ref document: A2 Designated state(s): AT CH FR GB IT LI |
|
PUAL | Search report despatched |
Free format text: ORIGINAL CODE: 0009013 |
|
RHK1 | Main classification (correction) |
Ipc: A63H 27/08 |
|
AK | Designated contracting states |
Kind code of ref document: A3 Designated state(s): AT CH FR GB IT LI |
|
17P | Request for examination filed |
Effective date: 19880205 |
|
17Q | First examination report despatched |
Effective date: 19880530 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AT CH FR GB IT LI |
|
REF | Corresponds to: |
Ref document number: 57311 Country of ref document: AT Date of ref document: 19901015 Kind code of ref document: T |
|
ITF | It: translation for a ep patent filed |
Owner name: DE DOMINICIS & MAYER S.R.L. |
|
ITTA | It: last paid annual fee | ||
GBT | Gb: translation of ep patent filed (gb section 77(6)(a)/1977) | ||
ET | Fr: translation filed | ||
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
26N | No opposition filed | ||
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: GB Payment date: 19911121 Year of fee payment: 7 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 19911127 Year of fee payment: 7 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: AT Payment date: 19911205 Year of fee payment: 7 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: CH Payment date: 19920114 Year of fee payment: 7 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: GB Effective date: 19921205 Ref country code: AT Effective date: 19921205 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LI Effective date: 19921231 Ref country code: CH Effective date: 19921231 |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 19921205 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Effective date: 19930831 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: ST |