EP0449922A1 - Spielflugzeug, bewegt durch schwingungen der flügel. - Google Patents

Spielflugzeug, bewegt durch schwingungen der flügel.

Info

Publication number
EP0449922A1
EP0449922A1 EP90900894A EP90900894A EP0449922A1 EP 0449922 A1 EP0449922 A1 EP 0449922A1 EP 90900894 A EP90900894 A EP 90900894A EP 90900894 A EP90900894 A EP 90900894A EP 0449922 A1 EP0449922 A1 EP 0449922A1
Authority
EP
European Patent Office
Prior art keywords
slot
crank
wings
wing
flying toy
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.)
Granted
Application number
EP90900894A
Other languages
English (en)
French (fr)
Other versions
EP0449922B1 (de
Inventor
Ruymbeke Gerard Van
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of EP0449922A1 publication Critical patent/EP0449922A1/de
Application granted granted Critical
Publication of EP0449922B1 publication Critical patent/EP0449922B1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

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
    • A63H27/008—Propelled by flapping of wings

Definitions

  • the present invention relates to a flying toy able to move in the air by flapping its wings, imitating the flight of a bird whose said toy can advantageously have the appearance. It also relates to a process allowing the automatic blocking of the
  • French patent NO 1.604.345 includes: - an elongated hollow body made in two parts
  • the wing actuation mechanism is
  • this mechanism comprises two oscillating levers or wing feet passing through two lateral openings which the said body has in front of said socket, these oscillating levers or wing feet being connected or intended to be connected, each, to a wing beam on which is fixed the front edge of the flexible wing
  • flywheels of the aforementioned kind the flapping of the wings ensuring the sustenance of the flying toy ceases when the motor elastic is completely relaxed.
  • the rhythm of the wing beats decreasing with the torsional torque of the motor elastic it happens that these beats cease, as a result of the complete relaxation of the latter, while the toy is at a short distance from the ground or has just make contact with it, allowing a soft landing of the toy.
  • this type of toy is struck by a servitude resulting from the obligation to manually place the retainer in the neutralization position of the wing actuation mechanism, before proceeding to reassemble the latter, which users who are most frequently children do not immediately think of doing.
  • the object of the invention is in particular to remedy these drawbacks.
  • this objective is achieved by a method and a device according to which the stop is applied, under the effect of an elastic pressure, against the periphery provided with a notch of the circular plate of the crank d drive of the wing actuation mechanism, so that when the engine elastic develops its normal power under the effect of the torque, the retainer cannot engage and be maintained in this notch, while when this power approaches its lowest value, when approaching full untwisting of said power elastic, said retainer can engage and
  • the locations of the active part of the stopper and the notch in the kinematic chain of said mechanism being preferably determined so that the engagement position of said stopper and of said slot corresponds to the position of the wings allowing the flight plane.
  • the flying toy always ends its gliding flights, which allows it to land smoothly.
  • the wing actuation mechanism is always locked by the stopper, so it is not necessary to handle this stopper before proceeding with a new reassembly of the drive system of said mechanism by the rotation of the crank arranged at the rear part of the toy body.
  • Figure 1 is a perspective view, partially broken away, of a flying toy which can be advantageously equipped with the actuating and immobilizing device of the wings according to the invention.
  • Figure 2 is a front view of this device shown in the locking position.
  • Figure 3 is a front view showing the device in a dynamic situation.
  • Figure 4 is a front view of the fixed structure of this device.
  • Figure 5 is a side view of the system providing the driving force to the mechanism
  • Figure 6 is a front view of this
  • Figure 7 is a front view of the stop. Reference is made to said drawings to describe an interesting example of embodiment of the device and implementation of the method according to the invention.
  • the flying toy to which the invention relates is of the kind comprising a hollow body 1 of elongated shape, executed in two parts assembled by interlocking, this body usually being made of plastic.
  • this body In the front part of this body is housed an actuation mechanism of the wings designated as a whole by the reference 2 in FIG. 1 and moved by means of an elastic strap providing the driving force.
  • This mechanism makes it possible to communicate identical oscillations to wing feet 3 placed through lateral openings 4 formed in the body 1 and the external parts of which are connected or arranged so that they can be connected, for example by interlocking, to the beams or wing spars 5 on which is fixed the front edge of the main wing 6 constituting the flexible wings of the toy and whose rear edge is secured to said body, by hooking on a lug, by gluing or otherwise.
  • elastic motor is installed at the rear part of the body 1 which also carries an adjustable tail blade 8 acting as a rudder.
  • the wing actuation mechanism 2 installed in the rear portion of the front part of the body 1, comprises a rigid annular frame 9 conforming to the transverse profile of said rear portion.
  • This frame ( Figure 4) is provided, on its periphery, with at least one lug 10 housed in a notch 11 provided in the body 1, so as to cooperate in the immobilization of said frame inside the latter.
  • the fixed frame 9 stiffened by reinforcements is formed in one piece with:
  • a circular cage 39 arranged around the bearing 12 and concentrically with the latter.
  • the drive crank or front crank 18 ( Figures 5 and 6) mainly comprises:
  • a rear end 19 arranged in the form of a hook on which is fixed one of the ends of the elastic strap 20 supplying the driving energy and the other end of which is fixed to the hook 7a of the crank of the winding system 7 installed at
  • crank plate 22 provided with a crank pin 23 ending in a hook 24.
  • the crank plate 22 is constituted by a cylinder of short length, having a smooth outer surface and in the periphery of which is formed a slot 25 of variable width and dividing said cylinder into two parts:
  • a first flexible part 26 connected to the shaft 21, on the one hand, by a rigid rib 27 and, on the other hand, by a flexible hinge 37 much thinner than the previous one; said flexible part thus constituting a spring;
  • the flexible 26 and movable 28 parts have approximately equal lengths and the crank pin 23 of the crank 18 is integral with said movable part 28.
  • the movable part 28 itself consists of two parts:
  • the end of the shaft 21 is provided with:
  • a ramp 29 arranged inside the space delimited by the cylindrical wall of the plate 22 and near the free end of the movable part 28 thereof, in order to guide this end towards the fixed edge 38 of the slot 25;
  • a radial projection 30 intended to cooperate with a projection 31 which is provided,
  • the crank plate 22 is rotatably mounted in the fixed cage 39 formed by a split cylinder, and which opposes the rotation of the deformable crank plate 22 in the opposite direction to that of its functional drive, forming a braking drum.
  • the stop 32 is constituted by a rocking lever mounted with a pivoting ability, by means of its intermediate portion, on the axis 14, and it comprises:
  • the slot 25 At rest or when approaching the rest position of the drive crank 18, the slot 25 has a width greater than that of the tooth 33 of
  • the tooth 33 of the retainer 32 has a width greater than the minimum width that the slot 25 has when the flexible part 26 is bent and when the end 28a of the movable part 28 occupies a position close to the fixed edge 38 of said slot, so that, in this situation, the tooth can not engage and be maintained in the slot.
  • the free end of the internal part 32b is provided with lugs 34 and 35 intended to come into abutment against the stops 16 and 17 which limit the amplitude of the pivoting of the stop 32 in both directions.
  • the wing actuation mechanism further comprises two transmission b-links 36 which are articulated, on the one hand, via one of their ends, on the crank pin 23 of the crank
  • the wing actuation mechanism which has just been described is arranged, according to the invention, so that when the tooth 33 of the stopper 32 meshes with the notch 25, the external part of the wing feet and, by Consequently, the wing beams 5 engaged in the latter, occupy a position according to which they form an angle of small amplitude at or below the horizontal (of the order of 10 degrees), this position allowing gliding (figure 2).
  • the operation of the device and the implementation of the method according to the invention are well understood.
  • the tooth 33 of the stopper 32 is engaged, under the pressure of the spring 15, in the notch or slot 25 of variable width of the plate 22 of the drive crank 18.
  • the wing actuation mechanism is is locked and it is therefore possible to twist the elastic motor strap 20 by means of the crank of the winding system 7, so as to store the energy necessary for flight.
  • the wing actuation mechanism is then unlocked by tilting the stop 32 by means of the operating lever 32a, so as to remove the tooth 33 from the slot 25, and the toy can then be released.
  • the drive crank 18 is driven in
  • the resistance opposed by the movement of the wings to the power developed by the elastic motor generates a torque which causes a deformation of the flexible part 26 of the crank plate 22, so that the movable part 28 of said plate tilts around the hinge 37 and that the flexible portion 28c of said movable part slides on the ramp 29 and that its free end 28a approaches the fixed edge 38 opposite the slot 25, the width of which is thus narrowed. Because of this
  • the wing actuation mechanism is locked, so that it is possible to reassemble the engine system without

Landscapes

  • Toys (AREA)
EP90900894A 1988-12-20 1989-12-19 Spielflugzeug, bewegt durch Schwingungen der Flügel Expired - Lifetime EP0449922B1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR8817547 1988-12-20
FR8817547A FR2640518B1 (fr) 1988-12-20 1988-12-20 Jouet volant se mouvant par battements d'ailes, et procede permettant le blocage automatique des ailes, en fin de vol
PCT/FR1989/000663 WO1990006794A1 (fr) 1988-12-20 1989-12-19 Jouet volant se mouvant par battements d'ailes, et procede permettant le blocage automatique des ailes, en fin de vol

Publications (2)

Publication Number Publication Date
EP0449922A1 true EP0449922A1 (de) 1991-10-09
EP0449922B1 EP0449922B1 (de) 1995-03-08

Family

ID=9373672

Family Applications (1)

Application Number Title Priority Date Filing Date
EP90900894A Expired - Lifetime EP0449922B1 (de) 1988-12-20 1989-12-19 Spielflugzeug, bewegt durch Schwingungen der Flügel

Country Status (9)

Country Link
US (1) US5163861A (de)
EP (1) EP0449922B1 (de)
JP (1) JP2854127B2 (de)
AT (1) ATE119422T1 (de)
AU (1) AU4822890A (de)
DE (1) DE68921642T2 (de)
ES (1) ES2071813T3 (de)
FR (1) FR2640518B1 (de)
WO (1) WO1990006794A1 (de)

Families Citing this family (48)

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US5100357A (en) * 1990-05-10 1992-03-31 Aerovironment, Inc. Toy aircraft and method of flight control thereof
US5176559A (en) * 1992-03-27 1993-01-05 Stephen Lane Toy glider
US5993286A (en) * 1999-04-27 1999-11-30 Tacquard; Timothy L. Walking insect and method of assembling the same
US6206324B1 (en) 1999-08-30 2001-03-27 Michael J. C. Smith Wing-drive mechanism, vehicle employing same, and method for controlling the wing-drive mechanism and vehicle employing same
US6632119B2 (en) * 2000-03-01 2003-10-14 Marvel Enterprises, Inc. Winding device and ornithopter utilizing same
US6227483B1 (en) 2000-04-05 2001-05-08 SUCCESSION CLéMENT THERRIAULT Wing movement for ornithopters and apparatus of the like
WO2002010014A1 (en) * 2000-07-28 2002-02-07 Aerodavinci Co., Ltd. Flying object by flapping motion of wings equipped with compressed air engine
US6773329B2 (en) 2000-10-02 2004-08-10 All Season Toys, Inc. Amusement device including a thematic play set
JP3889956B2 (ja) * 2001-02-27 2007-03-07 シャープ株式会社 移動装置
US6565039B2 (en) 2001-03-19 2003-05-20 Michael J. C. Smith Wing-drive mechanism and vehicle employing same
WO2003020585A1 (en) * 2001-09-04 2003-03-13 Aerodavinci Co., Ltd. Wing assembly of flying object for flapping motion of wings
GB0122677D0 (en) 2001-09-20 2001-11-14 Tomas Eric E Toy ornithopter aircraft
KR20030037916A (ko) * 2001-11-07 2003-05-16 (주)에어로다빈치 압축공기엔진 및 이를 이용한 비행체
KR100451984B1 (ko) * 2001-11-16 2004-10-08 주식회사 뉴로스 동력식 날개치기형 비행기
KR20030044625A (ko) * 2001-11-30 2003-06-09 주식회사 뉴로스 원격조종이 가능한 동력식 날개치기형 비행기
US6824094B2 (en) * 2002-06-06 2004-11-30 Charron Richard Power assembly for ornicopter
JP4115349B2 (ja) * 2002-07-12 2008-07-09 シャープ株式会社 羽ばたき浮上移動装置
JP4011538B2 (ja) * 2003-01-16 2007-11-21 シャープ株式会社 羽ばたき装置
US20070138339A1 (en) * 2003-06-18 2007-06-21 Sinclair Peter L Motion assisting apparatus for flying objects
US6783097B1 (en) 2004-01-12 2004-08-31 Michael J. C. Smith Wing-drive mechanism and vehicle employing same
US8181907B2 (en) * 2004-01-12 2012-05-22 Smith Michael J C Wing-drive mechanism and vehicle employing same
US7255305B2 (en) * 2004-11-02 2007-08-14 Milan Dennis Earl Flying device utilizing natural principles
US20070205322A1 (en) * 2006-03-06 2007-09-06 Wei-Hsiang Liao Micro aviation vehicle
US20070210207A1 (en) * 2006-03-06 2007-09-13 Wei-Hsiang Liao Flying wing rotation mechanism of micro air vehicle
US7654881B2 (en) 2006-06-12 2010-02-02 Mattel, Inc. Action figure with movable appendages
US7536823B2 (en) * 2006-10-18 2009-05-26 Brint George W Flying bird decoy and method
USD558661S1 (en) * 2007-08-03 2008-01-01 Silverlit Toys Manufactory, Ltd. Flying device
US20100136877A1 (en) * 2008-01-10 2010-06-03 Maddi Michael S Self-supporting puppet
TW200930619A (en) * 2008-01-15 2009-07-16 Univ Tamkang Biomimetc micro air vehicle with 8-shaped flapping wing trajectory
US9144236B2 (en) * 2008-03-27 2015-09-29 Craig A. Price Bird decoy
US8210896B2 (en) * 2008-04-21 2012-07-03 Mattel, Inc. Light and sound mechanisms for toys
FR2934789B1 (fr) * 2008-08-05 2010-10-29 Ruymbeke Edwin Van Jouet volant apte a se mouvoir par battement d'ailes.
CN105966616B (zh) * 2009-06-05 2019-06-11 威罗门飞行公司 飞行器飞行机构和控制方法
KR101031869B1 (ko) 2009-06-08 2011-05-02 건국대학교 산학협력단 큰 날갯짓 각도를 발생하는 날갯짓 장치
GB2481458A (en) * 2010-06-26 2011-12-28 Darren John Bailey Radio Controlled Flapping and Flying Decoy
US8382546B2 (en) * 2010-07-05 2013-02-26 Edwin VAN RUYMBEKE Flying toy able to move by the flapping of wings
US9669925B2 (en) 2011-02-16 2017-06-06 Aerovironment, Inc. Air vehicle flight mechanism and control method for non-sinusoidal wing flapping
EP2675708A4 (de) * 2011-02-17 2014-09-10 Georgia Tech Res Inst Schwebendes und gleitendes mehrflügel-mikroluftfahrzeug
CA2846886C (en) 2013-03-15 2016-02-09 Francois Matte Wing flapping mechanism and method
US9072981B2 (en) * 2013-05-15 2015-07-07 Tanous Works, Llc Hovering toy figure
US9533234B2 (en) * 2013-05-15 2017-01-03 Tanous Works, Llc Hovering toy creature
CN104163083A (zh) * 2013-05-19 2014-11-26 刘祖学 多用车
US10017248B2 (en) * 2014-04-28 2018-07-10 University Of Maryland, College Park Flapping wing aerial vehicles
FR3032126B1 (fr) * 2015-02-02 2017-01-06 Ruymbeke Gerard Ange Marie Joseph Van Jouet a moteur a elastique a remontage manuel et dispositif qui evite sa rupture lors d'un remontage excessif
TWI580463B (zh) * 2016-01-20 2017-05-01 Genius Toy Taiwan Co Ltd Wings flying toys
CN107080957A (zh) * 2016-02-15 2017-08-22 智高实业股份有限公司 振翅飞行玩具
KR102217798B1 (ko) * 2019-10-03 2021-02-18 이상철 고속 하향 날갯짓 비행장치
US12427436B1 (en) * 2022-04-12 2025-09-30 Russell Reiner Wing assembly and a device for coupling to a toy

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US2457281A (en) * 1946-05-11 1948-12-28 John K Shannon Control mechanism for model airplanes
US2763348A (en) * 1954-04-30 1956-09-18 Harry W Corbitt Brake for motor-operated airplane landing gear
FR1604345A (de) * 1968-12-31 1971-10-11
US3626555A (en) * 1969-12-01 1971-12-14 Prosper Albertini Flying toy
DE2411148C3 (de) * 1974-03-08 1980-10-30 Hermann Dr. 8510 Fuerth Neuhierl Modell-Luftschraube mit zusammenklappbaren Luftschraubenblättern
GB1564900A (en) * 1975-06-24 1980-04-16 Allied Int Designers Models propelled by elastic motors
DE2755786A1 (de) * 1976-12-21 1978-06-29 Gerard De Ruymbeke Spielflugzeug mit mechanischem antrieb der fluegel
FR2422423A1 (fr) * 1978-04-14 1979-11-09 Lapierre Philippe Moteur a ressort caoutchouc a remontage rapide
JPS6071291U (ja) * 1983-10-21 1985-05-20 株式会社トミー 走行玩具
FR2580944B1 (fr) * 1985-04-26 1987-06-19 Ruymbeke Gerard Van Jouet volant
US4850931A (en) * 1988-09-06 1989-07-25 Buddy L Corporation Spin-out toy vehicle

Non-Patent Citations (1)

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Title
See references of WO9006794A1 *

Also Published As

Publication number Publication date
JP2854127B2 (ja) 1999-02-03
EP0449922B1 (de) 1995-03-08
DE68921642T2 (de) 1995-12-14
WO1990006794A1 (fr) 1990-06-28
DE68921642D1 (de) 1995-04-13
FR2640518B1 (fr) 1991-03-22
AU4822890A (en) 1990-07-10
FR2640518A1 (fr) 1990-06-22
JPH04503615A (ja) 1992-07-02
ATE119422T1 (de) 1995-03-15
US5163861A (en) 1992-11-17
ES2071813T3 (es) 1995-07-01

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