ES2141982T3 - Giravion con estabilizacion giroscopica del rotor. - Google Patents

Giravion con estabilizacion giroscopica del rotor.

Info

Publication number
ES2141982T3
ES2141982T3 ES96102268T ES96102268T ES2141982T3 ES 2141982 T3 ES2141982 T3 ES 2141982T3 ES 96102268 T ES96102268 T ES 96102268T ES 96102268 T ES96102268 T ES 96102268T ES 2141982 T3 ES2141982 T3 ES 2141982T3
Authority
ES
Spain
Prior art keywords
rotor
stabilisation bar
mixture
stabilisation
lever
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
Application number
ES96102268T
Other languages
English (en)
Inventor
Bruno Ziegler
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
Priority claimed from DE29502393U external-priority patent/DE29502393U1/de
Application filed by Individual filed Critical Individual
Application granted granted Critical
Publication of ES2141982T3 publication Critical patent/ES2141982T3/es
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
    • A63H27/12—Helicopters ; Flying tops
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/58—Transmitting means, e.g. interrelated with initiating means or means acting on blades
    • B64C27/59—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical
    • B64C27/625—Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical including rotating masses or servo rotors

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Processing And Handling Of Plastics And Other Materials For Molding In General (AREA)

Abstract

SE PROPONE UN HELICOPTERO CON ALETAS SOPORTE SUJETADAS EN UNA PIEZA (1) CENTRAL DE UN CABEZAL DE ROTOR GIRATORIO, QUE FORMA EL ROTOR Y SU ANGULO ES AJUSTABLE CONTRA EL PLANO DE GIRO DEL ROTOR POR MEDIO DE BARRAS (4) DE CONTROL, ASI COMO CON UNA BARRA (5) DE ESTABILIZACION, QUE ES GIRATORIA ALREDEDOR DE UN EJE QUE DISCURRE DE FORMA PARALELA CON RESPECTO AL EJE DE AJUSTE DE LAS PALETAS SOPORTE Y ESTA SUJETO EN EL CABEZAL DEL ROTOR, DE MODO QUE EL EJE LONGITUDINAL ESTA DIRIGIDO DE FORMA PARALELA CON RESPECTO AL PLANO DEL GIRO DEL ROTOR, ASI COMO CON UN ELEMENTO (8) DE MEZCLA QUE ENGRANA EN LAS ALETAS SOPORTE, EN LAS BARRAS (4) DE CONTROL Y LA BARRA (5) DE ESTABILIZACION DE FORMA INMEDIATA O A TRAVES DE DISPOSITIVOS (7) DE TRANSMISION EN FORMA DE ENGRANE, DE TAL MODO QUE EL ANGULO DE BASCULACION DE LA BARRA (5) DE ESTABILIZACION SE MODIFICA CONTRA EL PLANO DE GIRO DEL ROTOR EN EL MISMO SENTIDO DEL ANGULO DE AJUSTE DE LA PALETA DE SUSTENTACION, DONDE SE AUMENTA LA RELACION ENTRE EL ANGULO DE BASCULACION Y LA MODIFICACION DEL ANGULO DE AJUSTE POR MEDIO DE UN DISPOSITIVO (7) DE TRANSFORMACION.
ES96102268T 1995-02-15 1996-02-15 Giravion con estabilizacion giroscopica del rotor. Expired - Lifetime ES2141982T3 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE29502393U DE29502393U1 (de) 1995-02-15 1995-02-15 Stabilisierung für Drehflügler
DE19524793A DE19524793C2 (de) 1995-02-15 1995-07-07 Steuerung für den Rotor eines Drehflügelflugzeuges

Publications (1)

Publication Number Publication Date
ES2141982T3 true ES2141982T3 (es) 2000-04-01

Family

ID=26016609

Family Applications (1)

Application Number Title Priority Date Filing Date
ES96102268T Expired - Lifetime ES2141982T3 (es) 1995-02-15 1996-02-15 Giravion con estabilizacion giroscopica del rotor.

Country Status (3)

Country Link
EP (1) EP0727350B1 (es)
AT (1) ATE186695T1 (es)
ES (1) ES2141982T3 (es)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE20121609U1 (de) 2001-03-06 2003-04-10 Vogel, Heribert, Dipl.-Ing., 71711 Steinheim Fernsteuerbares Fluggerät
US7883392B2 (en) 2008-08-04 2011-02-08 Silverlit Toys Manufactory Ltd. Toy helicopter
US8357023B2 (en) 2006-01-19 2013-01-22 Silverlit Limited Helicopter
US8002604B2 (en) 2006-01-19 2011-08-23 Silverlit Limited Remote controlled toy helicopter
BE1016960A3 (nl) 2006-01-19 2007-11-06 Rostyne Alexander Jozef Magdal Verbeterde helikopter.
USD579403S1 (en) 2006-01-19 2008-10-28 Silverlit Toys Manufactory, Ltd. Helicopter propeller rotor
US7815482B2 (en) 2006-01-19 2010-10-19 Silverlit Toys Manufactory, Ltd. Helicopter
USD546269S1 (en) 2006-01-19 2007-07-10 Silverlit Toys Manufactory, Ltd. Helicopter propeller
US7662013B2 (en) 2006-01-19 2010-02-16 Silverlit Toys Manufactory Ltd. Helicopter with horizontal control
USD582336S1 (en) 2006-08-03 2008-12-09 Silverlit Toys Manufactory Ltd. Helicopter blade, shafts and fins
US8052500B2 (en) 2008-11-25 2011-11-08 Silverlit Limited Helicopter with main and auxiliary rotors
CN102743880B (zh) * 2012-07-05 2014-12-10 罗之洪 一种碟型飞行器玩具

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2646848A (en) * 1947-02-18 1953-07-28 Bell Aircraft Corp Automatic helicopter rotor stabilizer
US4741672A (en) * 1985-07-08 1988-05-03 Gerald Breuner Collective pitch change system for teter-bar type gyroplane rotary wing aircraft
US4958786A (en) * 1987-02-03 1990-09-25 Sumitomo Precision Products Co., Ltd. Active control mechanism for a helicopter
DE29502541U1 (de) * 1995-02-16 1995-04-06 Ziegler, Bruno, 97535 Wasserlosen Rotorkopf für Drehflügler

Also Published As

Publication number Publication date
ATE186695T1 (de) 1999-12-15
EP0727350A1 (de) 1996-08-21
EP0727350B1 (de) 1999-11-17

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