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ES8605202A1 - Motocicleta-avion ultraligero - Google Patents

Motocicleta-avion ultraligero

Info

Publication number
ES8605202A1
ES8605202A1 ES534398A ES534398A ES8605202A1 ES 8605202 A1 ES8605202 A1 ES 8605202A1 ES 534398 A ES534398 A ES 534398A ES 534398 A ES534398 A ES 534398A ES 8605202 A1 ES8605202 A1 ES 8605202A1
Authority
ES
Spain
Prior art keywords
motorcycle
translation
machine
legally binding
google translate
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
Application number
ES534398A
Other languages
English (en)
Other versions
ES534398A0 (es
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
Priority to ES534398A priority Critical patent/ES8605202A1/es
Publication of ES534398A0 publication Critical patent/ES534398A0/es
Publication of ES8605202A1 publication Critical patent/ES8605202A1/es
Expired legal-status Critical Current

Links

Abstract

MOTOCICLETA-AVION ULTRALIGERO. COMPRENDE DOS ESTRUCTURAS: LA DE UNA MOTOCICLETA TODO TERRENO, CON TODOS SUS ELEMENTOS NORMALES, Y POR OTRA LA SUSTENTADORA DE UN AVION ULTRALIGERO, QUE UNIDAS COMPARTEN EL MISMO MOTOR QUE ES EL DE LA MOTOCICLETA, PARA PROPULSAR EL APARATO EN EL AIRE, O PROPULSAR LA MOTOCICLETA EN TIERRA; SIENDO LA ESTRUCTURA DE VUELO DE TIPO <CANARD>, FORMADA POR UN TUBO LONGITUDINAL (1) AL QUE ESTAN UNIDAS TRANSVERSALMENTE EL ALA (B) Y EL ESTABILIZADOR HORIZONTAL (C), INCLUYENDO EL TIMON DE DIRECCION (P), ESTANDO FORMADA EL ALA (B) POR DOS LARGUEROS SOLAMENTE Y POR CUATRO TRAVESAÑOS, QUE JUNTO AL TUBO LONGITUDINAL (A) Y LOS CABLES SUJETOS A LOS PUNTOS (A, B, C, E, F) FORMAN UN CONJUNTO SUFICIENTEMENTE RIGIDO PARA EL VUELO, HABIENDOSE INCLUIDO ADEMAS EN LOS EXTREMOS DE LAS ALAS, PATINES (H) UTILES PARA EVITAR QUE LA PUNTA ALAR ROCE CON EL SUELO.
ES534398A 1984-07-05 1984-07-05 Motocicleta-avion ultraligero Expired ES8605202A1 (es)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES534398A ES8605202A1 (es) 1984-07-05 1984-07-05 Motocicleta-avion ultraligero

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES534398A ES8605202A1 (es) 1984-07-05 1984-07-05 Motocicleta-avion ultraligero

Publications (2)

Publication Number Publication Date
ES534398A0 ES534398A0 (es) 1986-04-01
ES8605202A1 true ES8605202A1 (es) 1986-04-01

Family

ID=8487644

Family Applications (1)

Application Number Title Priority Date Filing Date
ES534398A Expired ES8605202A1 (es) 1984-07-05 1984-07-05 Motocicleta-avion ultraligero

Country Status (1)

Country Link
ES (1) ES8605202A1 (es)

Also Published As

Publication number Publication date
ES534398A0 (es) 1986-04-01

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