PE20200098Z - LANDING GEAR WITH SELF-BRAKING MECHANISM FOR LANDING OF UNMANNED AIR VEHICLES - Google Patents

LANDING GEAR WITH SELF-BRAKING MECHANISM FOR LANDING OF UNMANNED AIR VEHICLES

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Publication number
PE20200098Z
PE20200098Z PE2019002204U PE2019002204U PE20200098Z PE 20200098 Z PE20200098 Z PE 20200098Z PE 2019002204 U PE2019002204 U PE 2019002204U PE 2019002204 U PE2019002204 U PE 2019002204U PE 20200098 Z PE20200098 Z PE 20200098Z
Authority
PE
Peru
Prior art keywords
landing
self
braking mechanism
wheel
uav
Prior art date
Application number
PE2019002204U
Other languages
Spanish (es)
Inventor
Jimenez Fredy Marcell Villanueva
Original Assignee
Jimenez Fredy Marcell Villanueva
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 Jimenez Fredy Marcell Villanueva filed Critical Jimenez Fredy Marcell Villanueva
Priority to PE2019002204U priority Critical patent/PE20200098Z/en
Publication of PE20200098Z publication Critical patent/PE20200098Z/en

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Abstract

La presente invencion se refiere a un tren de aterrizaje con un mecanismo de autofrenado para el aterrizaje de un UAV de pequenas dimensiones que comprende dos ruedas (2) acopladas simetricamente respecto del plano de simetria longitudinal del UAV en la parte inferior del fuselaje (1), donde cada rueda (2) comprende un neumatico (205) que cubre un aro (204) y el aro (204) tiene un eje en forma de bocina (213) que se acopla concentrica y giratoriamente sobre un eje (202) de la rueda (2) a traves de un elemento de rodamiento que se caracteriza porque ademas la rueda comprende un mecanismo de autofrenado. Los efectos beneficiosos de esta invencion son que tiene un diseno compacto, se mejora la aerodinamica durante el vuelo del UAV y proporciona un medio de amortiguacion que reduce los impactos ocasionados normalmente por los UAV del estado de la tecnica.The present invention refers to a landing gear with a self-braking mechanism for landing a small UAV that comprises two wheels (2) symmetrically coupled with respect to the longitudinal plane of symmetry of the UAV in the lower part of the fuselage (1) , where each wheel (2) comprises a tire (205) that covers a rim (204) and the rim (204) has a horn-shaped shaft (213) that is concentrically and rotatably coupled on an axis (202) of the wheel (2) through a rolling element characterized in that the wheel also comprises a self-braking mechanism. The beneficial effects of this invention are that it is compact in design, improves aerodynamics during flight of the UAV, and provides a cushioning means that reduces the impacts normally caused by state-of-the-art UAVs.

PE2019002204U 2019-10-30 2019-10-30 LANDING GEAR WITH SELF-BRAKING MECHANISM FOR LANDING OF UNMANNED AIR VEHICLES PE20200098Z (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PE2019002204U PE20200098Z (en) 2019-10-30 2019-10-30 LANDING GEAR WITH SELF-BRAKING MECHANISM FOR LANDING OF UNMANNED AIR VEHICLES

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PE2019002204U PE20200098Z (en) 2019-10-30 2019-10-30 LANDING GEAR WITH SELF-BRAKING MECHANISM FOR LANDING OF UNMANNED AIR VEHICLES

Publications (1)

Publication Number Publication Date
PE20200098Z true PE20200098Z (en) 2020-01-16

Family

ID=70471115

Family Applications (1)

Application Number Title Priority Date Filing Date
PE2019002204U PE20200098Z (en) 2019-10-30 2019-10-30 LANDING GEAR WITH SELF-BRAKING MECHANISM FOR LANDING OF UNMANNED AIR VEHICLES

Country Status (1)

Country Link
PE (1) PE20200098Z (en)

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