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 VEHICLESInfo
- 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
Links
- 230000009286 beneficial effect Effects 0.000 abstract 1
- 238000005096 rolling process Methods 0.000 abstract 1
Landscapes
- Braking Arrangements (AREA)
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.
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) |
-
2019
- 2019-10-30 PE PE2019002204U patent/PE20200098Z/en unknown
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