FIELD: astronautics.
SUBSTANCE: invention relates to controlled rockets, namely, to mechanism for unfolding collapsible aerodynamic rudders or wings of unmanned aerial vehicles. Opening mechanism of aerodynamic rudder or wing is located in cavity of axis of rotation in the form of torsion block, connected by its one end to fixed part, and by another - through cocking mechanism to rotary part. Torsion unit represents cylindrical torsion located between two packages of plate torsion bars fixed on ends by inserts.
EFFECT: technical result consists in optimization of overall dimensions of aerodynamic rudders or wings in folded position while providing unfolding force in conditions of powerful incident flow, as well as in improving reliability.
4 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
MECHANISM FOR OPENING AND LOCKING HANDLEBARS WITH TWO FOLDING SECTIONS | 2021 |
|
RU2770956C1 |
FOLDING AERODYNAMIC ROCKET RUDDER | 2023 |
|
RU2803760C1 |
ROCKET AERODYNAMIC RUDDER | 2013 |
|
RU2520846C1 |
MECHANISM FOR FIXING THE CONSOLE OF THE AERODYNAMIC SURFACE OF THE ROCKET | 2022 |
|
RU2794044C1 |
MECHANISM OF OPENING AND LOCKING ROCKET WINGS | 2017 |
|
RU2675275C1 |
FOLDING AERODYNAMIC RUDDER | 2013 |
|
RU2535789C1 |
AERODYNAMIC MISSILE VANE | 2014 |
|
RU2569234C1 |
DEPLOYABLE RUDDER OF MISSILE | 2013 |
|
RU2520812C1 |
ROCKET AERODYNAMIC RUDDER | 2013 |
|
RU2532286C1 |
FOLDING WING OF SMALL-SIZED ROCKET | 2001 |
|
RU2184339C1 |
Authors
Dates
2020-07-09—Published
2019-10-10—Filed