Flight controls with automatic balance
OwnerManuel Munoz Saizinventor
Life of this patent
Estimating the term…
Abstract
Flight controls with automatic balance for use in control of the movement of an aircraft through a fluid system, the control system consists of ailerons divided into two parts, which at low speed adopt the shape of a conventional aileron and rotate in their entirety with the same degree and at high speeds, a part of it rotates or extends to a determinated angle by means of the actuator and the other part of the aileron, that is hinged or articulated to the main part of the aileron, rotates with reference to the main part as a function of the air speed pressure, opposing to this rotation by means of one or more springs.
Claims12
Flight controls with automatic balance that at low speed adopt the shape of a conventional aileron and at high speed flex backward comprising:
- a wing,
- an aileron comprising:
- a front part, wherein said front part is rigid,
- a rear part, wherein said rear part is flexible and is connected to said front part,
- a hinge that connects said wing to the front section of said aileron,
- an actuator that rotates said aileron on said hinge, and,
- springs that tend to keep said rear part in line with said front part.
Flight controls with automatic balance that at low speed adopt the shape of a conventional aileron and at high speed flex backward comprising:
- a wing,
- an aileron comprising:
- a front part, wherein said front part is rigid,
- a rear part, wherein said rear part is flexible and is connected to said front part,
- a hinge that connects said wing to the front section of said aileron,
- an actuator that rotates said aileron on said hinge, springs that tend to keep said rear part in line with said front part, wherein the rear part is attached to the front part by a strip that extends from said rear part to under said front part.
Flight controls with automatic balance that at low speed adopt the shape of a conventional aileron and at high speed flex backward comprising:
- a wing,
- an aileron comprising:
- a front part, wherein said front part is rigid,
- a rear part, wherein said rear part is flexible and is connected to said front part,
- a hinge that connects said wing to the front section of said aileron,
- an actuator that rotates said aileron on said hinge, springs that tend to keep said rear part in line with said front part, wherein said rear part further comprises:
- a top surface,
- a bottom surface,
- a first wavy strip wherein said first wavy strip is inside said aileron and is attached to said top surface, and
- a second wavy strip, wherein said second wavy strip is inside said aileron and is attached to said bottom top surface.
Flight controls with automatic balance that at low speed adopt the shape of a conventional aileron and at high speed flex backward comprising:
- a wing,
- an aileron comprising:
- a front part, wherein said front part is rigid,
- a rear part, wherein said rear part is flexible and is connected to said front part,
- a hinge that connects said wing to the front section of said aileron,
- an actuator that rotates said aileron on said hinge, springs that tend to keep said rear part in line with said front part, wherein said rear part comprises a plurality of plates wherein each plate has a strip extending laterally across said plate.
Flight controls with automatic balance that at low speed adopt the shape of a conventional aileron and a high speed flex backward comprising:
- two symmetric wings, wherein each of said wings is connected by a hinge to an aileron comprising:
- a front part, wherein said front part is rigid,
- a rear part, wherein said rear part is flexible and is connected to said front part,
- an actuator that rotates said ailerons on said hinges, and springs that tend to keep said rear part in line with said front part.
Flight controls with automatic balance that at low speed adopt the shape of a conventional control surface aileron, rudder or elevator and at high speed flexes backward comprising:
- a wing,
- a flight control surface having
- a first rigid section, and a second flexible section connected to said first rigid section,
- a hinge that connects said wing to said first rigid section of said flight control surface,
- an actuator that rotates said flight control surface on said hinge, and,
- a spring that tends to keep said second flexible section in line with said first rigid second.
Dependencies are inferred from the claim text.