Continuous force actuator

Claim 2

A continuous force actuator comprising: a housing, said housing being formed by a pair of C-shaped members, means for securing said C-shaped members together at substantially the midpoint thereof to form first and second substantially identical chambers, and a first and second space formed between respective ends of said pair of C-shaped members; a first piston located within said first chamber and a second piston located in said second chamber, each of said pistons having an elongated arm terminating in a T-shaped protrusion extending from one end thereof, said T-shaped protrusions being slidable within said first and said second chambers, respectively, and said elongated arms being slidable within said first and second spaces, respectively, said pistons providing said continuous force; means provided within each of said chambers for altering the position of said pistons located therein, each of said position altering means including a hollow resilient tube between one side of said T-shaped protrusion and said securing means, and a pair of hollow resilient tubes adjacent each side of said elongated arm on the other side of said T-shaped protrusion, said plurality of hollow resilient tubes also acting as a guide for said elongated arm situated within each of said chambers; and means operably connected to said position altering means for providing a motive force thereto, whereby said motive force providing means determines the amount of said continuous force.

Claim 3

In a variable configured airfoil having a first surface and a second surface, the improvement therein being in the form of at least one continuous force actuator operably connected between said first and said second surfaces, said continuous force actuator comprising: a housing, said housing being formed by a pair of C-shaped members, means for securing said C-shaped members together at substantially the midpoint thereof to form first and second substantially identical chambers, and a first and second space formed between respective ends of said pair of C-shaped members; a first piston located within said first chamber and a second piston located in said second chamber, each of said pistons having an elongated arm terminating in a T-shaped protrusion extending from one end thereof, said T-shaped protrusions being slidable within said first and said second chambers, respectively, and said elongated arms being slidable within said first and second spaces, respectively, and operably attached between said airfoil surfaces, said pistons providing said continuous force to said first and said second surfaces; means provided within each of said chambers for altering the position of said pistons located therein, each of said position altering means including a hollow resilient tube between one side of said T-shaped protrusion and said securing means, and a pair of hollow resilient tubes against each side of said elongated arm on the other side of said T-shaped protrusion, said plurality of hollow resilient tubes also acting as a guide for said elongated arm situated within each of said chambers; and means operably connected to said position altering means for providing a motive force thereto, whereby said motive force providing means determines the amount of said continuous force and thereby the configuration of said air foil.

Claim 4

In a variable configured airfoil having a first surface and a second surface, the improvement therein being in the form of at least one continuous force actuator operably connected between said first and said second surfaces, said continuous force actuator comprising: a housing, said housing being formed by a pair of C-shaped members, means for securing said C-shaped members together at substantially the midpoint thereof to form first and second substantially identical chambers, and a first and second space formed between respective ends of said pair of C-shaped members; a first piston located within said first chamber and a second piston located in said second chamber, each of said pistons having an elongated arm terminating in a T-shaped protrusion extending from one end thereof, said T-shaped protrusions being slidable within said first and said second chambers, respectively, and said elongated arms being slidable within said first and second spaces, respectively, and operably attached between said airfoil surfaces, said pistons providing said continuous force to said first and said second surfaces; means provided within each of said chambers for altering the position of said pistons located therein, each of said position altering means including a hollow resilient tube between one side of said T-shaped protrusion and said securing means, and a pair of hollow resilient tubes against each side of said elongated arm on the other side of said T-shaped protrusion, said plurality of hollow resilient tubes also acting as a guide for said elongated arm situated within each of said chambers; and means operably connected to said position altering means for providing a motive force thereto, whereby said motive force providing means determines the amount of said continuous force and thereby the configuration of said air foil.