Helical spring damper

1. An aircraft damped spring assembly comprising:

an aircraft system including an aircraft component, the aircraft component having a movable member and a spring biasing the movable member in a desired direction;

a damper coacting with the spring to apply a damping load transverse to the desired direction, wherein the aircraft system includes an operating frequency, the spring includes a natural frequency near the operating frequency, and the damper reduces natural frequency below the operating frequency with the damping load;

wherein the spring is a helical coil spring and the desired direction is an axis of the spring, and the damper applies the damping load to the spring in a radial direction the spring and damper having a cylindrical shape; and

wherein the damper is in engagement with the spring generating a friction force on the spring to damp the spring.

2. The damped spring assembly of claim 1 , wherein the aircraft system is a turbine engine, and the aircraft component is a turbine case cooling valve.

3. The damped spring assembly of claim 2 , wherein the movable member is a piston having a fluid acting on the piston to move the piston in a direction opposite the desired direction.

4. The damped spring assembly of claim 3 , wherein the spring is a helical coil spring having a winding direction, and the damper is helical in shape and wound in a direction opposite the winding direction.

5. The damped spring assembly of claim 4 , comprising a solenoid for providing a fluid to move the piston to an open position opposite the direction.

6. An aircraft damped spring assembly comprising:

an aircraft system including an aircraft component, the aircraft component having a movable member and a spring biasing the movable member in a desired direction; and

a damper coacting with the spring to apply a damping load transverse to the desired direction, wherein the aircraft system includes an operating frequency, the spring includes a natural frequency near he operating frequency, and the damper reduces natural frequency below the operating frequency with the damping load, wherein the spring and damper are coaxial with one another.

7. An aircraft damped spring assembly comprising:

an aircraft system including an aircraft component, the aircraft component having a movable member and a spring biasing the movable member in a desired direction;

a damper coacting with the spring to apply a damping load transverse to the desired direction, wherein the aircraft system includes an operating frequency, the spring includes a natural frequency near the operating frequency, and the damper reduces natural frequency below the operating frequency with the damping load, wherein the damper is arranged interiorly of the spring.

8. An aircraft damped spring assembly comprising:

an aircraft system including an aircraft component, the aircraft component having a movable member and a spring biasing the movable member in a desired direction; and

a damper coacting with the spring to apply a damping load transverse to the desired direction, wherein the aircraft system includes an operating frequency, the spring includes a natural frequency near the operating frequency, and the damper reduces natural frequency below the operating frequency with the damping load;

wherein the spring is a helical coil spring and the desired direction is an axis of the spring, and the damper applies the damping load to the spring in a radial direction the spring and damper having a cylindrical shape; and

wherein the damper is helical in shape and wound in a direction opposite of a winding direction of the spring.

9. A damped spring assembly comprising:

a helical spring movable along an axis and having a winding direction;

a damper movable along the axis and including a cylindrical helical shape, the damper wound in a direction opposite the winding direction, the damper applying a radial load to the spring for damping movement of the spring along the axis;

wherein the spring includes a first axial spring rate and the damper includes a second axial spring rate, the second spring rate substantially less that the first spring rate; and

wherein the second spring rate is less than approximately 10% of the first spring rate with the spring and the damper in an assembled state.

10. The damped spring assembly of claim 9 , wherein spring and damper are coaxial with one another and include heights approximately the same as one another.

11. The damped spring assembly of claim 10 , wherein the damper includes a compressed and uncompressed stated, the damper coaxial with and applying the radial load to the spring in the compressed state in which the spring and the damper are in the assembled state, the damper having a diameter of approximately 10-15% less than that of a diameter of the damper in the uncompressed state.

12. The damped spring assembly of claim 10 , wherein the damper engages the spring and generates a friction force between the spring and damper, wherein opposing ends of the damper each include planar surfaces axially aligning the damper relative to the spring.

13. The damped spring assembly of claim 12 , wherein the damper is arranged interiorly of the spring.

14. The damped spring assembly of claim 9 , wherein the spring is a coil spring having a generally circular cross-section, and the damper is generally rectangular in shape having a width substantially greater that a thickness, a surface defined by the width engaging the spring.

15. The damped spring assembly of claim 9 , wherein the spring becomes excited at a natural frequency, the radial load damps the spring at the natural frequency.