Steering system and method for use in seismic survey applications
View Patent ↗A technique facilitates the steering of seismic survey related devices during seismic survey applications. A steering device is provided with a wing pivotably mounted to a body via a pivot member. As the steering device is moved through a liquid, the liquid acts against the wing and creates a torque about the pivot member which varies according to the angle of attack of the steering device. The steering device further comprises at least one feature designed to change the torque that would otherwise act on the pivot member.
1. A method of making a steering system for use in seismic survey applications, comprising:
mounting a wing to a body via a pivot member to create a steering device in which movement of the steering device through liquid causes the wing to create a torque about the pivot member that varies according to an angle of attack;
selecting a wing profile having a blunt trailing edge of the wing which maintains a desired torque at angles of attack close to zero; and
lowering the torque at high angles of attack by providing a turbulence trigger mechanism on the wing.
2. The method as recited in claim 1 , further comprising mounting the wing to the pivot member such that the pivot member is located at a position approximately 25 percent of the length of the wing from a leading edge.
3. The method as recited in claim 1 , further comprising mounting the wing to the pivot member such that the pivot member is located at a position less than 25 percent of the length of the wing from a leading edge.
4. The method as recited in claim 1 , further comprising mounting the wing to the pivot member such that the pivot member is located at a position greater than 25 percent of the length of the wing from a leading edge.
5. The method as recited in claim 2 , wherein creating comprises creating the blunt trailing edge as a generally flat surface which transitions to adjacent wing surfaces via sharp corners, the blunt trailing edge having a height at least as great as 10 percent of the maximum thickness of the wing.
6. The method as recited in claim 3 , wherein providing comprises forming the turbulence trigger mechanism as a strip located between 5 percent and 15 percent of the chord length of the wing from a leading edge of the wing.
7. The method as recited in claim 3 , wherein providing comprises forming the turbulence trigger mechanism as a strip located approximately 10 percent of the chord length of the wing from a leading edge of the wing.
8. The method as recited in claim 3 , wherein providing comprises providing a rough surface region.
9. The method as recited in claim 3 , wherein providing comprises providing a negative step.
10. The method as recited in claim 3 , wherein providing comprises providing a positive step.
11. The method as recited in claim 3 , wherein providing comprises providing a positive step and a negative step.
12. A method of steering for use in seismic survey applications, comprising:
forming a steering device by mounting a wing to a body via a pivot member; and
positioning a blunt edge along a trailing edge of the wing to maintain a positive torque acting about the pivot member at angles of attack approaching zero.
13. The method as recited in claim 12 , further comprising pulling the steering device through an ocean to perform a seismic survey related operation.
14. The method as recited in claim 12 , further comprising creating the blunt edge with a generally flat surface.
15. The method as recited in claim 12 , further comprising lowering the torque at higher angles of attack by providing a turbulence trigger mechanism along the wing.
16. A system, comprising:
a steering device having a wing pivotably mounted to a body via a pivot member such that movement of the steering device through a liquid causes the wing to create a torque about the pivot member that varies according to an angle of attack, the steering device comprising a first feature acting to increase torque at angles of attack approaching zero and a second feature acting to decrease torque at higher angles of attack, wherein the second feature comprises a turbulence trigger mechanism positioned along a surface of the wing.
17. The system as recited in claim 16 , wherein the pivot member is located at a position approximately 25 percent of the chord length of the wing from a leading edge.
18. The method as recited in claim 16 , wherein the first feature comprises a blunt trailing edge of the wing.