초록 ▼

A stability system for a vehicle moving through a fluid includes stabilizers each having a drive surface that follows the position of the fluid stream perceived by the vehicle. The movement of the drive surface positions control surfaces of the stabilizers, which are coupled to the drive surfaces by

A stability system for a vehicle moving through a fluid includes stabilizers each having a drive surface that follows the position of the fluid stream perceived by the vehicle. The movement of the drive surface positions control surfaces of the stabilizers, which are coupled to the drive surfaces by mechanical linkages. Lift forces on the drive surfaces provide the force that is used in positioning the control surfaces. The deflection of the control surfaces provides a force on the vehicle that affects stability of the vehicle, for instance in making an inherently unstable vehicle more stable. The stability system may work completely passively, without any active control, and without the need for power to operate it.

대표청구항 ▼

1. A stability system for a vehicle moving through a fluid, the system comprising: a drive surface pivotable on a fuselage of the vehicle; anda control surface pivotable on the fuselage;wherein the drive surface passively pivots on the fuselage in response to changes in fluid flow external to and re

1. A stability system for a vehicle moving through a fluid, the system comprising: a drive surface pivotable on a fuselage of the vehicle; anda control surface pivotable on the fuselage;wherein the drive surface passively pivots on the fuselage in response to changes in fluid flow external to and relative to the vehicle; andwherein the drive surface is mechanically coupled to the control surface such that pivoting of the drive surface on the fuselage causes pivoting of the control surface on the fuselage, thereby passively providing a stabilizing moment on the vehicle. 2. The stability system of claim 1, wherein the pivoting of the control surface caused by pivoting of the drive surface is proportional to the pivoting of the drive surface. 3. The stability system of claim 1, wherein the pivoting of the control surface caused by pivoting of the drive surface is greater in magnitude than the pivoting of the drive surface. 4. The stability system of claim 1, wherein the pivoting of the control surface is in the same direction as the pivoting of the drive surface. 5. The stability system of claim 1, wherein the pivoting of the control surface is in the opposite direction from the pivoting of the drive surface. 6. The stability system of claim 1, further comprising a mechanical linkage that mechanically couples the drive surface and the control surface. 7. The stability system of claim 6, wherein the mechanical linkage includes a damper for damping movement of the surfaces. 8. The stability system of claim 1, further comprising: an additional drive surface on an opposite side of the fuselage from the drive surface; andan additional control surface on an opposite side of the fuselage from the control surface;wherein the additional drive surface passively pivots on the fuselage in response to changes in fluid flow external to and relative to the vehicle; andwherein the additional drive surface is mechanically coupled to the additional control surface such that pivoting of the additional drive surface on the fuselage causes pivoting of the additional control surface on the fuselage. 9. The stability system of claim 1, wherein the vehicle is inherently unstable, with a center of pressure of the vehicle forward of a center of gravity of the vehicle. 10. The stability system of claim 9, wherein the control surface is forward of the center of gravity of the vehicle. 11. The stability system of claim 9, wherein the control surface is aft of the center of gravity of the vehicle. 12. The stability system of claim 1, wherein a distance between a center of pressure of the drive surface and an axis of rotation of the drive surface is greater than a distance between a center of pressure of the control surface and an axis of rotation of the control surface. 13. The stability system of claim 1, wherein a surface area of the drive surface is less than a surface area of the control surface. 14. The stability system of claim 1, in combination with the fuselage, as parts of the vehicle. 15. A vehicle comprising: a fuselage;a drive surface pivotable on the fuselage;a control surface pivotable on the fuselage; anda mechanical linkage;wherein the drive surface passively pivots on the fuselage in response to changes in fluid flow external to and relative to the vehicle; andwherein the drive surface is mechanically coupled to the control surface by the mechanical linkage, such that pivoting of the drive surface on the fuselage causes pivoting of the control surface on the fuselage, thereby passively providing a stabilizing moment on the vehicle. 16. The vehicle of claim 15, wherein the vehicle is an air vehicle. 17. The vehicle of claim 15, wherein the vehicle is a water vehicle. 18. A method of passively stabilizing a vehicle, the method comprising: passively aligning drive surfaces of the vehicle toward an external fluid flow relative to the vehicle, by pivoting the drive surfaces on a fuselage of the vehicle; andpassively positioning control surfaces that are operatively coupled to the control surfaces by linkages, using fluid forces on the drive surfaces, acting through the linkages, pivot the control surfaces;wherein the positioning control surfaces provides stability to the vehicle. 19. The method of claim 18, wherein some of the control surfaces are forward of a center of gravity of the vehicle; andwherein other of control surfaces are aft of the center of gravity of the vehicle. 20. The method of claim 19, wherein the pivoting of the drive surfaces and the pivoting of the some of the control surfaces are rotations in the same direction; andwherein the pivoting of the drive surfaces and the pivoting of the other of the control surfaces are rotations in opposite directions.