Fluid turbine with aero-elastic damping

Abstract

An apparatus and method for designing a diffuser-augmented wind turbine with significantly reduced time-averaged loads and significantly reduced dynamic amplification factors. Some embodiments have an annular airfoil in fluid communication with the circumference of a rotor plane, and a vertical surface with a substantially symmetrical aerodynamic form with an articulated portion.

Claims

1. A fluid turbine comprising: a rotor rotationally engaged with a generator in a nacelle; and a tower engaged with said nacelle and residing upwind of said rotor; and a pivot axis coaxial with a long axis of said tower; and a substantially vertical aerodynamic form in fluid communication with said rotor and configured to pivot about said pivot axis, having a leading edge and a trailing edge; said leading edge upwind of said trailing edge and upwind of said pivot axis; and said trailing edge downwind of said pivot axis and proximal to said rotor; and an apportioned flap pivotally engaged with said pivot axis; wherein acceleration in a first direction deflects said apportioned flap to increase force in a second direction, which opposes said first direction.

2. The fluid turbine of claim 1 further comprising: said apportioned segmented flap is engaged with a pivot arm; and said pivot arm is pivotally engaged about said pivot axis and is fixedly engaged with a mass that resides upwind of said pivot axis.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a front, right-perspective view of an exemplary embodiment of a shrouded fluid turbine with an aeroelastic damper.

(2) FIG. 2 is a side, orthographic view of the fluid turbine of FIG. 1.

(3) FIG. 3 is a top, orthographic view of the fluid turbine of FIG. 1.

(4) FIG. 4 is a top, cross-sectional, detail view of the fluid turbine of FIG. 1.

(5) FIG. 5 is a top, cross-sectional, detail view of an iteration of the fluid turbine.

DETAILED DESCRIPTION

(6) A ducted turbine provides an improved means of generating power from fluid currents. A primary shroud contains a rotor which extracts power from a primary fluid stream. A mixer-ejector pump ingests flow from the primary fluid stream and secondary flow, and promotes turbulent mixing of the two fluid streams. This enhances the power system by increasing the amount of fluid flow through the system, increasing the velocity at the rotor for more power availability, and reducing back pressure on turbine blades.

(7) Rotor refers to any assembly in which one or more blades are attached to a shaft and rotate, allowing for the extraction of power or energy from wind rotating the blades. Any propeller-like rotor or a rotor/stator assembly may be enclosed in the turbine shroud in the present disclosure.

(8) The leading edge of a turbine shroud may be considered the front, and the trailing edge of an ejector shroud may be considered the rear of the fluid turbine. A first component of the fluid turbine, located closer to the front of the turbine, may be considered upstream of a second, downstream component closer to the rear of the turbine.

(9) A wind turbine has a ringed turbine shroud surrounding a rotor, and an ejector shroud that surrounds the exit of the turbine shroud. Vertical, aerodynamic surfaces mitigate aero-elastic loads on the turbine structures.

(10) FIG. 1, FIG. 2 and FIG. 3 show a shrouded fluid turbine 100 with rotor blades 140 that are engaged with a nacelle 150 and rotate about a central axis 105. The rotor is joined to a shaft that is coaxial with the hub and with the nacelle 150. The nacelle 150 houses electrical-generation equipment. A primary airfoil 110 (referred to as a turbine shroud) is in fluid communication with the rotor 140 and is coaxial with the central axis 105. The annular airfoil 110 comprises a leading-edge, inlet portion 112, and an outlet, trailing-edge portion 116. A secondary annular airfoil 120 (referred to as an ejector shroud) has a leading edge 122 and a trailing edge 124. The leading edge 122 of the ejector shroud 120 is in fluid communication with the trailing edge 116 of the primary annular airfoil 110. The annular airfoils 110, 120 are coaxial with the rotor 140 and nacelle 150 on central axis 105. The turbine and annular airfoils are supported by a tower structure 102 and rotate about a yaw axis 107. A fairing 130 is engaged with tower structure 102 above the yaw mechanism 118.

(11) A fairing, engaged with the rotating portion of the tower, from the yaw mechanism upward, provides aerodynamic damping. In one embodiment the pivot axis of the fairing is coaxial with the pivot axis of the yaw mechanism. Mass-balancing is accomplished with a mass ahead of, or up-wind of, the yaw axis. The mass is engaged with a pivot arm or linkage that is in turn engaged with a movable flap.

(12) FIG. 4 shows a fairing 130. The fairing is a substantially symmetrical, vertical, aerodynamic form that counters the aero-elastic response of the structure to provide aerodynamic damping. The fairing 130 comprises a leading edge 132 and a trailing edge 138. The fairing's pivot axis 131 is coaxial with the yaw axis 107 (FIG. 2). In the present embodiment, the yaw axis is coaxial with the long axis of the tower 102. The fairing 130 is engaged with a mass 136. The mass 136 is ahead of (upwind of) the pivot axis 131. The weighted, pivoting fairing 130 provides mass-balancing as acceleration to the left deflects the fairing to increase the force to the right. Acceleration to the right causes the fairing 130 to deflect and increase force to the left. The passive action of the fairing counters the dynamic amplification factor of forces on the structure.

(13) FIG. 5 shows a fairing 230 with a leading edge 232 and an apportioned flap 235 that makes up the trailing edge of the fairing. The leading edge 232 pivots with the turbine 200 about the yaw axis. The pivot axis 231 is coaxial with the yaw axis, which is coaxial with the long, vertical axis of the tower 202. The apportioned flap 235 is engaged with a pivot arm 234 that is further engaged with a mass 236. The pivot arm 234 rotates about the yaw axis 231. The mass 236 is ahead of (upwind of) the pivot axis 231. The weighted, pivoting, apportioned flap 235 provides mass-balancing as acceleration to the left deflects the flap to increase the force to the right. Acceleration to the right causes the flap 235 to deflect to increase force to the left.

(14) One skilled in the art understands that the pivoting flap or pivoting fairing may also be driven to provide an aerodynamic yaw mechanism.