IP Library › Granted Patent US 6,866,475
Granted Patent B2
US 6,866,475 · App. 10/179,424 · Granted Mar 15, 2005

Fan assembly for use in powered airborne vehicles

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 6,866,475
App. No.
10/179,424
Granted
Mar 15, 2005
Kind
B2
Abstract

A fan assembly for use in association with an airborne vehicle, the fan assembly comprising a propeller assembly and a shroud. The propeller assembly is rotatably coupled to an output shaft of a motor. The propeller assembly includes at least two blades each having a first end proximate an output shaft of a motor and a second end distally spaced therefrom. The shroud extends circumferentially around the propeller assembly, and includes a groove along the lower surface thereof. In turn, the second end of the at least two blades extends at least partially into the groove.

Claims (10)

1. A fan assembly for use in association with an airborne vehicle, the fan assembly comprising:

a propeller assembly rotatably coupled to an output shaft of a motor, the propeller assembly including at least two blades each having a first end proximate an output shaft of a motor and a second end distally spaced therefrom; and

a shroud extending circumferentially around the propeller assembly, the shroud including a groove along the lower surface thereof, the groove further includes a leading side and a following side, the leading side of the groove having a depth greater than that of the following side, wherein the second ends of the at least two blades extend at least partially into the groove.

2. The fan assembly of claim 1 , wherein the shroud includes a cross-sectional configuration, the cross-sectional configuration comprising an airfoil.

3. The fan assembly of claim 1 , wherein the groove comprises a substantially uniform depth.

4. The fan assembly of claim 1 , wherein the propeller assembly comprises at least three blades.

5. The fan assembly of claim 1 , further comprising a filler assembly positioned within the groove, the fill material cooperating with the second ends of the at least two blades.

6. The fan assembly of claim 5 , wherein the filler assembly comprises a fibrous material within the groove.

7. The fan assembly of claim 6 , wherein the fibrous material comprises a brush-like material.

8. The fan assembly of claim 6 , wherein the fibrous material comprises a brush-like material.

Continuity (1)
Related Publication 20030235495A1 · Dec 25, 2003