Winglet ejector configurations

Patent metadata

Field	Value
Publication number	US-11053012-B2
Application number	US-202016786894-A
Country	US
Kind code	B2
Filing date	Feb 10, 2020
Priority date	Sep 2, 2015
Publication date	Jul 6, 2021
Grant date	Jul 6, 2021

Abstract

An ejector system for propelling a vehicle. The system includes a diffusing structure and a duct coupled to the diffusing structure. The duct includes a wall having openings formed therethrough and configured to introduce to the diffusing structure a primary fluid produced by the vehicle. An airfoil is positioned within the flow of the primary fluid through the openings to the diffusing structure.

First claim

What is claimed is:

1. An ejector system for propelling a vehicle, the system comprising:
a diffusing structure;
a duct coupled to the diffusing structure, the duct comprising a wall having openings formed therethrough, the openings configured to introduce to the diffusing structure a primary fluid produced by the vehicle; and
one or more airfoils coupled to the wall and positioned within the flow of the primary fluid through the openings.

2. The system of claim 1 , further comprising an intake structure coupled to the diffusing structure and configured to introduce to the diffusing structure a secondary fluid accessible to the vehicle, wherein the diffusing structure comprises an outlet structure out of which propulsive fluid flows at a predetermined adjustable velocity, and the propulsive fluid comprises the primary and secondary fluids.

3. The system of claim 1 , wherein the ejector further comprises a convex surface, the diffusing structure is coupled to the convex surface, and the duct is coupled to the convex surface and configured to introduce the primary fluid through the openings to the convex surface.

4. The system of claim 1 , wherein the one or more airfoils are triangular.

5. The system of claim 3 , wherein the convex surface includes a plurality of recesses.

6. The system of claim 1 , further comprising an actuating element coupled to the one or more airfoils and configured to cause the one or more airfoils to vibrate.

7. The system of claim 2 , wherein the intake structure is asymmetrical.

8. A vehicle, comprising:
a main body;
a gas generator coupled to the main body and producing a gas stream;
a diffusing structure coupled to the main body;
a duct coupled to the gas generator, the duct comprising a wall having openings formed therethrough, the openings configured to introduce to the diffusing structure the gas stream; and
one or more airfoils positioned within the flow of the gas stream through the openings.

9. The vehicle of claim 8 , further comprising an intake structure coupled to the diffusing structure and configured to introduce to the diffusing structure a secondary fluid accessible to the vehicle, wherein the diffusing structure comprises an outlet structure out of which propulsive fluid flows at a predetermined adjustable velocity, and the propulsive fluid comprises the gas stream and secondary fluid.

10. The vehicle of claim 8 , wherein the ejector further comprises a convex surface, the diffusing structure is coupled to the convex surface, and the duct is coupled to the convex surface and configured to introduce the gas stream through the openings to the convex surface.

11. The vehicle of claim 8 , wherein the one or more airfoils are triangular.

12. The vehicle of claim 10 , wherein the convex surface includes a plurality of recesses.

13. The vehicle of claim 8 , further comprising an actuating element coupled to the one or more airfoils and configured to cause the one or more airfoils to vibrate.

14. The vehicle of claim 9 , wherein the intake structure is asymmetrical.

Assignees

• Jetoptera Inc

Inventors

• Evulet Andrei

Classifications

• B64U50/12

  using turbine engines, e.g. turbojets or turbofans · CPC title

• B64U30/10

  Wings · CPC title

• Y02T50/10

  Drag reduction · CPC title

• B64C9/38

  Jet flaps · CPC title

• B64D27/18 Primary

  within, or attached to, wings · CPC title