Ejector and airfoil configurations

Patent metadata

Field	Value
Publication number	US-10875658-B2
Application number	US-201816031586-A
Country	US
Kind code	B2
Filing date	Jul 10, 2018
Priority date	Sep 2, 2015
Publication date	Dec 29, 2020
Grant date	Dec 29, 2020

Abstract

A propulsion system coupled to a vehicle. The system includes an ejector having an outlet structure out of which propulsive fluid flows at a predetermined adjustable velocity. A control surface having a leading edge is located directly downstream of the outlet structure such that propulsive fluid from the ejector flows over the control surface.

First claim

What is claimed is:

1. A propulsion system for a vehicle, the system comprising:
a primary airfoil coupled to the vehicle;
a first augmenting airfoil coupled to the vehicle and positioned downstream of fluid flowing over the primary airfoil, the first augmenting airfoil comprising a first output structure and at least one first conduit coupled to the first output structure, the at least one first conduit configured to introduce to the first output structure a primary fluid produced by the vehicle, the first output structure comprising a first terminal end configured to provide egress for the introduced primary fluid toward the primary airfoil and out of the first augmenting airfoil; and
a secondary airfoil located directly downstream of the first augmenting airfoil such that the fluid flowing over the primary airfoil and the primary fluid from the first augmenting airfoil flows over the secondary airfoil.

2. The system of claim 1 , further comprising a second augmenting airfoil coupled to the vehicle and positioned downstream of fluid flowing over the primary airfoil, each of the first and second augmenting airfoils having a leading edge disposed toward the primary airfoil, the first augmenting airfoil opposing the second augmenting airfoil whereby:
the first and second augmenting airfoils define a diffusing region; and
the leading edges define an intake region configured to receive and introduce to the diffusing region the primary fluid and the fluid flowing over the primary airfoil, the diffusing region comprising a primary terminal end configured to mix and provide the introduced primary fluid and fluid flowing over the primary airfoil to the secondary airfoil.

3. The system of claim 2 , wherein the second augmenting airfoil comprises a second output structure and at least one second conduit coupled to the second output structure, the at least one second conduit configured to introduce to the second output structure the primary fluid produced by the vehicle, the second output structure comprising a second terminal end configured to provide egress for the introduced primary fluid toward the primary airfoil and out of the second augmenting airfoil.

4. The system of claim 1 , further comprising a first actuator configured to rotate the first augmenting airfoil relative to the vehicle.

5. The system of claim 2 , further comprising a second actuator configured to rotate the second augmenting airfoil relative to the vehicle.

Assignees

• Jetoptera Inc

Inventors

• Evulet Andrei

Classifications

• Y02T50/10

  Drag reduction · CPC title

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title

• B64C9/38

  Jet flaps · CPC title

• B64C15/00 Primary

  Attitude, flight direction, or altitude control by jet reaction · CPC title

• F02C6/04

  Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output (F02C6/18 takes precedence {; for a fluidised-bed combustor F02C3/205}) · CPC title