IP Library › Granted Patent US 12,331,767
Granted Patent B2
US 12,331,767 · App. 17/823,700 · Granted Jun 17, 2025

Adjustable flow control systems

Inventors: Bradley Jerome Rafferty (St. Louis, MO); Rene Woszidlo (Lawrence, KS)
Assignee: The Boeing Company
F15D1/12B64C21/08F15D1/00F15D1/008
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Quick Facts
Patent No.
US 12,331,767
App. No.
17/823,700
Granted
Jun 17, 2025
Kind
B2
Abstract

An adjustable flow control system includes a fluid source, a mass-flux device and a controller. The fluid source is configured to generate a fluid flow. The mass-flux device has an inlet to receive the fluid flow. The fluid flow is transferred from the inlet to an outlet that has an exit area with a variable geometry. The controller is configured to calculate a particular exit area of the mass-flux device to achieve a flow performance metric, calculate a fluid property of the fluid flow to produce the flow performance metric based on the particular exit area, determine if the fluid source could generate the fluid flow to match the fluid property, and control the variable geometry of the exit area to establish the particular exit area in response to the fluid source being able to generate the fluid flow to match the fluid property.

Claims (57)

1. An adjustable flow control system comprising:

a fluid source configured to generate a fluid flow;

a mass-flux device with an inlet and an outlet, wherein the inlet is in fluid communication with the fluid source to receive the fluid flow, the fluid flow is transferred from the inlet to the outlet, and the outlet has an exit area with a variable geometry; and

a controller configured to:

calculate a first particular exit area of the mass-flux device to achieve a flow performance metric;

calculate a fluid property of the fluid flow to produce the flow performance metric based on the first particular exit area;

after determining that the fluid source is unable to generate the fluid flow to match the fluid property based on the first particular exit area, calculate a second particular exit area of the mass-flux device to achieve the flow performance metric; and

after determining that the fluid source is able to generate the fluid flow to match the fluid property based on the second particular exit area, control the variable geometry of the exit area of the mass-flux device to establish the second particular exit area.

2. The adjustable flow control system according to claim 1 , wherein the controller is further configured to control the fluid source to produce the fluid flow with the fluid property as calculated.

3. The adjustable flow control system according to claim 1 , wherein the fluid flow from the fluid source to the mass-flux device is reduced to approximately a minimum flow while the mass-flux device operates at the second particular exit area to produce the flow performance metric.

4. The adjustable flow control system according to claim 1 , wherein the controller is further configured to control the fluid source to adjust one or more of a pressure and a mass flow rate of the fluid flow to produce the flow performance metric.

5. The adjustable flow control system according to claim 1 , further comprising a plurality of sensors configured to measure a plurality of operating conditions.

6. The adjustable flow control system according to claim 5 , wherein the controller is further configured to:

determine the flow performance metric repeatedly in time to account for one or more changes in the plurality of operating conditions; and

update the variable geometry of the exit area of the mass-flux device in response to the one or more changes in the plurality of operating conditions.

7. The adjustable flow control system according to claim 1 , wherein the controller is further configured to iterate the variable geometry of the exit area of the mass-flux device in response to the fluid source being unable to generate the fluid flow to match the fluid property based on the first particular exit area.

8. The adjustable flow control system according to claim 1 , wherein the flow performance metric is a target momentum ratio of (i) a variable momentum of the fluid flow presented from the outlet of the mass-flux device to (ii) a freestream momentum of a freestream flow proximate the mass-flux device.

9. The adjustable flow control system according to claim 1 , wherein:

the mass-flux device is a plurality of mass-flux devices with a plurality of exit areas;

the plurality of exit areas form a total exit area; and

the control of the variable geometry is a combined control of the total exit area.

10. The adjustable flow control system according to claim 9 , wherein the combined control of the total exit area changes the plurality of exit areas to a plurality of different exit areas.

11. A method for adjustable flow control comprising:

generating a fluid flow with a fluid source;

transferring the fluid flow from an inlet to an outlet of a mass-flux device, wherein the outlet has an exit area with a variable geometry; and

calculating a first particular exit area of the mass-flux device to achieve a flow performance metric;

calculating a fluid property of the fluid flow to produce the flow performance metric based on the first particular exit area;

after determining that the fluid source is unable to generate the fluid flow to match the fluid property based on the first particular exit area, calculating a second particular exit area of the mass-flux device to achieve the flow performance metric; and

after determining that the fluid source is able to generate the fluid flow to match the fluid property based on the second particular exit area, controlling the variable geometry of the exit area of the mass-flux device to establish the second particular exit area.

12. The method according to claim 11 , further comprising:

controlling the fluid source to produce the fluid flow with the fluid property as calculated.

13. The method according to claim 11 , further comprising:

reducing the fluid flow from the fluid source to the mass-flux device to approximately a minimum flow while the mass-flux device operates at the second particular exit area to produce the flow performance metric.

14. The method according to claim 11 , further comprising:

controlling the fluid source to adjust one or more of a pressure and a mass flow rate of the fluid flow to produce the flow performance metric.

15. The method according to claim 11 , further comprising:

measuring a plurality of operating conditions with a plurality of sensors.

16. The method according to claim 15 , further comprising:

determining the flow performance metric repeatedly in time to account for one or more changes in the plurality of operating conditions; and

updating the variable geometry of the exit area of the mass-flux device in response to the one or more changes in the plurality of operating conditions.

17. The method according to claim 11 , further comprising:

iterating the variable geometry of the exit area of the mass-flux device in response to the fluid source being unable to generate the fluid flow to match the fluid property based on the first particular exit area.

18. The method according to claim 11 , wherein the flow performance metric is a target momentum ratio of (i) a variable momentum of the fluid flow presented from the outlet of the mass-flux device to (ii) a freestream momentum of a freestream flow proximate the mass-flux device.

19. The method according to claim 11 , wherein:

the mass-flux device is a plurality of mass-flux devices with a plurality of exit areas;

the plurality of exit areas form a total exit area; and

the controlling of the variable geometry is a combined controlling of the total exit area.

20. An aircraft comprising:

a flight control surface;

a plurality of sensors configured to measure a plurality of operating conditions of the aircraft;

a fluid source configured to generate a fluid flow;

a mass-flux device with an inlet and an outlet, wherein the inlet is in fluid communication with the fluid source to receive the fluid flow, the fluid flow is transferred from the inlet to the outlet, and the outlet has an exit area with a variable geometry disposed proximate the flight control surface; and

a controller configured to:

calculate a first particular exit area of the mass-flux device to achieve a flow performance metric in response to the plurality of operating conditions;

calculate a fluid property of the fluid flow to produce the flow performance metric based on the first particular exit area;

after determining that the fluid source is unable to generate the fluid flow to match the fluid property based on the first particular exit area, calculate a second particular exit area of the mass-flux device to achieve the flow performance metric; and

after determining that the fluid source is able to generate the fluid flow to match the fluid property based on the second particular exit area, control the variable geometry of the exit area of the mass-flux device to establish the second particular exit area.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 31, 2022
From: RAFFERTY, BRADLEY JEROME; WOSZIDLO, RENE
To: THE BOEING COMPANY
Reel/Frame 060954/0097 →
Continuity (1)
Related Publication 20240068495A1 · Feb 29, 2024
References Cited (5)
US 10082243B1 · Hagshenas · 2018 [cited by examiner]
US 11347204B2 · Rafferty · 2022 [cited by applicant]
US 20200102066A1 · Stefes · 2020 [cited by examiner]
US 20210223758A1 · Rafferty · 2021 [cited by examiner]
Arvin Shmilovich et al.“A Technique for Low Input Flow Control Actuation”, American Institute of Aeronautics and Astronautics, Jun. 5-9, 2017, 16 Pages, Denver, CO. [cited by applicant]