Peripheral Control Ejector

• US 20110250066A1
• Filed: 06/03/2010
• Published: 10/13/2011
• Est. Priority Date: 04/10/2010
• Status: Active Grant

• Current Assignee: Aeroflex Incorporated (Cobham PLC)
• Original Assignee: Aeroflex Incorporated (Cobham PLC)
• Inventors: De Roche, Mark Stephen
• Granted Patent: US 8,413,932 B2
• Time in Patent Office: Days
• US Class Current: 415/214.1
• CPC Class Codes: B64C 11/001 Shrouded propellers
• CPC Class Codes: F04D 29/544 Blade shapes
• CPC Class Codes: F04D 29/547 having a special shape in order to influence fluid flow

Abstract

A system for augmenting ducted fan thrust is provided, the system including a peripheral ejector comprised of inner and outer cowling members. With the addition of actuators mounted between the trailing edges of the inner and outer cowling members, the system may be used to generate control moments in the ducted fan. The peripheral ejector may be segmented to form discrete ejector control sections.

Claims

1. An airflow augmentation system for a ducted fan, wherein said ducted fan is comprised of a duct and a propeller, the airflow augmentation system comprising:

an inner cowling member, wherein said inner cowling member is mechanically mounted to an inside surface of a trailing edge of said duct via a plurality of inner cowling stand-offs, wherein said inner cowling member is mounted within the downwash of said propeller, and wherein a trailing edge of said inner cowling member extends below said trailing edge of said duct; and

an outer cowling member, wherein said outer cowling member is mechanically mounted to an outside surface of said trailing edge of said duct via a plurality of outer cowling stand-offs, and wherein a trailing edge of said outer cowling member extends below said trailing edge of said duct.

2. The airflow augmentation system of claim 1, wherein a leading edge of said inner cowling member is separated from a plane corresponding to said propeller by a distance equal to or less than 1/10 of a chord length of said propeller measured at said leading edge of said inner cowling member.

3. The airflow augmentation system of claim 1, wherein an inner surface of said inner cowling member is substantially parallel to an inner surface of said trailing edge of said duct.

4. The airflow augmentation system of claim 1, wherein an inner surface of said inner cowling member forms an angle of less than 18 degrees with a central inner surface of said duct.

5. The airflow augmentation system of claim 1, wherein an inner surface of said inner cowling member forms an angle of between 15 degrees and 18 degrees with a central inner surface of said duct.

6. The airflow augmentation system of claim 1, wherein an inner surface of said inner cowling member is separated from an adjacent inner duct surface by a distance equal to at least 10% of a radius corresponding to said propeller.

7. The airflow augmentation system of claim 1, wherein an inner surface of said inner cowling member is separated from an adjacent inner duct surface by a distance of between 5% and 15% of a radius corresponding to said propeller.

8. The airflow augmentation system of claim 1, wherein an inner surface of said inner cowling member is separated from an adjacent inner duct surface by a distance sufficient to allow said inner cowling member to capture at least 20% of the airflow created by said propeller within said duct.

9. The airflow augmentation system of claim 1, wherein a leading edge of an inner surface of said outer cowling member is substantially parallel to an adjacent outer surface of said duct.

10. The airflow augmentation system of claim 1, wherein said trailing edge of said outer cowling member is substantially parallel to said trailing edge of said inner cowling member.

11. The airflow augmentation system of claim 1, wherein said inner cowling member includes multiple pluralities of holes, said multiple pluralities of holes acting to reattach separated airflow.

12. The airflow augmentation system of claim 11, wherein each plurality of holes of said multiple pluralities of holes is located proximate an intersection of said inner cowling member and one of said inner cowling stand-offs.

13. The airflow augmentation system of claim 1, further comprising a plurality of ejector cavities, wherein each ejector cavity of said plurality of ejector cavities is comprised of a portion of said inner cowling member and a portion of said outer cowling member, and wherein adjacent ejector cavities are separated by a combination of one of said plurality of inner cowling stand-offs and one of said plurality of outer cowling stand-offs.

14. The airflow augmentation system of claim 13, wherein a single plurality of cowling stand-offs is comprised of said plurality of inner cowling stand-offs and said plurality of outer cowling stand-offs such that each of said plurality of cowling stand-offs is comprised of one of said plurality of inner cowling stand-offs and one of said plurality of outer cowling stand-offs.

15. The airflow augmentation system of claim 14, wherein an exit region corresponding to each ejector cavity of said plurality of ejector cavities is rectangularly-shaped.

16. The airflow augmentation system of claim 1, wherein a leading edge of said outer cowling member includes an outwardly curved inlet lip.

17. The airflow augmentation system of claim 1, further comprising a plurality of actuators, wherein each of said plurality of actuators is mounted between said trailing edge of said inner cowling member and said trailing edge of said outer cowling member, wherein each of said plurality of actuators may be positioned within at least two positions, wherein an actuator in a first position of said at least two positions provides minimal profile to airflow passing between said inner cowling member and said duct, and wherein said actuator in a second position of said at least two positions redirects airflow entering between said inner cowling member and said duct outboard between said outer cowling member and said duct.

18. The airflow augmentation system of claim 17, wherein each of said plurality of actuators has a curvilinear shape.

19. The airflow augmentation system of claim 18, wherein a cylindrical axis corresponding to said curvilinear shape is parallel to a downward vector corresponding to primary airflow when said actuator is in said first position.

20. The airflow augmentation system of claim 17, wherein each of said plurality of actuators is shaped to enhance mixing when said actuator is in said first position, said mixing occurring between said airflow entering between said inner cowling member and said duct and entrained airflow entering between outer cowling member and said duct.

21. The airflow augmentation system of claim 17, further comprising a control system coupled to said plurality of actuators, wherein said control system allows a user to select between said first position and said second position for each of said plurality of actuators.

22. The airflow augmentation system of claim 21, wherein said control system allows said user to individually select between said first position and said second position for each of said plurality of actuators.

23. The airflow augmentation system of claim 21, wherein said plurality of actuators is comprised of multiple actuator groups, wherein each actuator group is comprised of multiple individual actuators, and wherein said control system allows said user to select between said first position and said second position for individual actuator groups.

24. The airflow augmentation system of claim 23, further comprising a plurality of ejector control sections, wherein each ejector control section of said plurality of ejector control sections is comprised of a portion of said inner cowling member and a portion of said outer cowling member, wherein adjacent ejector control sections are separated by a combination of one of said plurality of inner cowling stand-offs and one of said plurality of outer cowling stand-offs, and wherein each actuator group corresponds to one of said plurality of ejector control sections.

25. The airflow augmentation system of claim 24, wherein a single plurality of cowling stand-offs is comprised of said plurality of inner cowling stand-offs and said plurality of outer cowling stand-offs such that each of said plurality of cowling stand-offs is comprised of one of said plurality of inner cowling stand-offs and one of said plurality of outer cowling stand-offs.

26. The airflow augmentation system of claim 24, wherein an exit region corresponding to each ejector control section of said plurality of ejector control sections is rectangularly-shaped.

27. The airflow augmentation system of claim 24, wherein each of said plurality of ejector control sections is of the same size.

28. The airflow augmentation system of claim 21, wherein said control system controls said position of said plurality of actuators via control cables.

29. The airflow augmentation system of claim 21, wherein said control system controls said position of said plurality of actuators via electro-mechanical servos.