IP Library Granted Patent US 8,091,335
Granted Patent B2
US 8,091,335 · App. 12/031,191 · Granted Jan 10, 2012

Swept fan ramp for pivot door thrust reverser

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Quick Facts
Patent No.
US 8,091,335
App. No.
12/031,191
Granted
Jan 10, 2012
Kind
B2
Abstract

A swept fan ramp for a pivot door thrust reverser includes a cylindrical unit with an elliptical flared portion, a side portion, and a rectangular flared portion. The elliptical flared portion is operable to reduce drag on airflow in a reverse direction and is coupled to the top center and bottom center of the circumference of the cylindrical unit. The side portion is operable to reduce side spillage airflow and is coupled to the central left side and central right side of the aft circumference of the cylindrical unit. The rectangular flared portion is operable to promote separation of airflow into an upper airflow path and a lower airflow path, is coupled with the aft circumference of the cylindrical unit, and is connected to the elliptical flared portion and the side portion.

Claims (42)

1. A fan ramp for a pivot door turbofan thrust reverser, the fan ramp comprising:

a cylindrical unit, operable to pass airflow from a turbine;

an elliptical flared portion, operable to reduce drag on airflow in a reverse direction, the elliptical flared portion coupled with an aft circumference of the cylindrical unit;

a side portion, operable to reduce side spillage airflow, the side portion coupled with the aft circumference of the cylindrical unit; and

a rectangular flared portion, operable to promote separation of airflow into an upper airflow path and a lower airflow path, the rectangular flared portion coupled with the aft circumference of the cylindrical unit and connected to the elliptical flared portion and the side portion.

2. The fan ramp of claim 1 , wherein the cylindrical unit is integrated with a fan duct.

3. The fan ramp of claim 1 , wherein the cylindrical unit, the elliptical flared portion, the rectangular flared portion, and the side portion form a monolithic structure.

4. The fan ramp of claim 1 , wherein the elliptical flared portion is located at the top center and bottom center of the circumference of the cylindrical unit.

5. The fan ramp of claim 1 , wherein the elliptical flared portion includes a pair of notches operable to allow movement of a pair of pivot door actuators, the pair of notches located in the top center and bottom center of the elliptical flared portion.

6. The fan ramp of claim 1 , wherein the cross section of the elliptical flared portion is approximately a quadrant of an ellipse with a roughly 2:1 ratio elliptical curve.

7. The fan ramp of claim 1 , wherein the cross section of the rectangular flared portion is approximately a quadrant of a rectangle with a rounded corner.

8. The fan ramp of claim 7 , wherein the radius of curvature of the rounded corner decreases when traversing from the elliptical flared portion to the side portion.

9. The fan ramp of claim 1 , wherein the length of the rectangular flared portion along the axis of the cylindrical unit increases and extends in the aft direction from the cylindrical unit, when traversing from the elliptical flared portion to the side portion.

10. The fan ramp of claim 1 , wherein the side portion is located at the left center and right center of the aft circumference of the cylindrical unit.

11. The fan ramp of claim 1 , wherein the side portion is generally an extension of the cylindrical unit, with a small outward flare at the aft end, the side portion being greater in length along the axis of the cylindrical unit than the elliptical flared portion and extends in the aft direction from the cylindrical unit.

12. A fan ramp for a pivot door turbofan thrust reverser, the fan ramp comprising:

a cylindrical unit, operable to pass airflow from a turbine, the cylindrical unit integrated with a fan duct;

an elliptical flared portion, operable to reduce drag on airflow in a reverse direction, the elliptical flared portion having a cross section of approximately a quadrant of an ellipse with a roughly 2:1 ratio elliptical curve and coupled with the aft circumference of the cylindrical unit;

a side portion, operable to reduce side spillage airflow, the side portion including a small outward flare at the aft end and coupled with the aft circumference of the cylindrical unit; and

a rectangular flared portion, operable to promote separation of airflow into an upper airflow path and a lower airflow path, the rectangular flared portion having a cross section of approximately a quadrant of a rectangle with a rounded corner and coupled with the aft circumference of the cylindrical unit.

13. The fan ramp of claim 12 , wherein the cylindrical unit, the elliptical flared portion, the rectangular flared portion, and the side portion form a monolithic structure.

14. The fan ramp of claim 12 , wherein the elliptical flared portion includes a pair of notches operable to allow movement of a pair of pivot door actuators, the pair of notches located in the top center and bottom center of the elliptical flared portion.

15. The fan ramp of claim 12 , wherein the elliptical flared portion is located at the top center and bottom center of the circumference of the cylindrical unit.

16. The fan ramp of claim 12 , wherein the radius of curvature of the rounded corner decreases when traversing from the elliptical flared portion to the side portion.

17. The fan ramp of claim 12 , wherein the length of the rectangular flared portion along the axis of the cylindrical unit increases and extends in the aft direction from the cylindrical unit, when traversing from the elliptical flared portion to the side portion.

18. The fan ramp of claim 12 , wherein the side portion is generally an extension of the cylindrical unit, the side portion being greater in length along the axis of the cylindrical unit than the elliptical flared portion and extends in the aft direction from the cylindrical unit.

19. A fan ramp for a pivot door turbofan thrust reverser, the fan ramp comprising:

a cylindrical unit, operable to pass airflow from a turbine, the cylindrical unit integrated with a fan duct;

an upper elliptical flared portion, operable to reduce drag on airflow in an upper airflow path, the upper elliptical flared portion having a cross section of approximately a quadrant of an ellipse with a roughly 2:1 ratio elliptical curve and coupled with the top center aft circumference of the cylindrical unit;

a lower elliptical flared portion, operable to reduce drag on airflow in a lower airflow path, the lower elliptical flared portion having a cross section of approximately a quadrant of an ellipse with a roughly 2:1 ratio elliptical curve and coupled with the bottom center aft circumference of the cylindrical unit;

a left side portion, operable to reduce spillage airflow on the left side of an airplane engine, the side portion including a small outward flare at the aft end and coupled with the left center of the aft circumference of the cylindrical unit;

a right side portion, operable to reduce spillage airflow on the right side of the airplane engine, the side portion including a small outward flare at the aft end and coupled with the right center of the aft circumference of the cylindrical unit;

a rectangular flared portion, operable to promote separation of airflow into an upper airflow path and a lower airflow path, the rectangular flared portion having a cross section of approximately a quadrant of a rectangle with a rounded corner, coupled with the aft circumference of the cylindrical unit, and connected to the upper elliptical flared portion, the lower elliptical flared portion, the left side portion, and the right side portion.

20. The fan ramp of claim 19 , wherein the cylindrical unit, the upper elliptical flared portion, the lower elliptical flared portion, the rectangular flared portion, the left side portion, and the right side portion form a monolithic structure.

21. A fan ramp for a pivot door turbofan thrust reverser, the fan ramp comprising:

a cylindrical unit, operable to pass airflow from a turbine;

an elliptical flared portion, operable to reduce drag on airflow in a reverse direction, the elliptical flared portion coupled with an aft circumference of the cylindrical unit and including a first outward flare with an elliptical cross-sectional shape;

a side portion, operable to reduce side spillage airflow, the side portion coupled with the aft circumference of the cylindrical unit and including a second outward flare that is located farther aftward than the elliptical flared portion; and

a rectangular flared portion, operable to promote separation of airflow into an upper airflow path and a lower airflow path, the rectangular flared portion coupled with the aft circumference of the cylindrical unit and positioned between the elliptical flared portion and the side portion, the rectangular flared portion including a third outward flare with a planar shape that couples to the first outward flare and extends aftward to couple with the second aftward flare.

22. The fan ramp of claim 21 , wherein the cross section of the elliptical flared portion is approximately a quadrant of an ellipse with a roughly 2:1 ratio elliptical curve.

23. The fan ramp of claim 21 , wherein the cross section of the rectangular flared portion is approximately a quadrant of a rectangle with a rounded corner.

24. The fan ramp of claim 23 , wherein the radius of curvature of the rounded corner decreases when traversing from the elliptical flared portion to the side portion.

Assignments (7)
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded May 2, 2016
From: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 038592/0181 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 22, 2015
From: SPIRIT AEROSYSTEMS, INC.
To: ROLLS-ROYCE DEUTSCHLAND LTD & CO KG
Reel/Frame 036155/0970 →
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded Jul 21, 2015
From: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 036140/0192 →
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded Apr 19, 2012
From: BANK OF AMERICA, N.A., AS COLLATERAL AGENT (INCLUDING AS SUCCESSOR COLLATERAL AGENT TO CITICORP NORTH AMERICA, INC.)
To: SPIRIT AEROSYSTEMS, INC. (FKA MID-WESTERN AIRCRAFT SYSTEMS, INC.)
Reel/Frame 028072/0314 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Apr 19, 2012
From: SPIRIT AEROSYSTEMS, INC.
To: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
Reel/Frame 028072/0647 →
PATENT SECURITY AGREEMENT Recorded Aug 24, 2009
From: SPIRIT AEROSYSTEMS, INC.
To: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
Reel/Frame 023134/0318 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 14, 2008
From: STERNBERGER, JOE E.
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 020510/0989 →