Active laminar flow control structural plenums fastened

Patent metadata

Field	Value
Publication number	US-11396366-B2
Application number	US-201816147064-A
Country	US
Kind code	B2
Filing date	Sep 28, 2018
Priority date	Sep 28, 2018
Publication date	Jul 26, 2022
Grant date	Jul 26, 2022

Abstract

An active laminar flow control arrangement may comprise a modular arrangement comprising a plurality of frames and cover panels coupled to an outer skin having a plurality of hat stiffeners and stringers. A first cover panel may be coupled between a first frame and a first hat stiffener. A second cover panel may be coupled between a second frame and a second hat stiffener. A third cover panel may be coupled between the first cover panel and the second cover panel. The cover panels may enclose associated plenums whereby a flow of air is pumped into the arrangement for maintaining a laminar flow across an aerodynamic surface of the outer skin.

First claim

What is claimed is:

1. An active laminar flow control arrangement, comprising:
an outer skin having a first hat stiffener and a second hat stiffener spaced apart along an inner surface of the outer skin and a first stringer and a second stringer spaced apart along the inner surface of the outer skin, the first stringer and the second stringer are oriented substantially orthogonal with respect to the first hat stiffener and the second hat stiffener;
a first frame coupled to the inner surface and disposed between the first hat stiffener and the second hat stiffener,
a second frame coupled to the inner surface and disposed between the first hat stiffener and the second hat stiffener, the first frame and the second frame oriented substantially parallel with respect to the first hat stiffener and the second hat stiffener;
a first cover panel coupled between the first frame and the first hat stiffener;
a second cover panel coupled between the second frame and the second hat stiffener;
a third cover panel coupled between the first cover panel and the second cover panel;
a first plenum at least partially defined circumferentially between the first stringer and the second stringer, radially between the inner surface and the first cover panel, and longitudinally between the first hat stiffener and the first cover panel and/or the first frame;
a second plenum at least partially defined circumferentially between the first stringer and the second stringer, radially between the inner surface and the third cover panel, and longitudinally between the first cover panel and the second cover panel; and
a third plenum at least partially defined circumferentially between the first stringer and the second stringer, radially between the inner surface and the second cover panel, and longitudinally between the second hat stiffener and the second cover panel and/or the second frame;
wherein at least one of the first cover panel, the second cover panel, or the third cover panel extend from the first stringer to the second stringer.

2. The active laminar flow control arrangement of claim 1 , further comprising a perforated area disposed in the outer skin.

3. The active laminar flow control arrangement of claim 1 , wherein the first cover panel is coupled to the first frame via a first fastener.

4. The active laminar flow control arrangement of claim 3 , wherein the first cover panel is coupled to the first hat stiffener via a second fastener.

5. The active laminar flow control arrangement of claim 4 , wherein the third cover panel is coupled to the first cover panel via a third fastener.

6. The active laminar flow control arrangement of claim 5 , wherein the first frame is coupled to the outer skin via a fourth fastener, the fourth fastener is flush with an outer surface of the outer skin.

7. The active laminar flow control arrangement of claim 2 , further comprising a pump in fluid communication with the outer skin.

8. The active laminar flow control arrangement of claim 5 , wherein at least one of the first cover panel and the second cover panel comprises a longitudinal wall and a radial wall extending from the longitudinal wall.

9. The active laminar flow control arrangement of claim 8 , wherein the third cover panel overlaps the first cover panel and the second cover panel.

10. A nacelle inlet, comprising:
an outer skin having a first hat stiffener and a second hat stiffener spaced apart along an inner surface of the outer skin and a first stringer and a second stringer spaced apart along the inner surface of the outer skin, the first stringer and the second stringer are oriented substantially orthogonal with respect to the first hat stiffener and the second hat stiffener;
a first frame coupled to the inner surface and disposed between the first hat stiffener and the second hat stiffener,
a second frame coupled to the inner surface and disposed between the first hat stiffener and the second hat stiffener, the first frame and the second frame oriented substantially parallel with respect to the first hat stiffener and the second hat stiffener;
a first cover panel coupled between the first frame and the first hat stiffener;
a second cover panel coupled between the second frame and the second hat stiffener;
a third cover panel coupled between the first cover panel and the second cover panel;
a first plenum at least partially defined circumferentially between the first stringer and the second stringer, radially between the inner surface and the first cover panel, and longitudinally between the first hat stiffener and the first cover panel and/or the first frame;
a second plenum at least partially defined circumferentially between the first stringer and the second stringer, radially between the inner surface and the third cover panel, and longitudinally between the first cover panel and the second cover panel; and
a third plenum at least partially defined circumferentially between the first stringer and the second stringer, radially between the inner surface and the second cover panel, and longitudinally between the second hat stiffener and the second cover panel and/or the second frame;
wherein at least one of the first cover panel, the second cover panel, or the third cover panel extend from the first stringer to the second stringer.

11. The nacelle inlet of claim 10 , further comprising:
a perforated area disposed in the outer skin;
wherein at least one of the first plenum, the second plenum, and the third plenum is configured to receive a flow of ambient air from an outer surface of the outer skin via the perforated area for maintaining a laminar flow of air over the outer skin.

12. The nacelle inlet of claim 11 , further comprising a pump in fluid communication with the perforated area and configured to maintain the flow of ambient air.

13. The nacelle inlet of claim 10 , wherein the first cover panel, the second cover panel, and the third cover panel are made from a carbon fiber composite material.

14. The nacelle inlet of claim 11 , wherein the first plenum, the second plenum, and the third plenum are at least partially defined by the first stringer and the second stringer.

15. A method of installing a laminar flow control arrangement onto a nacelle inlet, comprising:
coupling a first frame to an inner surface of an outer skin of the nacelle inlet between a first stiffener and a second stiffener;
coupling a second frame to the inner surface between the first stiffener and the second stiffener;
coupling a first cover panel to a first stringer and a second stringer between the first stiffener and the first frame to enclose a first plenum, the first stringer and the second stringer circumferentially spaced apart and extending longitudinally along the inner surface of the outer skin, the first stringer and the second stringer oriented substantially orthogonal with respect to the first stiffener and the second stiffener, the first stiffener and the second stiffener extending between the first stringer and the second stringer;
coupling a second cover panel to the first stringer and the second stringer between the second stiffener and the second frame to enclose a second plenum; and
coupling a third cover panel to the first stringer and the second stringer between the first cover panel and the second cover panel to enclose a third plenum, the third plenum at least partially defined circumferentially between the first stringer and the second stringer, radially between the inner surface and the third cover panel, and longitudinally between the first cover panel and the second cover panel.

16. The method

Assignees

• Rohr Inc

Inventors

• Sanz Martinez Pablo T
• Schrell Johann Steven
• Paolini Thomas

Classifications

• B64D33/02

  of combustion air intakes · CPC title

• B64D2033/0226

  comprising boundary layer control means · CPC title

• B64C2001/0072

  from composite materials · CPC title

• B64C2230/08

  by influencing fluid flow by means of surface cavities, i.e. net fluid flow is null · CPC title

• B64C2230/22

  by using a surface having multiple apertures of relatively small openings other than slots · CPC title