Leading edge structure for a flow control system of an aircraft

Patent metadata

Field	Value
Publication number	US-12291323-B2
Application number	US-202117796461-A
Country	US
Kind code	B2
Filing date	Jan 27, 2021
Priority date	Jan 30, 2020
Publication date	May 6, 2025
Grant date	May 6, 2025

Abstract

A leading edge structure ( 11 ) for a flow control system of an aircraft ( 1 ), including a leading edge panel ( 13 ) surrounding a plenum ( 17 ) and having a first side portion ( 21 ), a second side portion ( 27 ), an inner surface ( 33 ) facing the plenum ( 17 ) and an outer surface ( 37 ) in contact with an ambient flow ( 39 ), wherein the leading edge panel ( 13 ) includes micro pores ( 45 ), wherein a first port device ( 49 ) is arranged in the first side portion ( 21 ) fluidly connected to the plenum ( 17 ) via a duct ( 53 ) defined by a duct structure ( 105 ), and wherein the first port device ( 49 ) comprises a first door ( 55 ) pivotable by a first hinge ( 57 ) about a first hinge axis ( 59 ).

First claim

The invention claimed is:

1. A leading edge structure for a flow control system of an aircraft, the leading edge structure comprising
a leading edge panel that surrounds a plenum in a curved manner, the plenum extending in a span direction,
wherein the leading edge panel has a first side portion extending from a leading edge point to a first attachment end,
wherein the leading edge panel has a second side portion opposite the first side portion, extending from the leading edge point to a second attachment end,
wherein the leading edge panel comprises an inner surface facing the plenum and an outer surface in contact with an ambient flow, and
wherein the leading edge panel comprises a plurality of micro pores forming a fluid connection between the plenum and the ambient flow,
wherein a first port device is arranged in the first side portion of the leading edge panel,
wherein the first port device is fluidly connected to the plenum via a duct defined by a duct structure,
wherein the first port device comprises a first door pivotable by a first hinge about a first hinge axis between at least two positions of an outlet position, a closed position, and an inlet position,
wherein the leading edge structure comprises a first actuation mechanism configured to actuate the first door for movement between the at least two positions of the outlet position, the closed position and the inlet position,
wherein the first actuation mechanism extends through the duct structure, so that a first part of the first actuation mechanism is arranged inside the duct and a second part of the first actuation mechanism is arranged outside the duct,
wherein the second part of the first actuation mechanism is attached via a hinge to a front spar of an aircraft component to which the leading edge structure is attached, and
wherein the first door is linked via a lever to the first part of the first actuation mechanism and is forward of the front spar.

2. A leading edge structure for a flow control system of an aircraft, the leading edge structure comprising
a leading edge panel that surrounds a plenum in a curved manner, the plenum extending in a span direction,
wherein the leading edge panel has a first side portion extending from a leading edge point to a first attachment end,
wherein the leading edge panel has a second side portion opposite the first side portion, extending from the leading edge point to a second attachment end,
wherein the leading edge panel comprises an inner surface facing the plenum and an outer surface in contact with an ambient flow, and
wherein the leading edge panel comprises a plurality of micro pores forming a fluid connection between the plenum and the ambient flow,
wherein a first port device is arranged in the first side portion of the leading edge panel,
wherein the first port device is fluidly connected to the plenum via a duct defined by a duct structure,
wherein the first port device comprises a first door pivotable by a first hinge about a first hinge axis between at least two positions of an outlet position, a closed position, and an inlet position,
wherein the leading edge structure comprises a first actuation mechanism configured to actuate the first door for movement between the at least two positions of the outlet position, the closed position and the inlet position,
wherein the first actuation mechanism extends through the duct structure, so that a part of the first actuation mechanism is arranged inside the duct and another part of the first actuation mechanism is arranged outside the duct,
wherein the first actuation mechanism comprises a first actuator, a first lever, and a first shaft,
wherein the first shaft is aligned with and rotatable about the first hinge axis, and is fixedly mounted to the first door,
wherein the first lever is mounted to the first shaft in a torque proof manner,
wherein the first actuator is formed as a linear actuator configured to adjust the distance between a first end and a second end,
wherein the first actuator is pivotably mounted with its first end to the first lever via a third hinge, and
wherein the first actuator is configured for being pivotably mounted with its second end to a front spar via a fourth hinge.

3. The leading edge structure according to claim 2 , wherein the first shaft is arranged to penetrate the duct structure, so that the portion of the first shaft mounted to the first door is arranged inside the duct, and the portion of the first shaft mounted to the first lever is arranged outside the duct.

4. The leading edge structure according to claim 3 , wherein in the duct structure a first shaft fitting is configured to receive the first shaft and sealing the duct structure relative to the first shaft where the first shaft penetrates the duct structure.

5. The leading edge structure according to claim 2 , wherein the first shaft is rotatably mounted to the leading edge panel via the first hinge, and
wherein the first hinge is arranged inside the duct.

6. The leading edge structure according to claim 1 , wherein a second port device is arranged in the second side portion of the leading edge panel,
wherein the second port device is fluidly connected to the plenum via the duct,
wherein the second port device comprises a second door pivotable by a second hinge about a second hinge axis between at least two positions of an outlet position, a closed position, and an inlet position.

7. The leading edge structure according to claim 6 , wherein the leading edge structure comprises a second actuation mechanism for actuating the second door for movement between the at least two positions of the outlet position, the closed position and the inlet position, and
wherein the second actuation mechanism extends through the duct structure, so that a part of the second actuation mechanism is arranged inside the duct and another part of the second actuation mechanism is arranged outside the duct.

8. The leading edge structure according to claim 7 , wherein the second actuation mechanism comprises a second actuator, a second lever, and a second shaft,
wherein the second shaft is aligned with and rotatable about the second hinge axis, and is fixedly mounted to the second door,
wherein the second lever is mounted to the second shaft in a torque proof manner,
wherein the second actuator is formed as a linear actuator configured to adjust the distance between its first and second ends,
wherein the second actuator is pivotably mounted with a first end to the second lever via a fifth hinge,
wherein the second actuator is configured for being pivotably mounted with its second end to the front spar via a sixth hinge,
wherein the second shaft is arranged in a manner that it penetrates the duct structure, so that the portion of the second shaft that is mounted to the second door is arranged inside the duct, while the portion of the second shaft that is mounted to the second lever is arranged outside the duct,
wherein in the duct structure a second shaft fitting is provided receiving the second shaft and sealing the duct structure relative to the second shaft where the second shaft penetrates the duct structure,
wherein the second shaft is rotatably mounted to the leading edge panel via the second hinge, and
wherein the second hinge is arranged inside the duct.

9. The leading edge structure according to claim 8 , wherein the duct structure has an indentation to the inside of the duct, so that two wall sections of the duct structure face each other,
wherein the second shaft penetrates the duct structure at both wall sections, so that only the portion of the second shaft mounted to the second lever is outside the duct and the rest of the second shaft is insid

Assignees

• Airbus Operations Gmbh

Inventors

• Nielsen Frank
• Obermaier Martin
• Höft Michael
• Bertolini Ivano
• Yap Jeff Wee Hong
• Rajkowski Sergej

Classifications

• B64C21/06

  for sucking (BLI propulsion B64C21/01) · CPC title

• B64C2003/146

  comprising leading edges of particular shape · CPC title

• B64C21/08

  adjustable · CPC title

• B64C3/50

  by leading or trailing edge flaps · CPC title

• Y02T50/10

  Drag reduction · CPC title