Aero-acoustic optimisation method for complex-section mechanical parts and corresponding mechanical part and landing gear

• US 8,668,164 B2
• Filed: 06/20/2011
• Issued: 03/11/2014
• Est. Priority Date: 06/21/2010
• Status: Active Grant

• Current Assignee: Airbus Operations (European Aeronautic Defence and Space Company EADS NV)
• Original Assignee: Airbus Operations (European Aeronautic Defence and Space Company EADS NV)
• Inventors: Seror Goguet, Christelle
• Primary Examiner(s): Collins, Timothy D
• Assistant Examiner(s): Stehle, Jamie S
• Application Number:
  US13/163,895
• Publication Number:
  US 20110309193A1
• Time in Patent Office: 995 Days
• Field of Search: 244/1.N, 244/130, 244/121, 244/100.R, 244/102.R, 244/103.R, 244/102.A
• US Class Current: 244/102.A
• CPC Class Codes: B64C 2025/003 Means for reducing landing gear noise, or turbulent flow around it, e.g. landing gear doors used as deflectors
• CPC Class Codes: B64C 25/001 Devices not provided for in the groups B64C25/02 - B64C25/68
• CPC Class Codes: B64C 25/16 Fairings movable in conjunction with undercarriage elements
• CPC Class Codes: B64C 7/00 Structures or fairings not otherwise provided for
• CPC Class Codes: Y10T 29/49 Method of mechanical manufacture
• CPC Class Codes: Y10T 428/12361 having aperture or cut
• CPC Class Codes: Y10T 428/12375 having member which crosses the plane of another member [e.g., T or X cross section, etc.]

Abstract

An apparatus and method are provided for reducing the drag caused by a complex-section part in an airflow, for example the landing gear of an aircraft, making it possible to optimize the lift/drag ratio and to reduce the aerodynamic noise by reducing the local noise source. To do so, the complex-section part is masked with a special casing. More specifically, the aero-acoustically optimized complex-section metal mechanical part is fitted with an aerodynamically shaped cover made of several longitudinal parts articulated with hinges to facilitate their installation. This cover is attached to at least two supports placed away from one another along the axis of the part, each support locally mating with the section of the part.

Claims

1. An aero-acoustic optimization method for a mechanical metal part structure extending longitudinally along a longitudinal axis and that can be placed in an airflow, the metal part structure having a longitudinal groove extending parallel to the longitudinal axis and a transverse cross-section perpendicular to the longitudinal axis, the method comprising:

arranging at least two supports such that each support is positioned about the longitudinal axis of the metal part structure, each support having an external contour and an internal contour, the internal contours mated at least partially against the transverse cross-section of the metal part structure, and such that the at least two supports are arranged offset from each other in a direction of the longitudinal axis; and

aerodynamically enveloping the metal part structure with an aerodynamic envelope attached to the at least two supports and including a cover having an external cylindrical face and an internal face that presses against the external contours of the at least two supports, and the cover is attached to the at least two supports using fixed connectors, such that the cover transversely envelops the at least two supports and at least a portion of the longitudinal groove from the airflow.

2. The method according to claim 1, further comprising:

leaving the part partially visible to facilitate inspection of the part.

3. The method according to claim 1, further comprising:

providing passive noise absorption by partially enveloping the part with a mesh.

4. The method according to claim 1, further comprising:

enveloping the part by a variable-curvature aerodynamic shape.

5. A mechanical part that is aero-acoustically optimized for placement in an airflow, the mechanical part comprising:

a metal part structure extending longitudinally along a longitudinal axis, the metal part structure having a longitudinal groove extending parallel to the longitudinal axis and a transverse cross-section perpendicular to the longitudinal axis,

at least two supports, each support positioned about the longitudinal axis and having an external contour and an internal contour, the internal contour at least partially mated against the transverse cross-section of the part structure, wherein the at least two supports are arranged offset from each other in a direction of the longitudinal axis, and

an aerodynamic envelope attached to the at least two supports and including a cover having an external cylindrical face and an internal face that presses against the external contours of the at least two supports, and the cover is attached to the at least two supports using fixing connectors such that the cover transversely envelops the at least two supports and at least a portion of the longitudinal groove from the airflow.

6. The mechanical part according to claim 5, further comprising:

stops that are formed on the part structure and placed on either side of the at least two supports to stop the cover from moving.

7. The mechanical part according to claim 5, wherein each of the at least two supports comprises a plate of constant thickness.

8. The mechanical part according to claim 5, wherein each of the at least two supports comprises at least two parts connected to each other.

9. The mechanical part according to claim 5, wherein the external cylindrical face of the cover has an aerodynamic shape of circular, elliptical, oblong, oval or droplet section that is at least partially cylindrical.

10. The mechanical part according to claim 5, wherein at least one of the cover and the at least two supports are made of composite or plastic material defining a density significantly lower than a density of the metal part structure.

11. The mechanical part according to claim 5, wherein the cover comprises at least two cover parts and a longitudinal hinge between the at least two parts that can open along a longitudinal length of the part structure.

12. The mechanical part according to claim 5, wherein the cover partially covers the part structure and includes locally made apertures.

13. The mechanical part according to claim 11, wherein at least one of the at least two cover parts includes a longitudinal part made of plastic or composite translucent material.

14. The mechanical part according to claim 11, wherein at least one of the at least two cover parts includes a longitudinal part made of material providing passive noise absorption, selected from at least one of:

a mesh with an appropriate opening size,

a bristle surface of suitable density, or

a sharkskin coating.

15. Landing gear of an aircraft comprising:

at least one “

H”

shaped mechanical part according to claim 5, the mechanical part being used as a strut in the landing gear.