FLEXIBLE SEAL FOR AN AIRCRAFT

• US 20180236858A1
• Filed: 02/19/2018
• Published: 08/23/2018
• Est. Priority Date: 02/22/2017
• Status: Abandoned Application

• Current Assignee: Airbus Operations SAS (Airbus SE)
• Original Assignee: Airbus Operations SAS (Airbus SE)
• Inventors: LUNN, Thomas
• Application Number:
  US15/899,082
• Publication Number:
  US 20180236858A1
• Time in Patent Office: Days
• CPC Class Codes: B60J 10/22 having varying cross-section in the longitudinal direction
• CPC Class Codes: B60J 10/88 mounted on, or integral with, the glass-run seals
• CPC Class Codes: B64C 9/02 Mounting or supporting thereof
• CPC Class Codes: B64C 9/18 by single flaps
• CPC Class Codes: F16J 15/027 and with a hollow profile

Abstract

A flexible seal intended to be fixed between a fixed part and a mobile part of an aircraft, the seal comprising an elongate hollow body, a shoe secured to the hollow body, intended to be fixed to the fixed part, a blade secured to the hollow body and designed to extend from the hollow body towards the mobile part, the blade having a leak edge having a non-linear edge, such as with notches or chevrons. The provision of a notched leak edge reduces a pressure differential on either side of the blade, and by allowing the air to pass between the blade and the fixed part just before the contact with the fixed part, the lifting of the blade is prevented.

Claims

1. A flexible seal intended to be fixed between a fixed part and a mobile part of an aircraft, the seal comprising:

an elongate hollow body,

a shoe secured to the hollow body and configured to be fixed to the fixed part,

a blade secured to the hollow body and configured to extend from the hollow body towards the mobile part, the blade having a non-linear leak edge.

2. The flexible seal according to claim 1, wherein the leak edge has notches or chevrons.

3. The flexible seal according to claim 2, wherein the notches are distributed evenly along the leak edge.

4. The flexible seal according to claim 2, wherein the notches take the form of circular arc undulations.

5. The flexible seal according to claim 1, wherein the blade comprises an insert which extends over a full length of the blade.

6. An aircraft comprising:

a fixed part,

a mobile part next to the fixed part, and

a seal according to claim 1,

the shoe being fixed to the fixed part and the blade extending from the hollow body towards the mobile part.

7. The aircraft according to claim 6, wherein the fixed part is a wing and wherein the mobile part is a flap.