IP Library Granted Patent US 8,864,141
Granted Patent B2
US 8,864,141 · App. 12/349,116 · Granted Oct 21, 2014

Blade seal

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Quick Facts
Patent No.
US 8,864,141
App. No.
12/349,116
Granted
Oct 21, 2014
Kind
B2
Abstract

A blade seal comprising: a base; a tip; a first part formed from an elastomeric material which extends continuously from the base to the tip; and a second part formed from an elastomeric material mixed with conductive filler which extends continuously from the base to the tip. The blade seal is manufactured by compressing the first and second parts together; and curing one or both of the parts as they are compressed together.

Claims (23)

1. A blade seal comprising:

a base;

a tip;

a first part formed from a non-conductive material, wherein said non-conductive material is elastomeric which extends continuously from the base to the tip;

a second part formed from a conductive material, wherein said conductive material is elastomeric mixed with conductive filler which extends continuously from the base to the tip;

wherein a path of highest conductivity across the sealing member is provided by the conductive filler within the second part and not the first part; and,

wherein the first part is arranged to engage a component at the tip of the blade seal to form an environmental seal with the component, and the second part is arranged to engage the component at the tip of the blade seal to form an electrical connection with the component.

2. The blade seal of claim 1 wherein the filler comprises silver or carbon.

3. The blade seal of claim 1 wherein the second part comprises a projection for forming the electrical connection with the component.

4. The blade seal of claim 1 wherein the first and second parts are formed from different elastomeric materials.

5. The blade seal of claim 4 wherein the elastomeric material forming the first part has a higher degree of fuel resistance than the elastomeric material forming the second part.

6. The blade seal of claim 1 wherein the first part provides an external surface on a first side of the blade seal; and the second part provides an external surface on a second side of the blade seal.

7. The blade seal of claim 1 wherein the first and second parts are bonded together.

8. A joint comprising first and second components; and the blade seal of claim 1 with the base of the blade seal attached to the first component and the tip of the blade seal forming a seal with the second component, wherein the first part of the blade seal engages the second component at the tip of the blade seal to form an environmental seal with the second component and the second part of the blade seal engages the second component at the tip of the blade seal to form an electrical connection with the second component.

9. An aircraft comprising the joint of claim 8 .

10. A blade seal comprising:

a base;

a tip;

a first part formed from a non-conductive material, wherein said non-conductive material is an elastomeric material which extends continuously from the base to the tip;

a second part formed from a conductive material, wherein said conductive material is elastomeric mixed with conductive filler which extends continuously from the base to the tip;

wherein the first part as a whole is less conductive than the second part as a whole; and,

wherein the first part is arranged to engage a component at the tip of the blade seal to form an environmental seal with the component, and the second part is arranged to engage the component at the tip of the blade seal to form an electrical connection with the component.

11. A joint comprising first and second components; and the blade seal of claim 10 with the base of the blade seal attached to the first component and the tip of the blade seal forming a seal with the second component, wherein the first part of the blade seal engages the second component at the tip of the blade seal to form an environmental seal with the second component and the second part of the blade seal engages the second component at the tip of the blade seal to form an electrical connection with the second component.

Assignments (2)
CHANGE OF NAME Recorded Apr 18, 2011
From: AIRBUS UK LIMITED
To: AIRBUS OPERATIONS LIMITED
Reel/Frame 026141/0311 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 6, 2009
From: WEST, COLIN JOHN; SUTTON, DAVID ALISTAIR
To: AIRBUS UK LIMITED
Reel/Frame 022064/0265 →