IP Library Patent Application 10994285
Patent Application
App. No. 10/994,285

Assembly comprising two metallic parts protected against the formation of a galvanic couple

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Quick Facts
Patent No.
US None
App. No.
10/994,285
Abstract

The invention relates to an assembly ( 1 ) comprising a first metallic part ( 2 ) and a second metallic part ( 4 ) assembled together and made from different materials, the first and second parts being provided with a first contact surface and a second contact surface ( 2 a, 4 a ) respectively in contact with each other, at least one of the contact surfaces being provided with a protective coating ( 12,14 ) capable of preventing the metallic parts from forming a galvanic couple. According to the invention, at least one protective coating comprises a coat of paint ( 12 a, 14 a ) containing a filler of particles conducting electricity. To be applied to the domain of fluid conveyance systems onboard an aircraft.

Claims (10)

1 . Assembly ( 1 , 100 ) comprising a first metallic part ( 2 , 102 ) and a second metallic part ( 4 , 104 ) assembled together and made from different materials, the first and second parts ( 2 , 4 , 102 , 104 ) being provided with a first contact surface ( 2 a ) and a second contact surface ( 4 a ) respectively, in contact with each other, at least one of said first and second contact surfaces ( 2 a , 4 a ) being provided with a protective coating ( 12 , 14 ) capable of preventing said first and second metallic parts ( 2 , 4 , 102 , 104 ) from forming a galvanic couple, characterised in that at least one protective coating ( 12 , 14 ) comprises a paint coat ( 12 a , 14 a ) containing a filler of particles conducting electricity.

2 . Assembly ( 1 , 100 ) according to claim 1 , characterised in that each protective coating ( 12 , 14 ) is composed exclusively of one coat of paint ( 12 a , 14 a ) containing a filler of particles conducting electricity.

3 . Assembly ( 1 , 100 ) according to claim 1 or claim 2 , characterised in that the first metallic part ( 2 , 102 ) is made from carbon steel and the second metallic part ( 4 , 104 ) is made from an aluminum alloy, and in that only the first contact surface ( 2 a ) is coated with a protective coating.

4 . Assembly ( 1 , 100 ) according to claim 1 or claim 2 , characterised in that the first metallic part ( 2 , 102 ) is made from stainless steel and the second metallic part ( 4 , 104 ) is made from an aluminum alloy, and in that only the second contact surface ( 4 a ) is coated with a protective coating.

5 . Assembly ( 1 , 100 ) according to any one of the previous claims, characterised in that for each coat of paint ( 12 a , 14 a ) containing a filler of particles conducting electricity, said particles are carbon and/or metal particles.

6 . Assembly ( 100 ) according to any one of the previous claims, characterised in that said first part ( 102 ) is a fluid conveyance tube fitting, and in that said second part ( 104 ) is a fluid conveyance tube.

7 . Assembly ( 1 , 100 ) according to any one of the previous claims, characterised in that it comprises more than two metallic parts in contact.

8 . Aircraft comprising at least one assembly ( 1 , 100 ) according to any one of the previous claims.

9 . Method for manufacturing an assembly ( 1 , 100 ) comprising a first metallic part ( 2 , 102 ) and a second metallic part ( 4 , 104 ) assembled together and made from different materials, the first and second parts ( 2 , 4 , 102 , 104 ) being provided with a first contact surface ( 2 a ) and a second contact surface ( 4 a ) bearing on each other, said method comprising a step to protect said metallic parts ( 2 , 4 , 102 , 104 ) consisting of forming a protective coating ( 12 , 14 ) on at least the first or the second contact surface ( 2 a , 4 a ), each protective coating ( 12 , 14 ) being capable of preventing the first and second metallic parts ( 2 , 4 , 102 , 104 ) from cooperating to form a galvanic couple, characterised in that at least one protective coating ( 12 , 14 ) is formed so as to include a coat of paint ( 12 a , 14 a ) containing a filler of particles conducting electricity.

10 . Use of a paint containing a filler of particles conducting electricity to form a protective coating ( 12 , 14 ) capable of preventing a first metallic part ( 2 , 102 ) and a second metallic part ( 4 , 104 ) from forming a galvanic couple, these parts being in contact and assembled together, and being made from different materials.

Assignments (2)
MERGER Recorded May 18, 2011
From: AIRBUS FRANCE
To: AIRBUS OPERATIONS SAS
Reel/Frame 026298/0269 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Feb 22, 2005
From: DONNADIEU, ANDRE
To: AIRBUS FRANCE
Reel/Frame 016282/0299 →