IP Library Granted Patent US 10,239,601
Granted Patent B2
US 10,239,601 · App. 15/556,300 · Granted Mar 26, 2019

Method and device for fireproofing a part in composite material

Inventors: Fabrice Landais (Romain sur Cher, FR); Dominique Soubelet (Amboise, FR)
Assignee: DAHER AEROSPACE
B64C1/40A62C3/08A62C2/06B64C2001/0072B64D2045/009Y02T50/43
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Quick Facts
Patent No.
US 10,239,601
App. No.
15/556,300
Granted
Mar 26, 2019
Kind
B2
Abstract

A device for fireproofing a section of a structural part made of composite material. The device includes a skin having an outer surface configured to face the flame and an inner surface. The skin is made of composite material that includes fibrous reinforcement in a polymer matrix. The skin includes a fastener to fasten the part to the structure. The device includes a layer of needled mineral felt placed between the inner surface of the skin and a surface of the structural part.

Claims (12)

1. A method to fireproof a section of a structural part made of composite material using a device comprising:

a skin comprising an outer surface configured to face a flame and an inner surface, the skin is made of composite material that comprises fibrous reinforcement in a polymer matrix comprising a ply made of glass fabric on the inner surface of the skin and comprises a fastener to fasten the skin to the structural part; and

a layer of needled fire retardant felt placed between the inner surface of the skin and a surface of the structural part:

the method comprising the steps of:

(i) laying up a ply of non-impregnated glass on a tool corresponding to a shape of a section of the structural part, offset by a thickness of the fire retardant felt, wherein the ply of non-impregnated glass forms the inner surface of the skin;

(ii) laying up a ply of pre-impregnated glass on the ply of non-impregnated glass to form a laminate;

(iii) curing the laminate so as to form the skin;

(iv) placing a thickness of fire retardant felt on the inner surface of the skin;

(v) fixing the skin to a corresponding section of the structural part; and

repeating steps (i) to (v) for each section of the structural part until the structural part is covered.

2. The method according to claim 1 , wherein step (v) of fixing the skin comprises a riveting operation which comprise applying thermal protection of an ablative or intumescent type on rivet heads.

3. The method according to claim 1 , wherein the fire retardant felt is 10 mm thick.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 8, 2018
From: LANDAIS, FABRICE; SOUBELET, DOMINIQUE
To: DAHER AEROSPACE
Reel/Frame 046590/0181 →
Priority Claims (1)
FR 15 52080 · Mar 16, 2015 · national
Continuity (1)
Related Publication 20180043983A1 · Feb 15, 2018
Cited By (1)
US 12,441,454