IP Library Granted Patent US 9,086,260
Granted Patent B2
US 9,086,260 · App. 14/362,184 · Granted Jul 21, 2015

Pyrotechnique rupture method and components for implementing it

Inventors: Thomas Kister (Vaux Sue Seine, FR); Luc Preaud (Gargenville, FR)
Assignee: ASTRIUM SAS
F42B15/36B64G1/645C06C5/04F42B15/38
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Quick Facts
Patent No.
US 9,086,260
App. No.
14/362,184
Granted
Jul 21, 2015
Kind
B2
Abstract

According to the invention, the component to be ruptured comprises an alternation of oblong pre-cut zones and of non-pre-cut zones and the pyrotechnique rupture device ( 1 ) with detonating cord ( 2 ) comprises an alternation of sections ( 1.1 ) for rupturing said non-pre-cut zones and of inflatable sections ( 1.2 ) for parting the broken parts of said component.

Claims (20)

1. Method for the pyrotechnic rupture of a securing component ( 7 ) between two elements ( 8 , 9 ), wherein the securing component:

is intended to transmit mechanical forces between said elements ( 8 , 9 ) as required, and

comprises a pyrotechnic rupture device ( 1 ) having a detonating cord ( 2 ) which is incorporated into said securing component ( 7 ) and able to break the latter along a predetermined separation plane (S.S) when said elements ( 8 , 9 ) have to be separated from one another, wherein:

oblong pre-cut zones ( 7 . 2 ) are formed in said securing component ( 7 ), along said predetermined separation plane (S.S), and spaced apart from one another so as to form an alternating sequence of such oblong pre-cut zones ( 7 . 2 ) and non-pre-cut zones ( 7 . 1 ) which transmit mechanical forces between said elements ( 8 , 9 ); and

said pyrotechnic rupture device ( 1 ) is arranged such that:

in each of said non-pre-cut zones ( 7 . 1 ) of said securing component ( 7 ), said pyrotechnic rupture device ( 1 ) comprises a section ( 1 . 1 ) in which the corresponding section ( 2 . 1 ) of the detonating cord is arranged in an expansion tube ( 3 ), and

in each of said pre-cut oblong zones ( 7 . 2 ) of said securing component ( 7 ), said pyrotechnic rupture device ( 1 ) comprises a section ( 1 . 2 ) in which the corresponding section ( 2 . 2 ) of the detonating cord is enclosed in a sealed manner in an inflatable sheath ( 5 ).

2. Method according to claim 1 , wherein, in sections ( 1 . 2 ) of the pyrotechnic rupture device ( 1 ) corresponding to said pre-cut oblong zones ( 7 . 2 ) of said securing component ( 7 ), a deflagrating cord ( 6 ) which is enclosed in a sealed manner in said inflatable sheath ( 5 ) is arranged around said section ( 2 . 2 ) of detonating cord.

3. Pyrotechnic rupture securing component for securing two elements ( 8 , 9 ) between them, wherein said component ( 7 ):

is intended to transmit mechanical forces between said elements ( 8 , 9 ) as required, and

comprises a pyrotechnic rupture device ( 1 ) which has a detonating cord ( 2 ), is incorporated into said securing component ( 7 ) and able to break the latter along a predetermined separation plane (S.S) when said elements ( 8 , 9 ) have to be separated from one another, wherein

said securing component ( 7 ) comprises, along said predetermined separation plane (S.S), an alternating sequence of oblong pre-cut zones ( 7 . 2 ) and non-pre-cut zones ( 7 . 1 ) which transmit mechanical forces between said elements ( 8 , 9 ); and

said pyrotechnic rupture device ( 1 ) comprises:

in each of said non-pre-cut zones ( 7 . 1 ), a section of detonating cord ( 2 . 1 ) arranged in an expansion tube ( 3 ), and

in each of said pre-cut oblong zones ( 7 . 2 ), a section of detonating cord ( 2 . 2 ) enclosed in a sealed manner in an inflatable sheath ( 5 ).

4. Pyrotechnic rupture securing component according to claim 3 , wherein, in said pre-cut oblong zones ( 7 . 2 ), said pyrotechnic rupture device ( 1 ) comprises a deflagrating cord ( 6 ) which is enclosed in a sealed manner in said inflatable sheath ( 5 ) and which is arranged around the corresponding section ( 2 . 2 ) of the detonating cord.

5. Pyrotechnic rupture securing component according to claim 3 , comprising two wings ( 13 , 14 ) defining between them a groove ( 16 ) in which said pyrotechnic rupture device ( 1 ) is housed, said groove ( 16 ) being closed, on the side of one ( 8 ) of said elements ( 8 , 9 ), by a bottom ( 17 ) and, on the side of the other ( 9 ) of said elements ( 8 , 9 ), by this other element ( 9 ) itself, and said wings ( 13 , 14 ) comprising, in the vicinity of said bottom ( 17 ), pre-established rupture zones ( 18 , 19 ) defining said predetermined separation plane (S.S), wherein, in said pre-cut oblong zones ( 7 , 2 ), each of said wings ( 13 , 14 ) comprises an oblong opening ( 20 , 21 ) at the level of said pre-established rupture zones ( 18 , 19 ) and of said bottom ( 17 ) of the groove ( 16 ).

6. Profile for the pyrotechnic rupture component from claim 5 , the profile comprising two wings ( 13 , 14 ) defining between them a groove ( 16 ) which, on one side, is closed by a bottom ( 17 ) and, on the other, is open, said wings ( 13 , 14 ) comprising in the vicinity of said bottom ( 17 ) pre-established rupture zones ( 18 , 19 ), wherein, each of said wings ( 13 , 14 ) comprises a sequence of spaced oblong openings ( 20 , 21 ) at the level of said pre-established rupture zones ( 18 , 19 ) and of said bottom ( 17 ) of the groove ( 16 ), and each oblong opening of one of said wings is opposite an oblong opening of the other of said wings.

7. Pyrotechnic rupture device having a detonating cord for the component according to claim 3 , comprising, alternately, sections ( 1 . 1 ) in which the detonating cord ( 2 . 1 ) is arranged in an expansion tube ( 3 ) and sections ( 1 . 2 ) in which the detonating cord ( 2 . 2 ) is enveloped, in a sealed manner, in an inflatable sheath ( 5 ).

8. Pyrotechnic rupture device according to claim 7 , wherein the sections ( 1 . 2 ) having an inflatable sheath ( 5 ) each comprise an explosive cord ( 6 ) arranged inside said inflatable sheath, around said detonating cord ( 2 . 2 ).

Assignments (4)
CHANGE OF NAME Recorded Aug 19, 2019
From: AIRBUS SAFRAN LAUNCHERS SAS
To: ARIANEGROUP SAS
Reel/Frame 050083/0723 →
CHANGE OF NAME Recorded Aug 18, 2019
From: ASTRIUM SAS
To: AIRBUS DEFENCE AND SPACE SAS
Reel/Frame 050083/0345 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 18, 2019
From: AIRBUS DEFENCE AND SPACE SAS
To: AIRBUS SAFRAN LAUNCHERS SAS
Reel/Frame 050083/0896 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 30, 2014
From: KISTER, THOMAS; PREAUD, LUC
To: ASTRIUM SAS
Reel/Frame 033425/0496 →
Priority Claims (1)
FR 11 03744 · Dec 7, 2011 · national
Continuity (1)
Related Publication 20140331851A1 · Nov 13, 2014