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公开(公告)号:FR2630202B1
公开(公告)日:1990-08-17
申请号:FR8804951
申请日:1988-04-14
Applicant: AEROSPATIALE
Inventor: MAREE MICHEL
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公开(公告)号:FR2584323A1
公开(公告)日:1987-01-09
申请号:FR8510221
申请日:1985-07-04
Applicant: AEROSPATIALE
Inventor: SABATIE MICHELE , MAREE MICHEL
Abstract: The present invention relates to castings constituted by a metal matrix reinforced by fibers and having outgrowths. Firstly a reinforcing framework is produced, which is incorporated into the fibrous strengthening member, the complete entity being placed in a mould and the metal matrix is cast. The latter penetrates the fibrous strengthening member and the reinforcing framework. The latter is positioned at the location of an outgrowth which, after solidification of the metal matrix, is consequently reinforced. Application to the production of castings having fixing tabs or lobes.
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公开(公告)号:DE69009618T2
公开(公告)日:1994-12-22
申请号:DE69009618
申请日:1990-08-03
Applicant: AEROSPATIALE
Inventor: COMON JEAN PAUL , MAREE MICHEL
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公开(公告)号:ES2056411T3
公开(公告)日:1994-10-01
申请号:ES90402227
申请日:1990-08-03
Applicant: AEROSPATIALE
Inventor: COMON JEAN PAUL , MAREE MICHEL
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公开(公告)号:DE69009618D1
公开(公告)日:1994-07-14
申请号:DE69009618
申请日:1990-08-03
Applicant: AEROSPATIALE
Inventor: COMON JEAN PAUL , MAREE MICHEL
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公开(公告)号:DE68907257D1
公开(公告)日:1993-07-29
申请号:DE68907257
申请日:1989-04-12
Applicant: AEROSPATIALE
Inventor: MAREE MICHEL
IPC: F42B15/04
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公开(公告)号:FR2578665B1
公开(公告)日:1988-02-12
申请号:FR8111088
申请日:1981-06-04
Applicant: AEROSPATIALE
Inventor: GUILLOT JEAN , MAREE MICHEL , RAYNAUD JACQUES , VAILLANT ROBERT , ANSALDI JEAN
IPC: F02K9/80 , G05D1/10 , B64C15/02 , F42B15/033 , F42B15/24
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公开(公告)号:DE68907257T2
公开(公告)日:1993-12-16
申请号:DE68907257
申请日:1989-04-12
Applicant: AEROSPATIALE
Inventor: MAREE MICHEL
IPC: F42B15/04
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公开(公告)号:DE69001699T2
公开(公告)日:1993-11-18
申请号:DE69001699
申请日:1990-03-20
Applicant: AEROSPATIALE
Inventor: MAREE MICHEL , MOREAU PATRICK
Abstract: The bobbin according to the invention has normal dimensions, but contains a long length of optical fibre. It consists of a main cylindrical support (12) around which is wound a first part (18) of the optical fibre (16) which is intended to be unwound by traction. It consists of a first additional cylindrical support (14) which is concentric to and placed inside the main cylindrical support (12), a second part (20) of the optical fibre (16) being wound around this first additional support (14), the inner layer of the first part (18) of the optical fibre (16) being directly connected to an outer layer of the second part (20) of the optical fibre (16). Application to very long range missiles.
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公开(公告)号:AT91015T
公开(公告)日:1993-07-15
申请号:AT89401005
申请日:1989-04-12
Applicant: AEROSPATIALE
Inventor: MAREE MICHEL
IPC: F42B15/04
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