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Patent US4479417A successfully refreshed from Google Patents.
US4479417A
Expired / Lapsed
US
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Missile launcher module in particular for aircraft, with general reversible safety device
Assignee: E LACROIX Ste
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Filing: 1982-06-01
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Granted: 1984-10-30
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Expires: 2002-06-01
Abstract
Abstract A standard launcher module for various missiles, in particular flares, comprises a flat wall forming a base, provided with male engagement members. In the position engaged on the support incorporated in the aircraft, a connector is active. Provided in a central groove is a series of electrical initiators connected selectively to the connector and located opposite counterpart relay channels which lead respectively to the useful charges. A sliding bar located in the groove has orifices, located according to the working geometry of the initiators. Finally, a motor connected to the connector allows the movement of the bar between a safety position and an armed position.
Inventors
- 👤 Alain A. Billard
- 👤 Andr/e/ R. Santalucia
- 👤 Roland C. Encoyand
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 15:37
CPC Classifications
B; B64; B64D; B64D1/00; B64D1/02; B64D1/04; B64D1/06; F; F42; F42C; F42C15/00; F42C15/34; F42C15/40
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
171 words
A missile launcher module carried by an aircraft comprising: a flat wall forming a base provided with male engagement members which cooperate with counterpart female engagement members of a support rod fixed to the aircraft and an electrical connector establishing a connection between the module and the carrying aircraft in the engaged position of the module, said flat wall forming the base of the module defining a central groove, a series of electrical initiators housed within the groove and selectively connected to said electrical connector, the initiators being located opposite counterpart fire-transmission channels formed in the flat base wall in order to terminate respectively at useful charges contained in the module, the central groove also supporting a slide bar having orifices located according to the working geometry of the initiators, and an electrical motor electrically connected to the connector for energization and mechanically connected to the base in order to ensure movement of the bar between a safe position and an armed position in which the orifices are opposite the initiators.
Claim 2
Dependent Claim
171 words
A missile launcher module carried by an aircraft comprising: a flat wall forming a base provided with male engagement members which cooperate with counterpart female engagement members of a support rod fixed to the aircraft and an electrical connector establishing a connection between the module and the carrying aircraft in the engaged position of the module, said flat wall forming the base of the module defining a central groove, a series of electrical initiators housed within the groove and selectively connected to said electrical connector, the initiators being located opposite counterpart fire-transmission channels formed in the flat base wall in order to terminate respectively at useful charges contained in the module, the central groove also supporting a slide bar having orifices located according to the working geometry of the initiators, and an electrical motor electrically connected to the connector for energization and mechanically connected to the base in order to ensure movement of the bar between a safe position and an armed position in which the orifices are opposite the initiators.
Claim 3
Dependent Claim
19 words
Module according to claim 1, characterised by the fact that the bar is an aluminium sectional member of general/U-shape.
Claim 4
Dependent Claim
35 words
Module according to one of claims 1 and 2, characterised by the fact that the module also comprise two micro-contacts connected to the connector, in order to detect the safety position and the armed position.
Claim 5
Dependent Claim
35 words
Module according to claim 1, characterised by the fact that a device forming clips is provided, which is capable of keeping the bar in a safety position or armed position with a high retaining force.
Claim 6
Dependent Claim
17 words
Module according to claim 1, characterised by the fact that the electric motor comprises a cobalt/samarium magnet.
Claim 7
Dependent Claim
36 words
Module according to claim 3, characterised by the fact that the micro-contacts cooperate with notches provided laterally in the bar and offset overall with respect to the micro-contacts by the distance by which the bar moves.
References Cited (Backward Citations)
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Cited
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Cited
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Cited
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Cited
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1987-10-30 | 1988-04-30 | 1988-10-30 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1991-10-30 | 1992-04-30 | 1992-10-30 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1995-10-30 | 1996-04-30 | 1996-10-30 | $7700.00 | Window Closed / Lapsed |