FR3050815B1 - IGNITION SYSTEM AND ASSOCIATED MECHANICAL DRIVE DEVICE - Google Patents
IGNITION SYSTEM AND ASSOCIATED MECHANICAL DRIVE DEVICE Download PDFInfo
- Publication number
- FR3050815B1 FR3050815B1 FR1653790A FR1653790A FR3050815B1 FR 3050815 B1 FR3050815 B1 FR 3050815B1 FR 1653790 A FR1653790 A FR 1653790A FR 1653790 A FR1653790 A FR 1653790A FR 3050815 B1 FR3050815 B1 FR 3050815B1
- Authority
- FR
- France
- Prior art keywords
- optical signal
- state
- optical
- arming
- line
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 230000003287 optical effect Effects 0.000 abstract 8
- 239000007787 solid Substances 0.000 abstract 2
- 238000010304 firing Methods 0.000 abstract 1
- 230000000977 initiatory effect Effects 0.000 abstract 1
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B3/00—Blasting cartridges, i.e. case and explosive
- F42B3/10—Initiators therefor
- F42B3/113—Initiators therefor activated by optical means, e.g. laser, flashlight
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
- F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
- F02C7/27—Fluid drives
- F02C7/272—Fluid drives generated by cartridges
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
- F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
- F02C7/275—Mechanical drives
- F02C7/277—Mechanical drives the starter being a separate turbine
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/99—Ignition, e.g. ignition by warming up of fuel or oxidizer in a resonant acoustic cavity
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Air Bags (AREA)
- Lasers (AREA)
Abstract
L'invention concerne un système d'allumage d'une charge solide d'un générateur de gaz. Le système d'allumage est caractérisé en ce qu'il comprend un dispositif (124) de pilotage, une diode (130) laser adaptée pour émettre un signal optique en cas de réception d'un ordre de mise à feu, une ligne (140) optique adaptée pour transmettre le signal optique, un dispositif (136) d'armement adapté pour présenter un premier état, dit état désarmé, dans lequel le dispositif (136) d'armement empêche la propagation du signal optique dans la ligne (140) optique, et un deuxième état, dit état armé, dans lequel le dispositif (136) d'armement permet la propagation du signal optique dans la ligne (140) optique, l'état armé étant activé qu'en cas de réception d'un ordre d'armement, et un dispositif (128) d'initiation pyrotechnique comprenant une composition (134) pyrotechnique secondaire, adaptée pour être initiée par ledit signal optique et pour allumer la charge solide du générateur (12) de gaz.The invention relates to a system for igniting a solid charge of a gas generator. The ignition system is characterized in that it comprises a control device (124), a laser diode (130) adapted to emit an optical signal when a firing command is received, a line (140) ) optical adapted to transmit the optical signal, an arming device (136) adapted to present a first state, said disarmed state, wherein the arming device (136) prevents the propagation of the optical signal in the line (140) optical, and a second state, said armed state, wherein the arming device (136) allows the propagation of the optical signal in the optical line (140), the armed state being activated in the event of reception of a arming order, and a pyrotechnic initiation device (128) comprising a secondary pyrotechnic composition (134) adapted to be initiated by said optical signal and to ignite the solid charge of the gas generator (12).
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1653790A FR3050815B1 (en) | 2016-04-28 | 2016-04-28 | IGNITION SYSTEM AND ASSOCIATED MECHANICAL DRIVE DEVICE |
PCT/FR2017/050975 WO2017187079A1 (en) | 2016-04-28 | 2017-04-24 | Mechanical drive device comprising an ignition system |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1653790 | 2016-04-28 | ||
FR1653790A FR3050815B1 (en) | 2016-04-28 | 2016-04-28 | IGNITION SYSTEM AND ASSOCIATED MECHANICAL DRIVE DEVICE |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3050815A1 FR3050815A1 (en) | 2017-11-03 |
FR3050815B1 true FR3050815B1 (en) | 2019-05-24 |
Family
ID=57590555
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1653790A Active FR3050815B1 (en) | 2016-04-28 | 2016-04-28 | IGNITION SYSTEM AND ASSOCIATED MECHANICAL DRIVE DEVICE |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR3050815B1 (en) |
WO (1) | WO2017187079A1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2020160579A1 (en) * | 2019-01-28 | 2020-08-06 | Detnet South Africa (Pty) Ltd | Light sensitive arrangement for a detonator |
US11859554B2 (en) * | 2021-07-29 | 2024-01-02 | Pratt & Whitney Canada Corp. | Fast engine re-start for multi-engine system and method |
FR3127286B1 (en) * | 2021-09-17 | 2023-08-11 | Safran Aircraft Engines | Triggering by laser of an electrical or electronic device located in the rotating part of a rotating machine |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5729012A (en) * | 1995-04-25 | 1998-03-17 | Lockheed Martin Corporation | Photoluminescence built-in-test for optical systems |
US8750340B1 (en) * | 2010-07-28 | 2014-06-10 | Intuitive Research And Technology Corporation | Laser ordnance safe-arm distributor |
FR3010740B1 (en) * | 2013-09-19 | 2018-03-02 | Snecma | SYSTEM AND METHOD FOR EMERGENCY STARTING AN AIRCRAFT TURBOMACHINE |
FR3019524B1 (en) * | 2014-04-03 | 2017-12-08 | Turbomeca | HELICOPTER ENGINE CHAIN INCORPORATING A PYROTECHNIC ENGINE ASSISTANCE MODULE AND HELICOPTER COMPRISING THE SAME |
FR3019588B1 (en) * | 2014-04-08 | 2019-06-14 | Safran Helicopter Engines | DEVICE FOR ASSISTING A SOLID PROPERGOL PROPULSIVE SYSTEM OF A MONOMOTING HELICOPTER, MONOMOTOR HELICOPTER COMPRISING SUCH DEVICE AND CORRESPONDING METHOD |
-
2016
- 2016-04-28 FR FR1653790A patent/FR3050815B1/en active Active
-
2017
- 2017-04-24 WO PCT/FR2017/050975 patent/WO2017187079A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
FR3050815A1 (en) | 2017-11-03 |
WO2017187079A1 (en) | 2017-11-02 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20171103 |
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PLFP | Fee payment |
Year of fee payment: 3 |
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CD | Change of name or company name |
Owner name: SAFRAN HELICOPTER ENGINES, FR Effective date: 20180717 Owner name: SAFRAN CERAMICS, FR Effective date: 20180717 |
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PLFP | Fee payment |
Year of fee payment: 5 |
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PLFP | Fee payment |
Year of fee payment: 6 |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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PLFP | Fee payment |
Year of fee payment: 9 |