Pyrotechnic device

US11359545B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11359545-B2
Application numberUS-201716461944-A
CountryUS
Kind codeB2
Filing dateNov 17, 2017
Priority dateNov 18, 2016
Publication dateJun 14, 2022
Grant dateJun 14, 2022

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A pyrotechnic device comprising a main pyrotechnic charge, a firing device for firing the main pyrotechnic charge, a discharge passage for discharging the gas generated by firing the main pyrotechnic charge, and an injector device configured to inject a cooling fluid into said gas discharge passage, so as to deliver gas, specifically for driving turbines, at temperatures that are relatively low, and a method of cooling gas generated by firing the main pyrotechnic charge by injecting the cooling fluid.

First claim

Opening claim text (preview).

The invention claimed is: 1. A pyrotechnic device comprising a main pyrotechnic charge, a firing device for firing the main pyrotechnic charge, a discharge passage for discharging the gas generated by firing the main pyrotechnic charge, wherein the gas is discharged from the discharge passage to a turbine of a turbomachine, a tank containing a cooling fluid, in communication with the discharge passage, a pressurizing device comprising an auxiliary pyrotechnic charge in communication with the tank for pressurizing the tank solely with gas generated by firing the auxiliary pyrotechnic charge, and an injector device configured to inject the cooling fluid into said gas discharge passage; wherein the firing device for the main pyrotechnic charge and the auxiliary pyrotechnic charge are communicably coupled to a control unit, wherein the control unit is configured to fire the auxiliary pyrotechnic charge before the main pyrotechnic charge, and wherein the auxiliary pyrotechnic charge is dimensioned so as to spread out the injection of the cooling fluid over a duration that is longer than that for which the gas generated by firing the main pyrotechnic charge is discharged. 2. The pyrotechnic device according to claim 1 , wherein said cooling fluid is aqueous. 3. The pyrotechnic device according to claim 2 , wherein said cooling fluid also contains an antifreeze. 4. The pyrotechnic device according to claim 3 , wherein said antifreeze is methanol, ethylene glycol, propylene glycol, or glycerol. 5. The pyrotechnic device according to claim 2 , wherein the injector device comprises an ejector installed in said discharge passage. 6. The pyrotechnic device according to claim 1 , wherein the pressurizing device comprises a piston in said tank. 7. The pyrotechnic device according to claim 6 , wherein the injector device further includes a plug interposed between said tank and the discharge passage. 8. The pyrotechnic device according to claim 6 , wherein the injector device comprises an ejector installed in said discharge passage. 9. The pyrotechnic device according to claim 6 , wherein the injector device comprises an ejector installed in said discharge passage. 10. The pyrotechnic device according to claim 6 , further comprising a plug installed in said discharge passage. 11. The pyrotechnic device according to claim 1 , wherein the injector device further includes a plug interposed between said tank and the discharge passage. 12. The pyrotechnic device according to claim 11 , wherein the injector device comprises an ejector installed in said discharge passage. 13. The pyrotechnic device according to claim 11 , further comprising a plug installed in said discharge passage. 14. The pyrotechnic device according to claim 1 , wherein the injector device comprises an ejector installed in said discharge passage. 15. The pyrotechnic device according to claim 1 , further comprising a plug installed in said discharge passage. 16. A turbomachine including the turbine and the pyrotechnic device according to claim 1 , wherein the discharge passage is connected to an inlet passage of the turbine. 17. The pyrotechnic device according to claim 1 , wherein said pyrotechnic charge and auxiliary pyrotechnic charge are both solid pyrotechnic charges. 18. The pyrotechnic device according to claim 1 , wherein the pressurizing device comprises a diaphragm in said tank. 19. A method of cooling gas generated by firing a main pyrotechnic charge of a pyrotechnic device, wherein a cooling fluid is pressurized solely by gas generated by firing an auxiliary pyrotechnic charge, and injected by an injector device into a discharge passage in which the gas generated by firing the main pyrotechnic charge flows, wherein the gas is discharged from the discharge passage to a turbine of a turbomachine, wherein a firing device for the main pyrotechnic charge, and the auxiliary pyrotechnic charge, are communicably coupled to a control unit, wherein the control unit fires the auxiliary pyrotechnic charge before the main pyrotechnic charge, and wherein the injection of the cooling fluid is spread out over a duration that is longer than that for which the gas generated by firing the main pyrotechnic charge is discharged. 20. The pyrotechnic device according to claim 19 , wherein said pyrotechnic charge and auxiliary pyrotechnic charge are both solid pyrotechnic charges.

Assignees

Inventors

Classifications

  • F02C7/272Primary

    generated by cartridges · CPC title

  • using an ejector or a jet pump · CPC title

  • Control · CPC title

  • F02C7/141Primary

    of working fluid · CPC title

  • characterised by cooling medium · CPC title

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Frequently asked questions

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What does patent US11359545B2 cover?
A pyrotechnic device comprising a main pyrotechnic charge, a firing device for firing the main pyrotechnic charge, a discharge passage for discharging the gas generated by firing the main pyrotechnic charge, and an injector device configured to inject a cooling fluid into said gas discharge passage, so as to deliver gas, specifically for driving turbines, at temperatures that are relatively low…
Who is the assignee on this patent?
Safran Helicopter Engines
What technology area does this patent fall under?
Primary CPC classification F02C7/272. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jun 14 2022 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).