En gassgenerator og en turbojet utstyrt med en slik generator til starting

The generator has an annular case (11) forming a chamber for a pyrotechnic load (12) and composed of unitary load segments (120). The segments have an external dimension lower than the chamber so that passages constituting circulation paths for gas products during combustion of the load are arranged...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	Fischer, Roger, Soulie, Laurent
Format:	Patent
Sprache:	nor
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS AMMUNITION BLASTING CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION GAS-TURBINE PLANTS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE WEAPONS
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Beschreibung
Zusammenfassung:	The generator has an annular case (11) forming a chamber for a pyrotechnic load (12) and composed of unitary load segments (120). The segments have an external dimension lower than the chamber so that passages constituting circulation paths for gas products during combustion of the load are arranged between segments and the case. Vents or exhaust ports (111) are arranged on the case for ejecting the products during combustion. An independent claim is also included for a jet engine comprising a gas generator.