パルス駆動装置

Japanese Patent JP7268934

B2

A device serves for the repeated generation of explosions, in particular for the drive of an aircraft. It comprises: ▪a combustion chamber (21), ▪at least one feed line for feeding a flowable, explosive material or components which form an explosive material upon mixing to the combustion chamber (21); ▪a discharge device for the targeted discharge of a gas pressure which is generated by way of ignition of the explosive material in the combustion chamber (21), ▪a movable nozzle regulating element (26) for the partial or complete closure of the discharge device, ▪an actuating element (25) which is configured to open the discharge device further after opening of the discharge device and during an outflow of explosion gases by way of the discharge device. Here, the discharge device has a plurality of part nozzles (40) for the discharge of the gas pressure, and a position of the part nozzles (40) can be set by way of the actuating element (25).

WO/1998/014694	ENGINE WORKING ACCORDING TO THE METHOD OF PULSATING COMBUSTION
JP5276163	Pulse detonation engine
JP3981743	Steady detonation combustor and steady detonation wave generation method

ruegg, hans
peterhans, thomas
Sutter, Manuel

JP2020520771A

May 08, 2023

November 05, 2018

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P-Wave AG

F02K7/06; B64D27/02; F02C5/06; F02C5/12; F23R7/00

JP11294714A
JP2001355515A
JP2011185268A
JP2012502242A
JP2015524893A
JP2011185133A

US1980266
US3914935
US6477829
US20170082069
CN2856447Y

Ikeda Adult
Junichiro Sakamaki
Masakazu Noda

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