#F02K7/02

A ROCKET ENGINE WITH MULTI-STAGE COMBUSTION OF A MIXTURE OF PROPELLANTS

The invention relates to a rocket engine with the multi-stage combustion of a mixture of propellants, having at least one pre-combustion chamber and a main combustion chamber, a propellant mixture sup…

DRIVE·Feb 26·2 min read

F02K7/02 SIEC BADAWCZA LUKASIEWICZ INST LOTNICTWA [PL]

Pulse detonation tube with local flexural wave modifying feature

In one embodiment, a pulse detonation tube (10) includes a continuous base tube (12) having a substantially uniform wall thickness (56). The pulse detonation tube (10) also includes a local flexural w…

DRIVE·Apr 4·1 min read

F02K7/02 GEN ELECTRIC [US]

Rotary pulse detonation system for a gas turbine engine

A pulse detonation system for a gas turbine includes a rotatable cylindrical member (42) having a forward surface (44), an aft surface (46), and an outer circumferential surface, where at least one st…

DRIVE·Sep 21·2 min read

F02K7/02 GEN ELECTRIC [US]

Detonation chamber

A shock wave reflector (10) includes a number of reflective units (1) positioned along a longitudinal direction (2) and separated by a gap G. Each reflective unit has a length L. The length L and the …

DRIVE·Oct 8·1 min read

F02K7/02 GEN ELECTRIC [US]