| 摘要 |
#CMT# #/CMT# The arrangement has a rotary cell impeller (2) axially and pivotably supported in a stator (1) by a cell impeller hollow shaft (4), such that the cell impeller covers concentric combustion chambers (3) with cells. The concentric combustion chambers are arranged in the stator. Injection nozzles (5) are arranged in the combustion chambers for injection of liquid or gaseous fuel. Ignition assemblies (7) are arranged in the combustion chambers. A circulating annular edge of the cell impeller is formed as a rotary slide and engaged in a combustion chamber level of the stator. #CMT# : #/CMT# An independent claim is also included for a method for exploded-like ignition of liquid or gaseous fuels in concentric combustion chambers arranged on a stator. #CMT#USE : #/CMT# Arrangement of a core current power train for driving of an aircraft by a gaseous fuel. #CMT#ADVANTAGE : #/CMT# The arrangement provides an impulse turbine, which operates without a valve gear and a complex system of turbine sheets. A compact design configuration of the cell impeller provides a long service life to the arrangement and enables an effective supply of a high torque at low rotational speeds. #CMT#DESCRIPTION OF DRAWINGS : #/CMT# The drawing shows a schematic view of a core stream power train in a radial section and an arrangement for supply of load air, fuel injection and ignition. 1 : Stator 2 : Rotary cell impeller 3 : Concentric combustion chambers 4 : Cell impeller hollow shaft 5 : Injection nozzles 7 : Ignition assemblies. |
