US 5,473,897 AGranted

Internal combustion engine with exhaust-gas turbocharging

AssigneeABB Management AG

InventorPeter Elvekjaer

Life of this patent

Estimating the term…

Loading patent…

Abstract

The object of the invention is to create an internal combustion engine, connected to two exhaust-gas turbochargers, with reduced flow losses and an improved efficiency which is particularly suitable for relatively high boosting. According to the invention this is achieved by virtue of the fact that in an apparatus in accordance with the preamble of claim 1, the two exhaust-gas turbochargers (1,1') are arranged offset sideways relative to one another. The diffuser outlets (5,5') of the radial turbines (2,2') are arranged point-symmetrically with respect to the center (8) of the central wall (6). The lateral spacing of the axes (9,9') of the radial turbines (2,2') from the wall (10,10') of the turbine outflow casing (3) on the outflow side (11,11') of the radial turbines (2,2') is designed so as to be greater than their lateral spacing from the other wall (12,12') in each case.

Claims4

Dependent claims

An internal combustion engine with exhaust-gas turbocharging, in which

a) two exhaust-gas turbochargers of identical construction, each having a radial compressor and a radial turbine and being arranged in a common horizontal plane and opposite one another in the direction of flow, have a common turbine outflow casing into which the outflowing exhaust gas from the radial turbines is introduced,
b) the two radial turbines each have an exhaust diffuser, the diffuser outlet of which projects into the turbine outflow casing and
c) a central wall which separates the two exhaust-gas flows from one another before they are carried away via a flue arranged centrally on the turbine outflow casing,
wherein
d) the two exhaust-gas turbochargers are arranged offset sideways relative to one another,
e) the lateral spacing of the axes of the exhaust-gas turbochargers from the wall of the turbine outflow casing on the outflow side of the radial turbines is designed so as to be greater than their lateral spacing from the respectively opposite wall and
f) the diffuser outlets of the radial turbines are arranged point-symmetrically with respect to the center of the central wall.

4 more elements

Dependencies are inferred from the claim text.