Reciprocating piston internal combustion engine

Claim 2

A piston internal combustion engine, comprising several exhaust gas turbocharger means, of which at least one is adapted to be disengaged during partial load operation of the internal combustion engine, an exhaust gas line and a suction line for each exhaust gas turbocharger means adapted to be disengaged, closure means in each of the exhaust gas line and suction line of a respective exhaust gas turbocharger means adapted to be disengaged, and control means for controlling during the engagement or disengagement of the respective exhaust gas turbocharger means the flow cross section of both closure means, said control means being operable during engagement with increasing yield in exhaust gas energy to initially open the exhaust gas closure means of the exhaust gas turbocharger means to be engaged in such a manner that the continuously engaged exhaust gas turbocharger means is continued to be operated near its upper output limit, that only a strongly throttled rate of air flow is made possible to the compressor of the exhaust gas turbocharger means to be engaged during the engaging operation by means of a by-pass line adapted to be closed off which operatively connects a charging air manifold of the internal combustion engine with the suction line of the compressor downstream of the charging air closure means, and that the complete opening of the exhaust gas closure means is undertaken only when the exhaust gas turbocharger means has nearly reached the operating rotational speed necessary for the engagement.

Claim 3

A piston internal combustion engine according to claim 1, with a charging air cooler means arranged in the line between the charging air manifold of the internal combustion engine and the compressor of the exhaust gas turbocharger means adapted to be disengaged, the by-pass line branching off directly downstream of the charging air cooler means.

Claim 4

A piston internal combustion engine, comprising several exhaust gas turbocharger means, of which during partial load operation of the internal combustion engine at least one exhaust gas turbocharger means is adapted to be disengaged, each turbocharger means comprising compressor means and turbine means, a suction line leading to the compressor means and an exhaust gas line leading to the turbine means of the respective exhaust gas turbocharger means, one of said exhaust gas turbocharger means being continuously connected with the internal combustion engine, closure means in the exhaust line and in the suction line leading to a respective exhaust gas turbocharger means adapted to be disengaged, a charging air manifold, the compressor means of each exhaust gas turbocharger means feeding compressed air to the charging air manifold, a by-pass line from the compressor means of the respective exhaust gas turbocharger means adapted to be disengaged from the suction line of the corresponding compressor means downstream of the closure means in the corresponding suction line, valve means in said by-pass line, and control means controlling said closure means and said valve means in such a manner that during the engagement of a respective exhaust gas turbocharger means with increasing yield in exhaust gas energy, the continuously engaged exhaust gas turbocharger means continues to be operated near its upper output limit while only a very strongly throttled rate of air flow is made possible to the compressor means of the exhaust gas turbocharger means to be engaged during the engaging operation by means of the valve means, the complete opening of the exhaust gas closure means being undertaken by said control means only when the exhaust gas turbocharger means to be engaged has nearly reached the operating rotational speed necessary for its engagement.

Claim 5

A piston internal combustion engine, comprising several exhaust gas turbocharger means, of which during partial load operation of the internal combustion engine at least one exhaust gas turbocharger means is adapted to be disengaged, each turbocharger means comprising compressor means and turbine means, a suction line leading to the compressor means and an exhaust gas line leading to the turbine means of the respective exhaust gas turbocharger means, one of said exhaust gas turbocharger means being continuously connected with the internal combustion engine, closure means in the exhaust line and in the suction line leading to a respective exhaust gas turbocharger means adapted to be disengaged, a charging air manifold, the compressor means of each exhaust gas turbocharger means feeding compressed air to the charging air manifold, a by-pass line from the compressor means of the respective exhaust gas turbocharger means adapted to be disengaged from the suction line of the corresponding compressor means downstream of the closure means in the corresponding suction line, valve means in said by-pass line, and control means controlling said closure means and said valve means in such a manner that during the engagement of a respective exhaust gas turbocharger means with increasing yield in exhaust gas energy, the continuously engaged exhaust gas turbocharger means continues to be operated near its upper output limit while only a very strongly throttled rate of air flow is made possible to the compressor means of the exhaust gas turbocharger means to be engaged during the engaging operation by means of the valve means, the complete opening of the exhaust gas closure means being undertaken by said control means only when the exhaust gas turbocharger means to be engaged has nearly reached the operating rotational speed necessary for its engagement.

Claim 6

A piston internal combustion engine according to claim 3, further comprising a charging air cooler means connected to the output of the compressor means, the by-pass line branching off substantially directly downstream of the charging air cooler means coordinated to a respective exhaust gas turbocharger means adapted to be engaged.