A system for optimizing engine air-mass-flow intake of an aircraft includes a forward-facing airframe-inlet duct interoperably coupled to an inlet of an engine of the aircraft, an air-mass-flow bypass mechanism coupled to the forward-facing airframe-inlet duct and adjustable to allow a selected amount of air entering an inlet of the forward-facing airframe-inlet duct to bypass the inlet of the engine, and an air-pressure sensor arranged in the forward-facing airframe-inlet duct adjacent to the inlet of the engine. A measured value (“PT1”) from the air-pressure sensor is used to determine a degree to which the air-mass-flow bypass mechanism is to be opened.

Methods and systems are provided for forming an air-fuel mixture in a combustion chamber of an internal combustion engine. In one example, a system may include an adjustable intake line coupled to an inlet opening of the cylinder. The system may adjust turbulence formed in the cylinder in response to engine operating conditions by controlling a pivoting angle between a first section of the intake line and a second section of the intake line.

A silencer for noise reduction at an internal combustion engine is disclosed. The silencer comprises an input opening, an output opening, at least one chamber, and at least one partition configured to be inserted into and removed from the at least one chamber to convert the silencer to a collector.

A silencer for noise reduction at an internal combustion engine is disclosed. The silencer comprises an input opening, an output opening, at least one chamber, and at least one partition configured to be inserted into and removed from the at least one chamber to convert the silencer to a collector.