A multi-stage reconfigurable air intake and exhaust
system for an internal
combustion piston engine having a first row of at least two cylinders inclined relative to a
vertical plane, a second row of at least two cylinders inclined relative to the
vertical plane, and the two rows of cylinders form a V configuration with the
vertical plane being approximately
equidistant between the two rows. The
system comprises a Stage 1
package and a Stage 2
package. The Stage 1
package includes a first
exhaust manifold adapted to be secured to the first row of cylinders for receiving and collecting in a plenum exhaust gases from the first row of cylinders, where the first
exhaust manifold includes a first
exhaust gas discharge aperture for discharging exhaust gases, the first
exhaust gas discharge aperture is located at a first fixed spatial position when the first
exhaust manifold is secured to the first row of cylinders, and there is provided first connecting means
proximate the first
exhaust gas aperture. The Stage 1 package additionally includes a second exhaust manifold adapted to be secured to the second row of cylinders for receiving and collecting in a plenum exhaust gases from the second row of cylinders, where the second exhaust manifold includes a second exhaust gas
discharge aperture for discharging exhaust gases, the second exhaust gas discharge aperture is located at a second fixed spatial position when the second exhaust manifold is secured to the first row of cylinders, and there is provided second connecting means
proximate the second exhaust gas aperture. The Stage 2 package includes a first turbo exhaust manifold adapted to be secured to the first row of cylinders for receiving and collecting in a plenum exhaust gases from at least from the first row of cylinders, where the first turbo exhaust manifold includes a first
turbocharger connection aperture adapted for mounting a
turbocharger and for delivering to the
turbocharger exhaust gases from either the first row of cylinders or the first row of cylinders and the second row of cylinders, a first exhaust gas passage aperture and third connecting means
proximate the first exhaust gas passage aperture, the first turbo exhaust manifold being dimensioned so that the first exhaust gas passage aperture is located at about the first fixed spatial position when the first turbo exhaust manifold is secured to the first row of cylinders in lieu of the first exhaust manifold, and a
crossover pipe assembly having a second exhaust gas passage aperture and fourth connecting means proximate the second exhaust gas passage aperture, and having a third exhaust gas passage aperture and fifth connecting means proximate the third exhaust gas passage aperture, where the fourth and fifth connecting means are each adapted for
coupling to any two of the first, second and third connecting means