Patent ID: 8602159
Filing Date: 2013-12-10
Classification: F01N

Abstract:
1. A compact muffler for small two-stroke engines, comprising: (a) A substantially cylindrical shell having an axial dimension and a radial dimension, wherein the radial dimension is substantially greater than the axial dimension, the shell housing divided into at least four removable axial sections, wherein the interior is partitioned into three adjacent substantially cylindrical chambers disposed along the axial dimension, the three adjacent chambers comprising a middle chamber axially bounded by an upper partition plate and a lower partition plate, and radially bounded by an outer wall disposed along the perimeter of the middle chamber and extending between the upper partition plate and lower partition plate, the middle chamber further subdivided into an upper half bounded exteriorly by the second housing shell section and a lower half bounded exteriorly by the third housing shell section, a top auxiliary chamber and a bottom auxiliary chamber, the top and bottom auxiliary chambers disposed axially on opposite sides of the middle chamber, the exterior boundary of each auxiliary chamber coinciding with the first and fourth housing shell sections, the interior boundary of each auxiliary chamber coinciding with the upper and lower plates of the middle chamber; (b) An interior wall initiating as a bifurcation from said outer wall and extending axially from the upper plate to the lower plate, and radially into the interior of said central chamber by following a spiral trajectory along the radial dimension towards the center portion of said central chamber and terminating by joining itself at a point along its innermost spiral forming an enclosed space within said center portion, whereby a spiral exhaust passage of constant cross section is formed and is radially bound between the successive spiral windings of said interior wall and axially bound by the upper and lower plates, said spiral exhaust passage having a fore-portion and an aft-portion, wherein a peripheral terminus disposed near the outer wall demarks the beginning of the fore-portion and a point between the termini of said spiral exhaust passage demarks the boundary between the fore-portion and the aft-portion, said aft-portion continuing to extend along the spiral exhaust passage to an interior terminus disposed within the center portion of said central chamber, thereby demarking the end of the aft-portion; (c) an inlet port disposed along the periphery of the shell of the top auxiliary chamber wherein said inlet port extends through the top auxiliary chamber to communicate with said spiral passage via an aperture disposed at the peripheral terminus in the fore-portion of said spiral passage; (d) an exhaust port disposed along the outer surface of the bottom auxiliary chamber wherein said exhaust port extends through the bottom auxiliary chamber to communicate with said spiral passage via an aperture disposed at the interior terminus of said passage; (e) A plurality of perforations disposed on said top plate and said bottom plate of the central chamber whereby the central chamber communicates with both auxiliary chambers through the plurality of perforations, said plurality of perforations being substantially confined within contours of the aft-portion of the spiral exhaust passage; (f) An internal header coinciding with the non-perforated fore-portion of the spiral exhaust passage; and (g) A packing of sound dampening material enclosed within each of the two auxiliary chambers for attenuation of sound energy carried by exhaust gases entering within, wherein auxiliary chambers communicate with the spiral exhaust passage through the perforations disposed on the upper and lower partition plates of the middle chamber, whereby the exhaust gases do not pass through the sound absorbent material to the atmosphere.