Encased exhaust
11613374 ยท 2023-03-28
Inventors
Cpc classification
F01N2590/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B64U50/11
PERFORMING OPERATIONS; TRANSPORTING
B64D33/04
PERFORMING OPERATIONS; TRANSPORTING
F02K7/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01N13/1833
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B64C39/024
PERFORMING OPERATIONS; TRANSPORTING
F01N1/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
Abstract
The encased exhaust is a traditional aftermarket expansion chamber muffler system for a two stroke engine encompassing a duct fan/propeller. The propeller is mounted directly to the engine's driveshaft, eliminating reduction gears and belts allowing for more airflow and less weight. This eliminates the muffler and replaces the cage on a paramotor, allowing for more airflow through the funneled air duct. The configuration of these two functions exists in a particular sequence.
Claims
1. An exhaust device to increase airflow through an engine thereby increasing engine power, comprising: a two stroke engine that contains a ducted fan liner and further including an encased expansion chamber exhaust ring; the encased expansion chamber exhaust ring provides airflow through a funneled exhaust airduct of the ducted fan liner; the encased expansion chamber exhaust ring is assembled around the ducted fan liner and is configured to funnel exhaust from the engine into the exhaust airduct; the encased expansion chamber exhaust ring is manufactured of sheet metal formed in a circle, the width of the sheet metal varies according to the different number of the expansion chamber stages; the inner side of the encased expansion chamber exhaust ring contains an inlet and outlet and is welded to the respective inlet and outlet ducted fan liner cylinder; the end and beginning of each expansion chamber stage contains either a divergent or convergent diffuser cone arrangement, with the engine header connected to a divergent cone.
Description
BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWING
(1)
(2)
(3)
(4)
DETAILED DESCRIPTION OF THE INVENTION
(5) The expansion chamber stages consist of separate pieces of sheet metal formed in an arc shaped bend. These sheet metal sections are welded together at the inlet and outlet sides of the cylinder's ducting, and at the end and beginning of each stage. The inner liner/sleeve/ducting cylinder is welded to the outer sleeve/shell, creating a chamber. They all funnel air flow. The entire cylinder is the bottom of the expansion chamber stages. The width of the sheet metal changes according to the different number of the expansion chamber stages. The propeller is mounted directly to the engine's driveshaft, eliminating reduction gears and belts allowing for more airflow and less weight. The propeller's diameter determines the stages' combined radius. The engine's header connects to the divergent cone.
REFERENCE CHARACTERS
(6) 1: Header/Inlet 2: Divergent Cone Stage Diffuser (expands) 3: Divergent Cone Stage Diffuser (expands) 4: Divergent Cone Stage Diffuser (expands) 5: Belly 6: Belly 7: Convergent Cone (contracts) 8: Convergent Cone (contracts) 9: Stinger/Outlet