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US4487290A Expired / Lapsed US ⏱️ 0.0 years remaining

Light aircraft engine muffler

Assignee: MUSTANG UNITS Co
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Filing: 1983-04-29
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Granted: 1984-12-11
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Expires: 2003-04-29
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Abstract

Abstract A relatively small, lightweight muffler is provided, especially adapted to low horsepower aircraft and comprises an elongated, essentially cylindrical structure made up of inner and outer casings having sound-absorbent-material-containing chambers and pressure-wave trap elements to minimize exhaust noises. The rear end of the muffler is in the form of a cone having its apex to the rear and containing a quantity of sound-absorbent material in a rearward part thereof and the conical wall ahead of this material being perforated. One form of the structure has a convex or hemispherical front end for aerodynamic purposes in those cases where the muffler is installed externally of the aircraft. The pressure-wave traps comprise walled structures having louvered slots therein appropriately aimed to direct the pressure waves to the sound-absorbent material.

Inventors

  • 👤 William J. Flaherty

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-31 19:19
CPC Classifications
F; F01; F01N; F01N1/00; F01N1/24

Claims Analysis

Total Claims: 12
Claim 1
Independent Claim 220 words
A muffler for use with the internal-combustion engine of light aircraft, comprising an elongated, essentially hollow structure having a cylindrical body and front and rear end portions, said body being in the form of an imperforate cylindrical wall, said front end portion including a wall spanning and affixed to the front end of the body, one of said walls including a forward exhaust inlet leading to the interior of the structure, and said rear end portion being in the form of a cone coaxial with and having its base affixed to the rear end of the body and its apex disposed rearwardmost, said cone including a foraminous interior radial partition fixedly positioned intermediate the base and apex of the cone to form a conical chamber at the cone apex, the wall of the cone forwardly of the partition having a plurality of perforations therein, sound-absorbent material contained in the apex chamber, a tubular pressure-wave trap element within the cylindrical wall and extending from the exhaust inlet to the cone, said element having a peripheral wall spacedly surrounded by the cylindrical wall to provide an annular chamber between the element and the cylindrical wall, the element wall including a plurality of slots therein communicating the interior of the element with the annular chamber, and sound-absorbent material contained in the annular chamber.
Claim 2
Dependent Claim 220 words
A muffler for use with the internal-combustion engine of light aircraft, comprising an elongated, essentially hollow structure having a cylindrical body and front and rear end portions, said body being in the form of an imperforate cylindrical wall, said front end portion including a wall spanning and affixed to the front end of the body, one of said walls including a forward exhaust inlet leading to the interior of the structure, and said rear end portion being in the form of a cone coaxial with and having its base affixed to the rear end of the body and its apex disposed rearwardmost, said cone including a foraminous interior radial partition fixedly positioned intermediate the base and apex of the cone to form a conical chamber at the cone apex, the wall of the cone forwardly of the partition having a plurality of perforations therein, sound-absorbent material contained in the apex chamber, a tubular pressure-wave trap element within the cylindrical wall and extending from the exhaust inlet to the cone, said element having a peripheral wall spacedly surrounded by the cylindrical wall to provide an annular chamber between the element and the cylindrical wall, the element wall including a plurality of slots therein communicating the interior of the element with the annular chamber, and sound-absorbent material contained in the annular chamber.
Claim 3
Dependent Claim 20 words
The muffler of claim 1, further characterized in that the front wall is forwardly convex as respects the cylindrical wall.
Claim 4
Dependent Claim 14 words
The muffler of claim 1, further characterized in that the front wall is hemispherical.
Claim 5
Dependent Claim 29 words
The muffler of claim 1, further characterized in that the front wall is forwardly convex as repects the cylindrical wall and the exhaust inlet is in said front wall.
Claim 6
Dependent Claim 29 words
The muffler of claim 1, further characterized in that the front wall is forwardly convex as respects the cylindrical wall and the exhaust inlet is in the cylindrical wall.
Claim 7
Dependent Claim 35 words
The muffler of claim 1, further characterized in that the wall of the tubular element has louvers associated with the slots for directing pressure waves from the interior of the element to the annular chamber.
Claim 8
Dependent Claim 74 words
The muffler of claim 1, further characterized in that the front wall is forwardly convex as respects the cylindrical wall, the exhaust inlet is in the cylindrical wall, a forward radial partition is fixedly disposed at the junction of the cylindrical and convex walls to provide a forward chamber, said partition having slots opening from the interior of the cylindrical wall to the forward chamber, and sound-absorbent material is contained in the forward chamber.
Claim 9
Dependent Claim 15 words
The muffler of claim 7, further characterized in that the partition slots have louvers thereon.
Claim 10
Dependent Claim 42 words
The muffler of claim 1, further characterized in that the exhaust inlet is in the front wall and leads coaxially to the tubular element, and a diffuser member is disposed in the inlet upstream of the slots in the tubular element wall.
Claim 11
Dependent Claim 25 words
The muffler of claim 9, further characterized in that the diffuser is in the form of a radial wall having substantially radially disposed slots therein.
Claim 12
Dependent Claim 31 words
The muffler of claim 10, further characterized in that the radial wall has circumferentially directed deflector fins respectively along the slots and disposed at the downstream side of the diffuser wall.

References Cited (Backward Citations)

US2705541A Cited
US3710891A Cited
US3757892A Cited
US4263982A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1987-12-11 1988-06-11 1988-12-11 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1991-12-11 1992-06-11 1992-12-11 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1995-12-11 1996-06-11 1996-12-11 $7700.00 Window Closed / Lapsed

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