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US4671056A Expired / Lapsed US ⏱️ 0.0 years remaining

Pulse-sonic jet nozzle

Assignee: Individual
•
Filing: 1986-08-06
•
Granted: 1987-06-09
•
Expires: 2006-08-06
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Abstract

Abstract An improved valveless pulse jet combustor having an air inlet pipe connected to a combustion chamber having ignition means and fuel supply means is disclosed. The combustion chamber is further connected to an exhaust pipe. The combustion chamber is connected to the air inlet pipe via tapered fitting means adapted to receive relief port means, fuel injection means and compressed air inlet means directed towards the center of the chamber. Adjustable orifice flanges are positioned between the combustion chamber and an extension of the exhaust pipe. The inlet pipe and the tapered means have diverging interior diameters, the combustion chamber a converging interior diameter and the extension and exhaust pipe have diverging interior diameters such that in operation, backward thrust is directed through the release port means thereby reducing back flow through the inlet pipe.

Inventors

  • 👤 Matthew L. R. Genz
  • 👤 Bruce Villman

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-08 14:33
CPC Classifications
F; F23; F23R; F23R3/00; F23R3/02; F23R3/04; F23C; F23C15/00; F02; F02K; F02K7/00; F02K7/02; F02K7/04; Y; Y02; Y02T; Y02T50/00; Y02T50/60

Claims Analysis

Total Claims: 8
Claim 1
Independent Claim 159 words
An improved valveless pulse jet combustor having an air inlet pipe connected to a combustion chamber having ignition means and fuel supply means, said combustion chamber being further connected to an exhasut pipe, the improvement comprising: said combustion chamber being connected to said air inlet pipe via tapered fitting means; relief port means, fuel injection means and compressed air inlet means are fitted into said tapered fitting means and directed towards the centre of said chamber, the interior of said combustion chamber is converging towards an extension pipe, connecting said exhaust pipe with said combustion chamber; adjustable orifice flanges positioned between said combustion chamber and said extension pipe; and wherein said inlet pipe and said tapered means have diverging interior diameters, said combustion chamber a converging interior diameter and said extension and exhaust pipe have diverging interior diameters such that in operation, backward thrust is directed through said relief port means thereby reducing back flow through said inlet pipe.
Claim 2
Dependent Claim 159 words
An improved valveless pulse jet combustor having an air inlet pipe connected to a combustion chamber having ignition means and fuel supply means, said combustion chamber being further connected to an exhasut pipe, the improvement comprising: said combustion chamber being connected to said air inlet pipe via tapered fitting means; relief port means, fuel injection means and compressed air inlet means are fitted into said tapered fitting means and directed towards the centre of said chamber, the interior of said combustion chamber is converging towards an extension pipe, connecting said exhaust pipe with said combustion chamber; adjustable orifice flanges positioned between said combustion chamber and said extension pipe; and wherein said inlet pipe and said tapered means have diverging interior diameters, said combustion chamber a converging interior diameter and said extension and exhaust pipe have diverging interior diameters such that in operation, backward thrust is directed through said relief port means thereby reducing back flow through said inlet pipe.
Claim 3
Dependent Claim 22 words
A pulse jet combustor as defined in claim 1 wherein said relief port means is provided with said compressed air inlet means.
Claim 4
Dependent Claim 43 words
A pulse jet combustor as defined in claim 1 further comprising means positioned at said exhaust pipe to permit dehydration of food products by reducing the rate of flow of said product as it is exposed to hot gases produced by said combustor.
Claim 5
Dependent Claim 28 words
A pulse jet combustor as defined in claim 1 wherein the interior diameter of said tapered fitting is larger than the interior diameter of said air inlet pipe.
Claim 6
Dependent Claim 26 words
A pulse jet combustor as defined in claim 1 wherein said extension is U-shaped such that said exhaust pipe is generally parallel to said inlet pipe.
Claim 7
Dependent Claim 26 words
A pulse jet combustor as defined in claim 1 wherein said pulse jet combustor is made of heat resistant material such as ASTM A297 Grade HU.
Claim 8
Dependent Claim 27 words
A pulse jet combustor as defined in claim 1 wherein said adjustable orifice flanges comprises sliding metal plates to constrict the interior diameter of said combustion chamber.

References Cited (Backward Citations)

US2647365A Cited
US2738646A Cited
US2743575A Cited
US2812635A Cited
US2919542A Cited
US2970430A Cited
US3266252A Cited
US3456441A Cited
US3462955A Cited
US3592395A Cited
US3618655A Cited
US4033120A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1990-06-08 1990-12-08 1991-06-09 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1994-06-08 1994-12-08 1995-06-09 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1998-06-08 1998-12-08 1999-06-09 $7700.00 Window Closed / Lapsed

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