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US4054028A Expired / Lapsed US ⏱️ 0.0 years remaining

Fuel combustion apparatus

Assignee: Mitsubishi Heavy Industries Ltd
•
Filing: 1975-08-28
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Granted: 1977-10-18
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Expires: 1995-08-28
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Abstract

Abstract A fuel combustion apparatus of a double-shell construction in which the inner shell is composed of an upstream small-diameter section, a downstream large-diameter section, and a conically-shaped connecting section between the two sections of different diameters, all the sections being aligned and connected together on a common axis. Fuel injection valve and a first air supply port equipped with swirl blades surrounding the valve are provided at the upstream end of the small-diameter section of the inner shell. The cylindrical wall of the small-diameter section is not formed with any air supply port, but second air supply ports shrouded with scoops are formed in the cylindrical wall portion of the large-diameter section close to the small-diameter section. On the upstream side of the first air supply port is installed means for controlling the rate of air supply to the same port.

Inventors

  • 👤 Katsuyuki Kawaguchi

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-24 10:42
CPC Classifications
F; F23; F23C; F23C6/00; F23C6/04; F23C6/045; F23C7/00; F23R; F23R3/00; F23R3/02; F23R3/26

Claims Analysis

Total Claims: 8
Claim 1
Independent Claim 265 words
A fuel combustion apparatus comprising an outer shell defining an enclosed hollow chamber, an inner shell composed of an upstream small-diameter section located within said chamber, a downstream large-diameter section extending in part outwardly of one end of said outer shell and a conically shaped connecting section between the two sections of different diameters, all said sections being aligned and connected together on a common axis and spaced from said outer shell, duct means extending through said outer shell for the supply of air to the space between said shells, a fuel injection valve and a first air supply port in communication with the space between said shells equipped with swirl blades surrounding the injection valve, said injection valve and air supply port being both provided at the upstream end of the small-diameter section of the inner shell, both the cylindrical wall of the small-diameter section and the conical wall of the connecting section of the inner shell being not perforated for air supply, second air supply ports in communication with the space between said shells formed in the cylindrical wall portion of the large-diameter section close to the connecting section, each of said second ports being shrouded with scoops extending at an angle into the large-diameter section at least perpendicularly to the direction of flow of said fuel, and means installed on the upstream side of the first air supply port for controlling the rate of air supply from said duct to the said first port whereby the flow of air supply to said first port relative to said second ports may be regulated.
Claim 2
Dependent Claim 265 words
A fuel combustion apparatus comprising an outer shell defining an enclosed hollow chamber, an inner shell composed of an upstream small-diameter section located within said chamber, a downstream large-diameter section extending in part outwardly of one end of said outer shell and a conically shaped connecting section between the two sections of different diameters, all said sections being aligned and connected together on a common axis and spaced from said outer shell, duct means extending through said outer shell for the supply of air to the space between said shells, a fuel injection valve and a first air supply port in communication with the space between said shells equipped with swirl blades surrounding the injection valve, said injection valve and air supply port being both provided at the upstream end of the small-diameter section of the inner shell, both the cylindrical wall of the small-diameter section and the conical wall of the connecting section of the inner shell being not perforated for air supply, second air supply ports in communication with the space between said shells formed in the cylindrical wall portion of the large-diameter section close to the connecting section, each of said second ports being shrouded with scoops extending at an angle into the large-diameter section at least perpendicularly to the direction of flow of said fuel, and means installed on the upstream side of the first air supply port for controlling the rate of air supply from said duct to the said first port whereby the flow of air supply to said first port relative to said second ports may be regulated.
Claim 3
Dependent Claim 16 words
The apparatus according to claim 1, wherein said scoops are inclined at an angle directed upstream.
Claim 4
Dependent Claim 30 words
The apparatus according to claim 1 including a perforated baffle disk secured to the inner wall portion of the small-diameter section close to the large-diameter section of the inner shell.
Claim 5
Dependent Claim 41 words
The apparatus according to claim 1, wherein said air supply controlling means including a cylinder that opens in the space between the outer and inner shells and a piston that is actuated by the pressure of air in said annular space.
Claim 6
Dependent Claim 20 words
The apparatus according to claim 4 including means operable from the exterior of said outer shell to adjust said piston.
Claim 7
Dependent Claim 52 words
The apparatus according to claim 1, wherein said air supply control comprises a hollow enclosed housing located over the upstream end of said small-diameter section and includes a valve member located in the wall of said housing to regulate the flow of air into said housing from the space between said shells.
Claim 8
Dependent Claim 21 words
The apparatus according to claim 6 including means operable from the exterior of said outer shell to adjust said valve member.

References Cited (Backward Citations)

US2227666A Cited
US2446059A Cited
FR917080A Cited
US2458497A Cited
FR1033539A Cited
US3099134A Cited
US3577878A Cited
US3589127A Cited
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USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1980-10-17 1981-04-18 1981-10-18 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1984-10-17 1985-04-18 1985-10-18 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1988-10-17 1989-04-18 1989-10-18 $7700.00 Window Closed / Lapsed

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