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US3733824A Expired / Lapsed US ⏱️ 0.0 years remaining

Antipollution jet engine with reversible auxiliary jet engines operable independently to serve as auxiliary thrusters and brakes

Assignee: Individual
•
Filing: 1971-07-20
•
Granted: 1973-05-22
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Expires: 1991-07-20
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Abstract

Abstract An antipollution jet engine in which air is fed through the chamber walls of the combustion chamber downstream of the fuel oil nozzle. The air is caused to have a tangential swirling motion to assist in obtaining a complete burning mixture so as to burn all combustible material in the fuel to eliminate pollution. Additional fuel is supplied to a downstream burner similarly provided with downstream air admission ports to create a circular tangential turbulence for a complete mixing and complete burning of the combustible materials. The function of the downstream burner is to assist in completely burning all of the combustible materials resulting from the first burners. The fuel for the first burners and the downstream burner is preheated to improve ignition and burning.

Inventors

  • 👤 L Grainger

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-29 22:28
CPC Classifications
F; F02; F02K; F02K1/00; F02K1/54; F23; F23R; F23R3/00; F23R3/02; F23R3/26; F23R3/28; F23R3/30; F23R3/32; F23R3/42; F23R3/60; F05; F05D; F05D2250/00; F05D2250/40; F05D2250/41; F05D2250/411

Claims Analysis

Total Claims: 10
Claim 1
Independent Claim 291 words
An antipollution jet engine including a plurality of main burners each of said main burners including a combustion chamber, a fuel nozzle secured in one end of said combustion chamber, a supply of primary air connected to said one end of said combustion chamber, a supply of additional air passing through a plurality of bores in said combustion chamber sloped to direct the additional air tangentially and downstream to create a swirling action therein, said combustion chamber having a reduced diameter extension on the end thereof opposite said one end, said extension providing a downstream final burner and cooling section of said main burner and having a plurality of air directing bores to direct additional air tangentially and downstream, means detachably mounting said main burners in said jet engine, a downstream combustion chamber in said jet engine to receive the collective products of combustion of said main burners, a reduced diameter extension on said downstream combustion chamber, means for providing fuel to said downstream combustion chamber, means for supplying air to said downstream combustion chamber, a plurality of auxiliary jet engines mounted on said jet engine with the axes thereof parallel to the axis of said jet engine, means on said jet engine cooperating with means on said auxiliary jet engines for reversing the direction of said auxiliary jet engines for braking action, means for supplying fuel to said auxiliary jet engines, means for supplying air to said auxiliary jet engines from the additional air supply of said jet engine, means cooperating with said reversing means for interrupting the flow of fuel and air to said auxiliary jet engine during the reversing thereof, and selectively actuatable means for controlling the air supply to said main bUrners and the additional air supply.
Claim 2
Dependent Claim 291 words
An antipollution jet engine including a plurality of main burners each of said main burners including a combustion chamber, a fuel nozzle secured in one end of said combustion chamber, a supply of primary air connected to said one end of said combustion chamber, a supply of additional air passing through a plurality of bores in said combustion chamber sloped to direct the additional air tangentially and downstream to create a swirling action therein, said combustion chamber having a reduced diameter extension on the end thereof opposite said one end, said extension providing a downstream final burner and cooling section of said main burner and having a plurality of air directing bores to direct additional air tangentially and downstream, means detachably mounting said main burners in said jet engine, a downstream combustion chamber in said jet engine to receive the collective products of combustion of said main burners, a reduced diameter extension on said downstream combustion chamber, means for providing fuel to said downstream combustion chamber, means for supplying air to said downstream combustion chamber, a plurality of auxiliary jet engines mounted on said jet engine with the axes thereof parallel to the axis of said jet engine, means on said jet engine cooperating with means on said auxiliary jet engines for reversing the direction of said auxiliary jet engines for braking action, means for supplying fuel to said auxiliary jet engines, means for supplying air to said auxiliary jet engines from the additional air supply of said jet engine, means cooperating with said reversing means for interrupting the flow of fuel and air to said auxiliary jet engine during the reversing thereof, and selectively actuatable means for controlling the air supply to said main bUrners and the additional air supply.
Claim 3
Dependent Claim 48 words
A device as claimed in claim 1 wherein said reversible auxiliary jet engines are mounted on pivot pins extending outwardly from said jet engine and power driven means is provided for rotating said reversible auxiliary jet engines about said pivot pins to reverse the direction of thrust therefrom.
Claim 4
Dependent Claim 60 words
A device as claimed in claim 2 wherein the power means for reversing said reversible auxiliary jet engines includes a ring gear secured to each of said reversible auxiliary jet engines, an electric motor, and gears connecting said electric motor to said ring gear to rotate said ring gear with its attached jet engine upon rotation of said electric motor.
Claim 5
Dependent Claim 44 words
A device as claimed in claim 1 including an additional air supply in said downstream combustion chamber reduced diameter extension passing through a plurality of bores in said extension sloped to direct the additional air tangentially and downstream to create a swirling action therein.
Claim 6
Dependent Claim 28 words
A device as claimed in claim 1 wherein the means for controlling the air supply comprises a ported rotary plate valve and means for rotating said valve plate.
Claim 7
Dependent Claim 48 words
A device as claimed in claim 4 wherein said reversible auxiliary jet engines are mounted on pivot pins extending outwardly from said jet engine and power driven means is provided for rotating said reversible auxiliary jet engines about said pivot pins to reverse the direction of thrust therefrom.
Claim 8
Dependent Claim 61 words
A device as claimed in claim 6 wherein the power means for reversing said reversible auxiliary jet engines includes a ring gear secured to each of said reversible auxiliary jet engines, an electric motor, and gears connecting said electric motor to said ring gear to rotate said ring gear with its attached auxiliary jet engine upon rotation of said electric motor.
Claim 9
Dependent Claim 48 words
A device as claimed in claim 5 wherein said reversible auxiliary jet engines are mounted on pivot pins extending outwardly from said jet engine and power driven means is provided for rotating said reversible auxiliary jet engines about said pivot pins to reverse the direction of thrust therefrom.
Claim 10
Dependent Claim 61 words
A device as claimed in claim 8 wherein the power means for reversing said reversible auxiliary jet engines includes a ring gear secured to each of said reversible auxiliary jet engines, an electric motor, and gears connecting said electric motor to said ring gear to rotate said ring gear with its attached auxiliary jet engine upon rotation of said electric motor.

References Cited (Backward Citations)

No citation records indexed.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1976-05-21 1976-11-20 1977-05-22 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1980-05-21 1980-11-20 1981-05-22 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1984-05-21 1984-11-20 1985-05-22 $7700.00 Window Closed / Lapsed

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