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.