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公开(公告)号:US20210189951A1
公开(公告)日:2021-06-24
申请号:US17262732
申请日:2019-07-25
Applicant: Ravi Shankar Gautam
Inventor: Ravi Shankar Gautam
Abstract: This patent discloses thrust vectoring ignition chamber engine. Thrust vectoring ignition chamber used in this engine is an annular cylinder having nozzles mounted in a way such that during fuel suction phase they are sealed and during ignition of fuel they are unsealed so that hot jets of ignited fuel escaping through nozzles cause coupled rotatory motion on the ignition chamber. Engine uses cam operated two transverse piston based mechanism for suction and compression of fuel which facilitates separation of fuel valve from ignition chamber with the help of which combustion process and suction-compression process can occur simultaneously. Flywheel mounted on extension of ignition chamber functions as output of the engine. Each half rotation of flywheel completes three phases namely fuel/air suction, compression and combustion. Thus this engine fires for every half revolution and therefore can give improved power boost.
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公开(公告)号:US20210310405A1
公开(公告)日:2021-10-07
申请号:US17262762
申请日:2019-07-25
Applicant: Ravi Shankar Gautam
Inventor: Ravi Shankar Gautam
Abstract: This patent discloses thrust vectoring ignition chamber engine in which ignition chamber is an annular cylinder having nozzles mounted such that during fuel suction phase they are sealed and during ignition of fuel they are unsealed so that hot jets of ignited fuel escaping through nozzles cause coupled rotatory motion on the ignition chamber. Engine uses specially designed dwell barrel cam mechanism for two phase suction and compression of fuel which facilitates the separation of fuel valve from ignition chamber. Flywheel mounted on extension of ignition chamber functions as output of the engine. Timing of electrically controlled nozzle seal and fuel valve can be adjusted so that each half rotation of flywheel completes three phases namely fuel/air suction, compression and combustion, instead of two rotations as required in engine according to prior art. This engine can give improved power boost by firing for every half revolution.
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公开(公告)号:US20210310357A1
公开(公告)日:2021-10-07
申请号:US17262758
申请日:2019-07-25
Applicant: Ravi Shankar Gautam
Inventor: Ravi Shankar Gautam
Abstract: This patent discloses thrust vectoring ignition chamber engine. Thrust vectoring ignition chamber used in this engine is an annular cylinder having nozzles mounted in a way such that during fuel suction phase they are sealed and during ignition of fuel they are unsealed so that hot jets of ignited fuel escaping through nozzles cause coupled rotatory motion on the ignition chamber. Engine uses specially designed dwell barrel cam mechanism for suction and compression of fuel. Flywheel mounted on extension of ignition chamber functions as output of the engine. Each half rotation of flywheel completes three phases namely fuel/air suction, compression and combustion. Thus this engine fires for every half revolution and therefore can give improved power boost.
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公开(公告)号:US20210164394A1
公开(公告)日:2021-06-03
申请号:US17262725
申请日:2019-07-25
Applicant: Ravi Shankar Gautam
Inventor: Ravi Shankar Gautam
Abstract: This patent discloses thrust vectoring ignition chamber engine. Thrust vectoring ignition chamber used in this engine is an annular cylinder having nozzles mounted in a way such that during fuel suction phase they are sealed and during ignition of fuel they are unsealed so that hot jets of ignited fuel escaping through nozzles cause coupled rotatory motion on the ignition chamber. Engine uses cam operated suitably modified 3-screw compressor for suction and compression of fuel and therefore do not require piston mechanism. Flywheel mounted on extension of ignition chamber functions as output of the engine. Each half rotation of flywheel completes three phases namely fuel/air suction, compression and combustion. Thus this engine fires for every half revolution and therefore can give improved power boost.
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公开(公告)号:US20220178256A1
公开(公告)日:2022-06-09
申请号:US17442713
申请日:2020-05-26
Applicant: Ravi Shankar Gautam
Inventor: Ravi Shankar Gautam
Abstract: This patent discloses one cylinder axial internal combustion engine having Scotch-Yoke based two phase fuel compression system. Scotch-Yoke actuator employed here is a specially modeled Multi Purpose Multi H-Slot double action Scotch-Yoke Actuator. Each H-slot is quad-laterally operated by a special mechanism. It performs suction and compression in ignition chamber and auxiliary compression chamber via two piston plates one in each chamber and transfers compressed fuel-air mixture from auxiliary compression chamber to ignition chamber through yoke rod. Flywheel is coaxially mounted on the outward side of the auxiliary compression chamber.
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公开(公告)号:US20220097800A1
公开(公告)日:2022-03-31
申请号:US17421825
申请日:2020-01-10
Applicant: Ravi Shankar Gautam
Inventor: Ravi Shankar Gautam
Abstract: This patent discloses drive mechanism which facilitates the usage of multiple planetary gears of enhanced pivoted-slewing-bearing-epicyclic-gear, on both sides of the driving wheel of bicycle, reverse trike and unicycle to drive the wheel, thereby facilitating application of driving force on larger area. Mechanism helps in drawing more power from the rider efficiently. Helps to provide more restraining support to the wheel, thereby reduce the wobbling of the wheel. Additional arrangement is provided which facilitates syncing of pedals during reverse pedaling while allowing driving wheel to coast. Additionally the said mechanism also provides anti-tipping cum braking mechanism in unicycle.
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公开(公告)号:US20210189879A1
公开(公告)日:2021-06-24
申请号:US17262729
申请日:2019-07-25
Applicant: Ravi Shankar Gautam
Inventor: Ravi Shankar Gautam
Abstract: This patent discloses thrust vectoring ignition chamber engine. Thrust vectoring ignition chamber used in this engine is an annular cylinder having nozzles mounted in a way such that during fuel suction phase they are sealed and during ignition of fuel they are unsealed so that hot jets of ignited fuel escaping through nozzles cause coupled rotatory motion on the ignition chamber. Engine uses cam operated specially designed bilaterally operated double action scotch-yoke mechanism which facilitates two phase suction and compression of fuel and facilitates separation of fuel valve from ignition chamber. Flywheel mounted on extension of ignition chamber functions as output of the engine. Each half rotation of flywheel completes three phases namely fuel/air suction, compression and combustion. Thus this engine fires for every half revolution and therefore can give improved power boost.
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