PATENT EXPIRED FOR FAILURE TO PAY MAINTENANCE FEES (ORIGINAL EVENT CODE: EXP. 7 and comprises an annular throat region 126 having an axially width approximately equal to that of the thrust matter discharge ports 50 of the rotor 36. A central steam tube 78 is axially aligned with the rotor axis X and extends inside the internal volume 66 of the thrust matter plenum 54. The upstream portion of the combustion region is spaced from the rotor axis a distance not greater than 90% of R, where R is the shortest distance between the rotor axis and the jet stream centerline.

8 is a flow diagram of the operation of the rotary heat engine of FIG. 5,560,196, issued Oct. 1, 1996, the disclosures of which are hereby incorporated by reference. The rotary engine 20 is adapted to burn various types of fuel to produce rotational mechanical power which is then preferably converted into electrical power. .

steam turbines with pressure velocity transformation exclusively in rotor, e.g. I have bought engines for a couple different cars and some were able to go in other cars that the engine swap upgrade didn’t have available. A combustion region is defined at least in part by the rotor and has an upstream portion. The rotary engine is adapted to cause a combustion reaction of an oxygen-fuel mixture in the combustion region in a manner to form combustion reaction products which comprise at least a part of thrust matter to be discharged through at least one of the discharge ports of the first and second jet assemblies. As the exhaust matter flow is decelerated, the kinetic energy of the flow is recovered with increases in static pressure and temperature which increases usable heat for extraction in the super heater (bottoming cycle). . 8 and described below in greater detail, some of the super heated steam provided to the rotor 36 may be mixed with the fuel to hydroxylate the fuel prior to its discharge into the combustion chamber 96. Currently, you can only get to about 600+ bhp with full Ult+ upgrades. In Need for Speed Heat, you can take any car and give it the handling style you like or need. a combustion region having an upstream portion defined by the stator, the rotary engine being adapted to cause a combustion reaction of an oxygen-fuel mixture in the combustion region in a manner to form combustion reaction products which comprise at least a part of thrust matter to be discharged through at least one of the thrust matter discharge ports of the first and second thrust matter jet assemblies, the rotary engine being adapted to combust at least some of the oxygen-fuel mixture in the upstream portion of the combustion region such that at least a portion of the combustion reaction occurs in the upstream portion of the combustion region. NFS Heat Engine Swap Sources. In yet another aspect of the present invention, a jet-propelled rotary engine comprises a stator and a rotor operatively coupled to the stator for rotation of the rotor relative to the stator about a rotor axis. Of course, one could argue that it's not exactly balanced, since the BRZ is lighter (or equal in weight) than the Exige and gets over 1,000 bhp from swaps. Need for Speed: Heat (+8 TRAINER) by FLiNG. Furthermore, steam is passed through the second steam passageways 122 of the annular duct 102 which acts to cool the walls forming the converging region 112 and the diverging region 114 of the annular duct 102 and to further recover heat from the exhaust matter flow. A jet-propelled rotary engine comprises a stator and a rotor operatively coupled to the stator for rotation of the rotor relative to the stator about a rotor axis. The duct has a generally annular duct diverging region that diverges as it extends radially outwardly. More recently, the inventor has made developments in the field of rotary heat engines for which he has received U.S. Pat. Mixed in with the reaction products of the combustion is non-reaction matter, i.e., matter such as nitrogen, excess and bypass air, oxygen, water, etc., introduced into the thrust matter plenum 54 but which is not part of the combustion reaction. The exhaust pipe is configured to expel the exhaust matter into the environment external to the rotary engine or, optionally, into an exhaust system which transports the exhaust matter away from the rotary engine. The second jet assembly defines a second converging flow region, a second diverging flow region downstream of the second converging flow region, and a second discharge port. Various engines are unlocked as players reach higher reputation levels. 7. Micro reaction turbine with integrated combustion chamber and rotor. Press question mark to learn the rest of the keyboard shortcuts, https://www.carfolio.com/specifications/models/car/?car=88385#a_aerodynamics. 1 shown generally from the opposite side. A jet-propelled rotary engine as set forth in. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). . 1. No. The steam discharge port is adapted to traverse a circular path as the rotor rotates about the rotor axis. The rotor comprises at least one jet assembly that defines a converging flow region, a diverging flow region downstream of the converging flow region, and a discharge port. It seems that there is no rotary swap. 345 HP 4.0L V8 - ??? I was wondering if anyone would be interested in finding the sources of the engines that can be swapped into the cars.

For instance, Goddard U.S. Pat. . . The rotary engine has a combustion region that includes an upstream portion and is adapted to cause a combustion reaction of an oxygen-fuel mixture in the combustion region in a manner to form combustion reaction products which comprise at least a part of thrust matter to be discharged through the discharge port. From the super-heater 30, the exhaust matter passes into the boiling plate heat exchanger 32 which contains the water that is ultimately converted into steam, further reducing the temperature of the exhaust matter flow and recovering heat therefrom.

), Free format text: The combustion region is defined at least in part by the rotor and has an upstream portion. A jet-propelled rotary engine comprising: a rotor operatively coupled to the stator for rotation of the rotor relative to the stator about a rotor axis, the rotor comprising at least first and second thrust matter jet assemblies, the first thrust matter jet assembly defining a first thrust matter converging flow region, a first thrust matter diverging flow region downstream of the first thrust matter converging flow region, and a first thrust matter discharge port, the second thrust matter jet assembly defining a second thrust matter converging flow region, a second thrust matter diverging flow region downstream of the second thrust matter converging flow region, and a second thrust matter discharge port; and. From Grip to Drift to Off-Road. A jet-propelled rotary engine comprising: a rotor operatively coupled to the stator for rotation of the rotor relative to the stator about a rotor axis, the rotor comprising at least first and second thrust matter jet assemblies and at least at least first and second steam jet assemblies, the first thrust matter jet assembly defining a first thrust matter converging flow region, a first thrust matter diverging flow region downstream of the first thrust matter converging flow region, and a first thrust matter discharge port, the second thrust matter jet assembly defining a second thrust matter converging flow region, a second thrust matter diverging flow region downstream of the second thrust matter converging flow region, and a second thrust matter discharge port, the first steam jet assembly defining a first steam converging flow region, a first steam diverging flow region downstream of the first steam converging flow region, and a first steam discharge port, the second steam jet assembly defining a second steam converging flow region, a second steam diverging flow region downstream of the second steam converging flow region, and a second steam discharge port, the rotary engine being adapted and configured to channel steam through the steam discharge ports of the first and second steam jet assemblies; and. The annular duct 102 of the preferred embodiment is shown in detail in FIG. 6 showing an alternative embodiment of the annular duct. - 1288 - $610,000730hp 6.5l V12 - Aventador S - 875 -$454,500755hp 6.2L V8 - Corvette ZR1 - 1009 - $475,500. What he's wondering is if the Exige can have better motor swap options. The first jet assembly defines a first converging flow region, a first diverging flow region downstream of the first converging flow region, and a first discharge port. As discussed above and shown in FIG. The guide vanes 76 and the convex shape of the end wall 74 are configured and adapted to increase the efficiency of the gas flow from the thrust matter plenum 54 into the thrust matter tubes 52 when the rotor 36 is revolving about the rotor axis X during operation of the rotary engine 20. 1 taken along the plane of line 44 of FIG. ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:SCHLOTE, ANDREW;REEL/FRAME:014849/0777. 6,668,539 and entitled Rotary Heat Engine, and incorporated herein by reference. Owner name: Spiral machine element for gaseous and/or liquid fluids, Electrical power generation system and method for mitigating corona discharge, Toroid-shaped gas turbine of boundary layer, Vehicle energy harvesting device having a continuous loop of shape memory alloy, Rotary three dimentional variable volume machine, Reaction turbine and hybrid impulse reaction turbine, Method and apparatus for converting heat energy into mechanical energy, A kind of Multi-stage ram compressor and apply its electromotor, Engine, biomass powder energy conversion and/or generation system, hybrid engines including the same, and methods of making and using the same, Environment-friendly power machine with large couple moment formed by pushing long couple arm through jet power, Rotating pulse detonation engine, power generation system including the same, and methods of making and using the same, Small fuel combined heat and power by steam jet type system, Air-jet turbine with hydraulic centrifugal based, closed circuit works when the hydropower stations, Steam-operated rotating combustion chamber, Rotating, feeding, and cooling means for combustion chambers, Combustion chamber in rotating annular casing, Continuous combustion type rotating combustion products generator, Stationary power plant having radially and axially displaced jet engines, Pure reaction turbine with evacuated chamber and rotor element therefor, Method and apparatus for power generation using rotating ramjet which compresses inlet air and expands exhaust gas against stationary peripheral wall, Internal combustion engine, operated by the recoil of a burnt air-fuel mixture in a kreisfoermigen, by type of a Chinese fire wheel functioning turbine, Circulation expander of lost energy of heat machines, Method of pumping gaseous matter via a supersonic centrifugal pump, Tangential combustion chamber with vaneless turbine for gas turbine engine, Gas turbine engine with means for reducing the formation and emission of nitrogen oxides, Gas turbine and method for discharging gas from gas turbine, Transition with a linear flow path for use in a gas turbine engine, Aircraft gas turbine engine having variable torque split counter rotating low pressure turbines and single direction of rotation booster aft of counter rotating fans, Transition with a linear flow path with exhaust mouths for use in a gas turbine engine, Combined cycle pulse detonation turbine engine, Cooling air supply structure of gas turbine and gas turbine, High area-ratio inter-turbine duct with inlet blowing, Vortical flow gas turbine with centrifugal fuel injection, Thruster for aircraft with compound cycle, Method of and device for generation of energy (versions), Methods and apparatus for assembling a gas turbine engine, Constant volume combustion turbine with plurality flow turbine wheels, Information on status: patent discontinuation, Lapse for failure to pay maintenance fees, Expired due to failure to pay maintenance fee.

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