?400hp 3.0l V6 - Infiniti Q60 - 683 - $123,500404hp 3.0l I6 - M2 Competition444hp 3.0l F6 - 991 Carrera GTS - 678456hp 4.0l V8 - AMG GT - 857 - $191,000460hp 6.2l V8 - Corvette Grand Sport - 875 - $243,500471hp 2.9l V8 - Ferrari F40 - 766 - $163,500493hp 3.0l I6 - M4 GTS - 752 - $184,000503hp 2.9l V6 - Giulia Quadrifoglio - 739 - $192,500514hp 4.0l F6 - 991 GT3 RS - 722542hp 5.0l V8 - Porsche Panamera Turbo - 945 - $303,500562hp 3.8l V6 - Nissan GT-R R35 - 857562hp 3.8l V8 - Mclaren 570S - 912 - $288,000567hp 4.4L V8 - BMW X6 M - 890 - $281,500570hp 4.5l V8 - 458 Italia - 789 - $289,000577hp 4.0L V8 - AMG GT R - 883 - $271,500591hp 3.8L V8 - 600LT - 953 - $288,000591hp 4.4l V8 - BMW M5 - 909 - $324,500599hp 3.8l F6 - 991 Turbo S Exclusive - 867600hp 2.0l Hybrid - Polestar - 879 - $299,000600hp 5.2l V12 - DB11 - 1006 - $348,000601hp 5.2l V10 - Huracan - 879 - $349,500640hp 8.4l V10 - SRT Viper GTS - 875 - $380,500646hp 3.5l V6 - Ford GT - 1010 - $361,000710hp 3.9l V8 - 488 Pista - 1072 - $438,000721hp Forged 3.8l V6 - ??? The rotor comprises at least first and second jet assemblies. Producing motive power through the reactive force of jets has long been known. A second air bearing 92 supports the drive shaft 88 of the rotor 36. . Engine Swap in Need for Speed: Heat allows players to remove and replace the engine equipped in any of their owned cars with a different engine. 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. Preferably, the combustion chamber partially extends into the thrust matter plenum 54 of the rotor 36 through the first axial end 70 of the plenum wall 68. FIG. A jet-propelled rotary engine as set forth in. If your old school and use C.I. The stator 38 of the main engine assembly 22 preferably comprises a tubular combustion chamber 96, an annular air plenum 98, a steam passageway 100, and an annular duct 102. Nice, I didn't know that or more specifically, never used that motor in the Lotus. 2,637,166 discloses a turbine in which the reactions of high velocity jets are used to effect rotation of a turbine. Need for Speed: Payback/Performance Parts. 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. Finally, the exhaust matter is discharged from the heat exchanger 32 and the rotary engine 20 via an exhaust pipe. Likewise, as the steam travels in the steam passageways 58, it eventually passes through the steam jet assemblies 42 of the rotor 36 where the velocity of the steam is accelerated via the steam converging region 60 and the steam diverging region 62 to a supersonic velocity of approximately Mach 3.3 as it is discharged from the steam discharge ports 64 of the rotor 36. 6,668,539 and entitled Rotary Heat Engine, and incorporated herein by reference. Like the preferred embodiment of the duct 102 shown in FIG. New; 21:05. ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:INNOVATIVE ENERGY, INC.;REEL/FRAME:030061/0637, Owner name: The thrust matter tubes 52 are preferably round in cross-section and are preferably formed of titanium so as to be lightweight, strong, and heat resistant. FIG. 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. An alternative duct 124 is shown in FIG. The rotary engine is further adapted to combust at least some of the oxygen-fuel mixture in the upstream portion of the combustion region. TRUSTEES OF THE ALICE ANHEUSER BEIMS MOORE IRREVOC, Free format text: Alternatively, oxygen may be added to or used in place of the air being supplied to the rotary engine 20 (air and/or oxygen being referred to as âairâ throughout this specification). Each of the thrust matter passageways 44 is preferably partially defined by a thrust matter tube 52 that extends radially outward from a centrally positioned thrust matter plenum 54 at an angle perpendicular to the rotor axis X and thereafter turns to extend circumferentially about the rotor axis X in a direction opposite that of the designed rotation of the rotor such that the thrust matter discharge ports are configured and adapted to discharge thrust matter in a direction generally tangential to the rotor axis X. The spark wires 106 are utilized to initially ignite the fuel and air mixture. that one is a 444bhp V8 engine. #fix #rpm . The rotary engine is further adapted and configured to channel at least some of the thrust matter formed in the upstream portion of the combustion region through the discharge port of the jet assembly and further comprises a generally annular duct circumscribing the circular path traversed by the jet assembly. PATENT EXPIRED DUE TO NONPAYMENT OF MAINTENANCE FEES UNDER 37 CFR 1.362, Free format text: The rotary engine is further 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. From the annular duct 102, a portion of the super heated steam can optionally be used to hydroxylate the fuel being supplied to the combustion chamber 96 of the stator 38 while the remainder of the super heated steam passes into the central steam tube 78 of the rotor 36. From the minute you enter the garage, you have tons of parts for building and tinkering with your high-performance car. Other features and advantages of the invention will be in part apparent and in part pointed out hereinafter. The central steam tube 78 is attached at one of its axial ends to the end wall 74 of the thrust matter plenum 54 and has an opposite axial end that extends past the first axial end 70 of the cylindrical plenum wall 68. The combustion region is defined at least in part by the rotor and has an upstream portion. 1. Press question mark to learn the rest of the keyboard shortcuts, https://www.carfolio.com/specifications/models/car/?car=88385#a_aerodynamics. A jet-propelled rotary engine as set forth in, the jet assembly is adapted for supersonic discharge of a first jet stream of the thrust matter from the first thrust matter discharge port with the jet stream having a first jet stream centerline as the thrust matter is being discharged from the first thrust matter discharge port; and. . The duct has a generally annular duct diverging region that diverges as it extends radially outwardly. NFS Heat Engine Swap Sources. In one 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. A jet-propelled rotary engine as set forth in. https://nfs.fandom.com/wiki/Need_for_Speed:_Heat/Engine_Swap?oldid=140188. 2,544,420 discloses a combustion chamber used to provide rotational power in a propulsion apparatus such as in driving a propeller shaft. I love the exige a lot my favorite car in the game, I wanted to put a better engine in it than the 616 hp 2.8l flat 6. 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. The air supply assembly 28 preferably utilizes an electrically powered supercharger to provide pressurized air to the main engine assembly 22. brz weights 2-300kg more than the lotusit's not just weight eithercars are balanced weirdsome icon versions need more power to reach max, or get more or less performance with the same enginessome cars start out with similar 'PI' but when upgraded diverges even with similar engines. Thus, the annular converging region 112 and the annular diverging region 114 of the annular duct 102 act to reduce the flow rate of the exhaust matter without generating a strong shock wave in the path of the rotor. As the thrust matter passes through the thrust matter converging region 46 of the thrust matter jet assemblies 40, the velocity of the thrust matter is increased to approximately Mach 1.0 after which the thrust matter passes into the thrust matter diverging region 48 where it is further accelerated and ultimately discharges through the thrust matter discharge ports 50 at a velocity of preferably approximately Mach 2.7. ), TRUSTEES OF THE ALICE ANHEUSER BEIMS MOORE IRREVOC, ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:INNER POINT ENERGY CORPORATION;REEL/FRAME:046990/0054, Method of Pumping Gaseous Matter via a Supersonic Centrifugal Pump, System for the transport of an ore pulp in a line system located along a gradient, and components of such a system, Nozzle Capable of Maximizing the Quantity of Movement Produced by a Two-Phase Flow Through the Relief of a Saturating Flow, Rotation body of nozzle for reaction-type steam turbine, Turbine and liquid separator with such a turbine, Rotary jet, power generation systems and motors including the same, and methods of making and using the same, Micro reaction turbine with integrated combustion chamber and rotor.