TOUR ENGINE
TECHNOLOGY

Turning our superior thermal management strategy into efficiency gains and industry breakthroughs.

THE TOUR ENGINE IS A PATENTED, SPLIT-CYCLE, INTERNAL COMBUSTION ENGINE THAT STANDS TO DELIVER SUBSTANTIAL EFFICIENCY GAINS THROUGH SUPERIOR THERMAL MANAGEMENT

Unlike current combustion engines, which use the same cylinder for all four strokes (intake, compression, combustion, and exhaust), Tour’s patented engine design splits the conventional 4-stroke cycle between two cylinders: the compression-cylinder hosts intake and compression, and the expansion-cylinder hosts combustion and exhaust.

A PROPRIETARY CROSSOVER VALVE IS USED TO TRANSFER THE COMPRESSED

CHARGE FROM THE COMPRESSION-CYLINDER TO THE EXPANSION-CYLINDER. 

This thermal management strategy reduces the magnitude of the two major efficiency losses in

conventional 4-stroke engines – heat loss to the coolant/oil and exhaust energy loss.

The end result is a thermally optimized engine that advanced computer simulations and working prototypes suggest can be as much as 30% more efficient; dramatically reducing both fuel costs and noxious emissions. Better still, because Tour Engines employ the same “block and piston” architecture that has been at the heart of ICEs for more than a century, they will be inexpensive to manufacture, adopt and maintain.

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SUPERIOR THERMAL MANAGEMENT

The Tour split-cycle engine implements a superior thermal management strategy that reduces the magnitude of the two major thermal losses in conventional 4-stroke engines – heat loss to coolant/oil and exhaust energy or enthalpy loss.

The Tour cycle separates the cold and hot portions of the full thermodynamic cycle to separate cylinders, enabling less heat loss to both the induction/compression and combustion/exhaust strokes

PROPRIETARY TRANSFER VALVE

Measured pressure traces from the 1 kW Tour engine developed with support of the ARPA-E GENSETS program. 

To assist with following the Tour cycle, the upper section of the illustration shows the combustion chamber location relative to the input port (IP) and exit port (EP). More specifically, it shows: (1) the compression cylinder coupled to the combustion chamber via the IP, (2) the combustion chamber isolated from IP and EP, and (3) the combustion chamber coupled via the EP to the top of the expansion cylinder.
 
The lower section of the illustration represents three measured pressure traces at a spark timing of -6°ATDC. EXP_CYL and at an engine speed of 1600 rpm as a function of the expansion cylinder crank angle: (1) the blue line represents the measured in-cylinder pressure in the compression cylinder (cold cylinder; with the compression stroke from about -180°ATDC EXP_CYL to about -5°ATDC EXP_CYL and the intake stroke from -5°ATDC EXP_CYL to about +180°ATDC EXP_CYL ), (2) the red dashed line represents the measured in-cylinder pressure in the combustion chamber across a limited range (from -45°ATDC EXP_CYL to +45°ATDC EXP_CYL ), and (3) a green line that represents the measured in-cylinder pressure in the expansion cylinder (hot cylinder; the exhaust stroke from about -180°ATDC EXP_CYL to about -20°ATDC EXP_CYL and the power (expansion) stroke from 0°ATDC EXP_CYL to about +180 ° ATDC EXP_CYL ).
 
It is important to note that between -45°ATDC EXP_CYL and about -8°ATDC EXP_CYL , the blue and red dashed lines almost coincide as there is very little restriction (pressure drop) to the flow between the compression cylinder and the combustion chamber. Similarly, between +10°ATDC EXP_CYL to about +45°ATDC EXP_CYL , the red dashed lines and the green line almost coincide as there is very little restriction (pressure drop) to the flow from the combustion chamber into the expansion cylinder.

CLEANSHEET ENGINE DESIGN

A clean sheet engine has been designed, built and is currently being tested 

Based on detailed system simulations (GT-Power), first performed by Tour Engine and independently confirmed by Wisconsin Engine Research Consultants (WERC, which are a subrecipient of this project), the engine in this project has been designed with an expansion ratio of nearly two times the compression ratio and each cylinder has been fitted with a dedicated cooling circuit to characterize and subsequently minimize the heat losses of the engine. The combination of these two features provides the theoretical basis for significant efficiency gains of the Tour split-cycle over conventional engines.

DEVELOPED IN SAN DIEGO

Tour Engine built a state-of-the-art engine development and test facility in San Diego.

INCREASED THERMAL EFFICIANCY

Increase thermal efficiency based on first principle on 1D computer simulations

The efficiency of the split-cycle approach is significantly improved by over-expanding the gas in the Expansion-Cylinder (as in the Atkinson cycle for naturally aspirated engines and the Miller cycle for forced induction engines), which has the two-fold benefit of increasing the mechanical work extracted and lowering the average gas temperature at the Expansion-Cylinder (over expansion has an advantage also of lowering the temperature differential driving the heat rejection to the Expansion-Cylinder. See “superior thermal management strategy” above).

The Figure below (Panel A) depicts indicated thermal efficiency (ITE) results at a fixed speed of 2400 rpm from GT-Power simulations for three engine configurations: a 2-cylinder baseline 4-stroke engine with 1000 cc (blue, solid line), an Atkinson cycle engine (green, solid line) and various Tour cycle engines (dashed lines). A symmetric Tour engine (red, dashed line) with 1000 cc (500 cc compression/500 cc expansion) has only a slight advantage over the baseline but asymmetric (over-expanded) Tour engines gain a significant advantage up to 1500 cc (500 cc compression/1000 cc expansion).

Combustion strategies similar to those used in the Atkinson cycle enabling a 13:1 compression ratio would further increase the efficiency of the Tour cycle (orange, dashed line).  The results at 2400 rpm suggest that overexpansion of engines with the above stated displacements can increase indicated thermal efficiency (ITE) relative to the baseline by up to 19%, and relative to the Atkinson cycle by up to 13% depending on the specific engine configuration. In order to simulate the performance maps (shown with ITE contours) for the baseline engine (Panel B) and the over-expanded Tour engine (Panel C), a throttle was added to the models. The performance maps show a higher ITE for the Tour engine and an expanded high efficiency region across a wide range of engine speed, including low engine speeds.  This is advantageous for increasing engine durability while maintaining high efficiency.

POWER STROKES

The power stroke in the Expansion-Cylinder and the intake stroke (of the next cycle) in the Compression-Cylinder occur concurrently.

Hence in a pair of Tour engine cylinders, two 4-stroke cycles are being executed at the same time. In this respect, the Tour engine and a conventional four-stroke twin engine have exactly the same number of power strokes per crankshaft revolution. For example, a conventional twin engine will have one power stroke in each cylinder, while the Tour engine will have two power strokes in the Expansion-Cylinder and none in the Compression-Cylinder.

EARLY DEVELOPMENT

As demonstrated from early prototypes and modeling, TEI has built at its R&D facility in Israel two functional prototype engines that implement the Tour cycle.

The first prototype, Prototype I, used two identical off-the-shelf 50cc Honda GXV50 engines, one for the Compression-Cylinder and the other for the Expansion-Cylinder. Prototype I proved the mechanical feasibility of the Tour engine design and showed for the first time that the crossover valve can be built in such a way that there is very little energy loss due to the transfer of the working fluid from the compression cylinder to the expansion cylinder.

Tour Engine Prototype I

  • Design. Two Honda GXV50 engines were connected with the crossover valve positioned at the interface between the two cylinder heads.
  • Assembled. Notice that over 85% of the prototype parts are taken from off-the-shelf engines.

The second prototype, Prototype II, became operational on 2012 and is based on two identical off-the-shelf 190cc Briggs and Stratton engines.

Prototype II was designed primarily as a platform to test, in a modular fashion, various crossover valve designs. This prototype was later modified to implement an over-expanding of the gas in the Expansion-Cylinder (as in the Atkinson cycle), and a movie of this prototype being tested in our R&D facility in Israel can be seen here.

REIMAGINE THE FUTURE WITH TOUR ENGINE

Tour is backed by sophisticated technology investors and has won grants from both the US DOE’s ARPA-E and The California Energy Commission (CEC) and Israeli (DOE) governments. Tour has also been issued 48 patents (US and International) with several more pending.

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