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INDEX

 

FOREWORD.. 0

HISTORICAL CONSIDERATIONS. 0

CONCEPT AND DEVELOPMENT GOALS. 1

THE NEVIS PROTOTYPE SPECIFICATIONS. 2

STRUCTURE OF THE ENGINE SHAFT AND ITS CAM.. 4

STRUCTURE OF THE PISTON.. 5

STRUCTURE OF THE COMBUSTION CHAMBER.. 6

STRUCTURE OF THE EXHAUST VALVE. 7

STRUCTURE OF THE EXHAUST TIMING SYSTEM.. 9

STRUCTURE OF THE ACCELERATOR.. 11

STRUCTURE OF VARIABLE PHASE. 11

STRUCTURE OF THE VARIABLE COMPRESSION RATIO.. 11

CYCLE TIMING DIAGRAM AND LOADING THE ENGINE. 12

VIBRATIONS AND BALANCING ASPECTS. 13

INJECTION.. 13

COOLING SYSTEM AND THERMAL ASPECTS. 14

LUBRICATION SYSTEM.. 14

ENVIRONMENTAL CONSIDERATIONS. 14

NEVIS PREROGATIVES AND GENERAL CONSIDERATIONS. 15

 

 

 

NEVIS is a ground-breaking internal-combustion engine, and more particularly an engine concept that comprises an innovative exhaust valve and intake system, hence its name NEVIS (New Exhaust Valve and Intake System).

In illustrating the concepts behind the NEVIS engine, this document uses published data from the field of mechanical engineering as well as test results derived from proven engines.

In terms of the fluid dynamic characteristics of the NEVIS engine, time and cost has limited the numeric data currently available.  What has been set out in this document has been derived through simplified mathematical modeling.

 

Only four types of engines have been commercialized on a large scale in the history of engines: the four-stroke engine, the two-stroke engine, the Wankel engine and the gas turbine. Many other engines and power sources have been studied and tested such as the electric engine, the steam engine, the Stirling engine, the fuel-cell engine, hybrids and engines operating with compressed air, but the current stage of their development does not allow these alternatives to adequately compete with the main four internal-combustion engines because of excessive production costs, inefficiency or inferior functionality.

In the 1970s, the gas turbine seemed capable of replacing the traditional four-stroke engine within the automotive sector because of its simplicity and contained dimensions. In aeronautical applications, the gas-turbine engine showed even better efficiency than reciprocating engines: it was durable and powerful, produced little vibration and operated in a relatively clean manner. On the other hand, acceptable efficiency was obtainable only if a very high temperature could be reached in the combustion chamber. Accordingly, it was necessary to build the turbine with special materials, too expensive for large-scale automotive production.

The success of the Wankel engine, that possesses similar characteristics to the gas turbine without its prohibitive costs, has been hindered by its modest fuel efficiency and durability only recently improved. Nevertheless, it continues to be used in those applications where fuel consumption is not the main concern <!--

.

Until a few years ago the two-stroke engine had a large number of defects, such as high fuel consumption, excessive emissions and irregular functioning at low rpm or idle speeds. However, recent advances have led to very respectable levels of efficiency and functionality along with dimensions that are almost half the size for the same power output. A good example is provided by AVL two-stroke diesel engine[1] with a controllable exhaust timing system.

 

The following goals were pursued in the development of the NEVIS engine:

a)     Reduction in wasted energy from the exhaust as well as from heat radiation

b)     Improved efficiency at all rpm and power loads

c)     Optimal combustion for improved consumption and performance as well as reduced emissions

d)     Application versatility (aeronautical, automotive, nautical, etc.)

e)     Fuel versatility (gasoline, diesel, hydrogen and biofuels)

f)      Engine block modularity allowing for a wide range of power options

g)     Design simplicity excluding the need for complex or expensive technology and precious materials

h)     Compactness and reduced weight allowing for easy assembly and maintenance

All these goals were taken into account in developing the NEVIS engine and have been applied through the adoption of five key concepts inherent in the engine’s design:

1)     The first concept incorporated within the NEVIS engine relates to a method conceived and experimented by Kadenacy to obtain the scavenging of a two-stroke engine by means of the inertia of the air found in the intake duct and withdrawn by the depression existing in the combustion chamber immediately after the exit of exhaust gases. This method provides considerable advantages in terms of efficiency and overcomes the need to use turbines or compressors generally implemented for scavenging needs.

2)     Importantly, the second concept included within the engine addresses the serious limitations of the Kadenacy effect that is typically only useful within a very small range of rpm. To resolve this issue, the NEVIS engine incorporates a controlled annular exhaust valve of ample size. This exhaust valve allows for variable duration and phasing of its opening by varying the amount of residual pressure remaining from combustion expansion and thus giving the opportunity to correctly phase the scavenging at all rpm’s and loads. At the conclusion of the scavenging phase, the quantity of air that must be kept in the combustion chamber can also be regulated for the varying load demands of the subsequent combustion. Consequently, a new cycle has been implemented within the NEVIS engine. This new cycle allows partial loads to have an expansion stroke greater than the compression stroke like the Miller cycle but with the advantages of a two-stroke cycle. In contrast to what happens with butterfly throttling in the intake duct, the air is free to enter copiously into the combustion chamber with a better fluxing efficiency, thus providing an optimal scavenging even at partial loads and at minimum rpm.

3)     The third concept is based on the adoption of a special shaft for the transformation of the alternate motion of the pistons into rotary motion. This shaft is a sort of sinusoidal camshaft similar to those adopted in engines with cylinders arranged coaxially around the shaft (see the DYNACAM 12- cylinder engine below). However, the new shaft differs in many aspects. First, it has reduced mass and dimensions. Furthermore, it allows for very low average piston velocities with the cam providing for constant acceleration and deceleration of the piston along with the capability of allowing a brief full stop at both top and bottom dead centers in order to provide more time for combustion and scavenging. The shaft incorporated within the NEVIS engine also provides the ability to complete three combustion cycles within a single shaft revolution. 

 

 

NEVIS BP compet 4

The DynaCam engine, an updated design of

this is now called the Axial Vector Engine

 

4)     A variable compression ratio is the forth concept inherent within the NEVIS engine. This is made possible at all rpm and power loads by the simple regulation by of an annular screw element within the shaft itself - unlike the complicated mechanisms necessary in traditional engines to achieve this capability.

5)     The fifth concept incorporated within the NEVIS engine is the adoption of annular pistons which enhance the engine’s thermal efficiency and allow for a light and compact structure as well as a rational integration of the engine’s other key concepts.

 

THE NEVIS PROTOTYPE SPECIFICATIONS

 

 

 

Tech Nevis 3 way view of NEVIS engine

 

 

1st NEVIS Prototype

Cylinders

 

2

Displacement

 

1,000 cc

Power density Kw/L

 

190.0

Bore

 

80mm internal - 178 mm external

 

HP/Kw

 

  Estimated:     250/187 »  @ 2.000 rpm

Average piston velocity

 

7.5 meters/second

Engine Block

 

Steel /aluminum

Weight

 

80kg

Dimensions

 

64 x 36

Power/Weight ratio (Kw/kg)

 

2.38

Compression ratio

7:1  to  38:1

Injectors per cylinder                                 

3

Sparkplugs per cylinder                              

3

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Tech Nevis shaft and 3 lobed disk

Triple-lobed disk attached to the engine

shaft of the cylinder block

 

The shaft is hollow and has anterior and external grooves along with posterior and interior ones. One groove allows the joining to the shafts of other modular engine units that may be added. A substantially cylindrical support coaxially connected to the engine shaft, via respective grooves, hastwo protrusions encompassing it with a cyclic undulated profile. Between the two protrusions operate three couples of ball bearings attached to three supports of an annular piston;  when they are pushed by the pistons on the inclined parts of the profiles the resultant forces cause the rotation of the profile <!---->support, and therefore of the engine shaft.

Conversely, when it is the support on the engine shaft to set the ball bearings in alternate motion  through its rotation, the ball bearings will follow the constant accelerations and decelerations caused by the undulations of the profiles that, by the way, are flat at their vertices to allow the pistons to briefly stop at the dead points.  One of the two profiles is used to push and the other to call back the ball bearings depending on whether it is the engine shaft to drive the pistons’ motion or visa versa.  Likewise, the ball bearings invert their task to push and to decelerate the piston with every stroke.

The piston velocities and accelerations are represented in the graphic below where, for simplicity, only one operative cycle has been considered, while in reality the cycles are three for every revolution.

 

 

 

 

            Tech Nevis three way view of piston

Side, Top and Bottom views of the NEVIS piston

 

Tech Nevis piston with bearing on lobed disk

Bearing at the base of the annular piston running along triple-lobed disk

 

The piston is structured such that its top surface can be interchanged in order to allow for the possibility of future variations of the NEVIS engine to have different types of combustion; i.e. either spark ignition or compression ignition in which a thicker piston top and cavities would be used to allow correct combustion.

An internal thread, close to the external segments,  enables a secure and easy assembling of the two possible tops; the blocking is ensured by two bolts opposing each other on the thread to prevent  unscrewing (the prototype piston crown was forced into its position after being cooled in liquid nitrogen).

The interchangeable crown of the piston can be of aluminum, but the structural elements of the piston are best suited for materials like steel which have the advantage of restricted expansion and of greater strength of the cavities for the segments that are often subjected to wear. Furthermore, the robustness required for the support of the ball bearings would be difficult to achieve if it was made of aluminum.

The function of the cylindrical surrounding wall of the piston is to be considered as structural support for the annular piston, or as an obstruction of intake ports to avoid oil leakage from the basement, but no longer as a surface able to contain the lateral pressures caused by the traditional connecting rods that here have been eliminated together with all balancing problems.

While the external segments are traditional, the two <!--

-->internal elastic rings of the piston obviously tend to contract towards the inside; their hardened face is also internal and they require accurate definition and experimentation.

The annular piston  is subject to forces that cause it to rotate on its axis when the profiles of the cam engage the ball bearings to move. To solve this problem, a further 6 small ball bearings have been appropriately inserted on the walls of the basement block to contrast the guides at the sides of the   of the piston ball bearings support, the guides force the piston only in its reciprocating movement .

A thermodynamic analysis of a the annular piston has been carried out by the University of Catania to provide the correct structure considering the heat and mechanical stress to be undergone. Nevertheless, a further optimization of the piston weight is achievable while maintaining the pistons necessary level of strength.  

 

 

Tech Nevis 3d open view cross section Small

 

One of the most serious limitations of the normal two-stroke engines is due to the dimensions of the of the intake and exhaust ports that have very modest space on the cylinder walls. In annular chamber of the NEVIS, the total surface of the intake can be 3-4 times larger, because intake ports can be distributed along the entire lower part of the larger cylinder wall of the chamber, being  the exhaust port located in the high part of the cylinder. The annular exhaust port is even larger than the intake.  To this must be added the fact that the piston stops at the bottom dead point holding the intake ports  completely open for a certain period.  

The combustion chamber was designed in order to have unidirectional scavenging to achieve an efficient fluxage and a uniform distribution of temperature, which, together with the cooling of the internal and external cylinders of the chamber, helps prevent undesirable deformations of the chamber near the intake ports that typically occur in classic two-stroke engines.

The head is well cooled due to the absence of a traditional valve that normally subtracts space to cooling liquid

To achieve a certain degree of symmetry of in the expansion of the flame front and for security reasons in aeronautical applications, three spark plugs have been positioned on the head at a distance such that the farthest point that has to be reached by each flame front of is 77.5 mm.  This is not a lot but neither is it so short as it is 40% more in comparison with a traditional combustion chamber having a bore of 92mm and with a spark plug positioned in the center. Nevertheless, this difference has little importance considering that, due to the standstill of the piston, the flame front has almost triple the time to cover the 77.5 mm of distance (comparing the duration of the spark advance with a four-stroke engine, it is like having 150° instead of 60° of engine shaft rotation). The spark plugs used are of small dimension and commercially available.

Near each spark plug there is a fuel injector to allow a good spray and a good ignition anywhere in the chamber. The additional cost of a spark plug and two injectors per cylinder is compensated by the fact that a single annular piston realizes in the same amount of time a number of operative cycles comparable to four normal pistons, as later explained in greater detail.

 

The NEVIS exhaust valve operates by closing an annular fissure a few millimeters high; in the prototype this is 4.5 mm.  Accordingly, its shape is annular and it lifts and it shuts down like a guillotine from the point of contact with the cylinder toward the engine head and vice versa.

Like the annular piston, it involves less inertia to complete a lift which is half that of a traditional valve lift. Its larger mass, due to considerable diametrical dimensions, is distributed on 6 short stems symmetrically distant in order to avoid undesired flexion of the ring that is, in any case, lighter than 6 traditional valves.

 

NEVIS Exhaust valve

 

 

The sealing of the annular valve has to be ensured at the top with an internal boarded edge of the valve that lies on another boarded edge created on the engine head, where a thin trapezoidal spring ensures the desired sealing due to its shape and elasticity. For the realization of this trapezoidal spring, it was necessary to choose a material also capable of retaining its elastic properties at relatively high temperatures since as it can be affected by the blow-by of gases despite being protected within the boarded edge of the head.

The shape of the trapezoidal spring must ensure that the valve has a hermetic closure variable in height, considering that it is not possible to have a perfect matching of the head with the cylinder block and that the valves are integral with the head; if the coupling is not strictly accurate leaks may occur from the superior edge of the valve, or <!--

-->if the head is too distant from the cylinder block, leaks would occur from the lower part of the valve that is not able to close the fissure completely, as it already knocked against the upper edge of the head. With the trapezoidal spring mentioned before such problems are avoided, considering that the amplitude of the spring flexion will be higher than the amplitude of the coupling tolerance of the head with the cylinder block.

 

 

Tech Nevis sealing ring of exhaust valve

Sealing Ring of Exhaust Valve

 

In any case, the spring requires small oscillations and has to withstand a relative amount of mechanical strain; it can therefore be realized with a thin section that, together with the ample diameter, will not require elevated pressure to obtain the desired vertical deformation. The edge where the trapezoidal spring lies is removable from the top of the cylinder head to allow the disassembling of the valve.

The lower part of the valve presents no sealing problems, as it can be considered like a valve with a very large diameter; a traditional coupling is therefore easily created with the point of contact between the valve and the higher part of the cylinder block with an inclination of the edge of contact of 30-45 degrees. Of course, the contact surface between the valve and the cylinder will be covered with material similar to that of traditional valve seals.

Traditional exhaust valves have a very serious disadvantage: they open towards the inside of the combustion chamber and struggle against the normal outflow of exhaust gases which, after having increased the valve temperature, burn the stems too. This often leads to the necessity of using more resistant materials (chromium silicon steel, austenitic steel with a high content of nickel chromium) or realizing complex parts, such as hollow valves or parts partially composed of metallic sodium or <!--

-->lithium or potassium salts that improve the heat transmission from the head to the stem of the valve.

The temperatures that can be reached are very high in comparison to those of the intake valves:   the combustion chamber is therefore destined to have considerably different temperatures in the two respective areas, with all the consequences this entails for pre-ignition.

The NEVIS exhaust system, avoids these problems in terms of the outflow of exhaust gases; in fact, for the greater part of the expulsion of gases, the “guillotine” valve is well protected in its position above the exhaust fissure. For this reason, it is not exposed to exhaust gases and it does not hinder their flow.

The small quantity of heat that may be absorbed when it is closed is easily drawn through the stems and the lower edge that is close to the cooling liquid.

Six radial deflectors gently direct the exhaust gases toward the duct that collects the exhaust in order to utilize in the best possible way the kinetic energy of the exhaust.

 

 

Tech Nevis exhaust views

Exhaust assembly

 

 

 

In a future version of the NEVIS engine, the closure of the valve will be operated by means of a desmodromic timing distribution not disclosed here because object of a new patent request.

The current system to recall the valve in the NEVIS engine utilizes good-sized springs with a reduced number of spires that are calibrated in order to provide sufficient pressure for the sealing in its resting position and sufficient strength to bring down the valve after the lift and avoid detachment of the roller tappets from the cams.

The roller tappets for the annular valve consist of three ball bearings; each ball bearing is pivoted to a structure whose top side holds a recalling spring; the same axle of each ball bearing has room to join two rocker arms on each side connected with the two relative stems of the valve to be lifted.

 

Tech Nevis Image of Bearing and Rocker Arm of Exhaust Valve System

Image of Bearing and Rocker Arm of Exhaust Valve System

 

 

If two stems are lifted at the same time by one roller tappet, then the lifting of the valve can be effectuated with three cams acting on three roller tappets. 

The adoption of rockers helps eliminate the vibrations caused by the alternate motion of the valve.

The stems are very short and being fitted, but not welded, to a rather cold valve, they shouldn't be subject to appreciable lengthening when the engine’s operating temperature rises. Anyhow, their elongation does not cause the roller tappets to come close to the cams , but to draw away from them. For this reason the adjustment of the roller tappets is not necessary and the initial positioning has to be done by putting the roller tappets in contact with the surface of the disc or flat support of the cams that lies below , obviously in the point where it's flat and not where the cams are located.

 

 

 

 

Tech Nevis Unassembled accelerator

Unassembled accelerator

 

 

To vary the loading of the engine, it is necessary to vary the duration of the exhaust opening: this is possible through the special cams illustrated above. They are free to slide along the perimeter of their support that has an ample diameter in order to allow the three cams a sufficiently extended area to develop on the plane along the perimeter.

The regulation of this slide is obtained with a “regulating cylinder” that has internal and external helicoidal grooves and is located coaxially between the cylindrical part of the support of the cams and the concentric cylindrical part of the sliding cams. They are coupled via their respective helicoidal grooves; consequently moving back and forth the “regulating cylinder” it is possible to obtain the desired sliding of the cams. Although the “regulating cylinder” rotates at the same engine rpm, it needs to be supplied with a ball bearing fixed on its edge that can be grabbed while rotating This ball bearing has three protrusions on the external ring that are inserted in inclined fissures of two other concentric cylinders, one cylinder being fixed to the cover of the head, the other one free to rotate on its axis to solicit, with the edges of its contrasting fissures, each ball bearing protrusion for a lift or a lowering of the “regulating cylinder”. The external cylinder, free to rotate, has teeth on its lower edge engaged with a smaller gear that has an axle to transmit the rotation to the external part of the block, allowing the adjustment of the accelerator through extended devices.

 

Like the accelerator, the timing of the lifting phase is variable.  The NEVIS engine achieves this by varying the angular position of the support of the cams to the coaxial engine shaft.