The sleeve valve is a type of valve mechanism for piston engines, distinct from the more common poppet valve. Sleeve-valve engines saw use in a number of pre-World War II luxury cars, sports cars, the Willys-Knight car and light truck, the British Daimler and French Avions Voisin luxury cars, also used the same Willys-Knight double-sleeve system. They subsequently fell from use due to advances in poppet-valve technology (sodium cooling) and to their tendency to burn a lot of lubricating oil or to seize due to lack of it. The Scottish Argyll company used its own, much simpler and efficient, single-sleeve system in its cars, a system which, after extensive development, saw substantial use in aircraft engines of the 1940s, such as the Napier Sabre and Bristol Hercules and Centaurus, only to be supplanted by the jet engine.

Contents 1 Description 1.1 Types of sleeve valve 2 Advantages/disadvantages 2.1 Advantages 2.2 Disadvantages 3 History 3.1 Charles Yale Knight 3.2 Burt-McCollum 4 Modern usage 5 Steam engine 6 See also 7 References 8 External links

[edit] Description

A sleeve valve takes the form of one or more machined sleeves. It fits between the piston and the cylinder wall in the cylinder of an internal combustion engine where it rotates and/or slides, ports (holes) in the side of the valve(s) aligning with the cylinder's inlet and exhaust ports at the appropriate stages in the engine's cycle.

[edit] Types of sleeve valve

The first successful sleeve valve was patented by Charles Yale Knight, and used twin alternating sliding sleeves. It was used in some luxury automobiles, notably Daimler, but was noted for its high oil consumption.^[1]

The Burt-McCollum sleeve valve, as used by the Scottish company Argyll for its cars,^[2] and later adopted by Bristol for its radial aircraft engines, used a single sleeve which rotated around a timing axle set at 90 degrees to the cylinder axle. Mechanically simpler and more rugged, the Burt-McCollum valve had the additional advantage of reducing oil consumption (compared to other sleeve valve designs), while retaining the rational combustion chambers and big, uncluttered, porting area possible in the Knight system.

A small number of designs used a "cuff" sleeve in the cylinder head instead of the cylinder proper,^[3] providing a more "classic" layout compared to traditional poppet valve engines. This design also had the advantage of not having the piston within the sleeve, although in practice this appears to have had little practical value. On the downside, this arrangement limited the size of the ports to that of the cylinder head, whereas in-cylinder sleeves could have much larger ports.

[edit] Advantages/disadvantages

[edit] Advantages

The main advantages of the sleeve valve engine are:

• An increase in volumetric efficiency due to very large port openings, Sir Harry Ricardo demonstrated also a better mechanical efficiency. An additional advantage of the system is that the size of the ports can be readily controlled. This is of importance when an engine runs over a wide range of RPM, as the speed at which air can enter and exit the cylinder is defined by the size of the duct leading to the cylinder and varies according to the cube of the RPM. In other words, at higher RPM the engine typically requires larger ports that remain open for a greater proportion of the cycle, something that is fairly easy to arrange with sleeve valves, but difficult in a poppet valve system.

• The single sleeve valve offers good exhaust scavenging and controllable swirl of the inlet air/fuel mixture; when the intake ports open, the fuel air mixture can be made to enter tangentially to the cylinder. This helps scavenging when exhaust/inlet timing overlap is used and a wide speed range required, whereas poor poppet valve exhaust scavenging can dilute the fresh air/fuel mixture intake to a greater degree, being more speed dependent (relying principally on exhaust/inlet system resonant tuning to separate the two steams). Greater freedom of combustion chamber design (few constraints other than the spark plug positioning) means that fuel/air mixture swirl at TDC can also be more controlled allowing improved ignition and flame travel which as demonstrated by Ricardo, at least one extra unit of C.R. before detonation c.f. the poppet valve engine.

• The combustion chamber formed with the sleeve at the top of its stroke is ideal for complete, detonation-free combustion of the charge, as it does not have to contend with compromised chamber shape and hot exhaust (poppet) valve(s).

• No springs are involved in the sleeve valve system, therefore the power needed to operate the valve remains largely constant with the engine's RPM meaning that the system can be used at very high speeds with no penalty for doing so. A problem with high-speed engines which use poppet valves is that as engine speed increases, the speed at which the valve moves also has to increase. This in turn increases the loads involved due to the inertia of the valve, which has to be opened quickly, brought to a stop, then reversed in direction and closed and brought to a stop again. Large valves that allow good air-flow have considerable mass and require a strong spring to overcome the opening inertia. At some point, the valve spring reaches its resonance frequency, causing a compression wave to oscillate within the spring, which in turn causes it to become effectively weaker and therefore unable to properly close the valve. This valve float can result in the valve not closing as quickly as the cam profile and it may strike the top of the piston as it rises. In addition, camshaft, pushrods, and valve rockers can be dispensed with in a sleeve valve design, as the sleeve valves are generally driven by a single gear powered from the crankshaft. For an aircraft engine this produced desirable reductions in weight and complexity.

• Another advantage of the sleeve valve in early automotive applications (Knight engine) was longevity. Prior to the advent of leaded gasolines, poppet-valve engines typically required grinding of the valves and valve seats after 20,000 to 30,000 miles (32,000 to 48,000 km) of service. Sleeve valves did not suffer from the wear and recession caused by the repetitive impact of the poppet valve against its seat. Sleeve valves were also subjected to less intense heat buildup than poppet valves, owing to their greater area of contact with other large metal surfaces. In the Knight engine, carbon build-up actually helped to improve the sealing of the sleeves, the engines being said to "improve with use", in contrast to poppet valve engines, which lose compression and power as valves and valve stems/guides wear. Due to the continued motion of sleeve (Burt-McCollum type), the high wear points linked to poor lubrication in the TDC/BDC of piston course are suppressed, therefore also rings and cylinders lasted much longer.

• Other big advantages includes the fact the cylinder head is not required to house valves, therefore allowing the sparkplug to be placed in the best possible location for efficient ignition of the combustion mixture. For very big engines, where flame propagation speed limits both size and speed, the swirl induced by ports and described by Ricardo can be an additional advantage.

Most of these advantages were evaluated and established during the 1920s by Sir Harry Ricardo, possibly the sleeve-valve engine's greatest advocate. He conceded however, that some of these advantages were significantly eroded as fuels improved up to and during World War II, and sodium-cooled exhaust valves were introduced in high output aircraft engines.

[edit] Disadvantages

The sleeve valve's one major disadvantage is that perfect sealing is difficult to achieve. In a poppet valve engine, the piston possesses piston rings (often at least 3 and sometimes as many as 8) which form a seal with the cylinder bore. During the "breaking in" period (known as "running-in" in the UK) any imperfections in one are scraped into the other, resulting in a good fit. This type of "breaking in" is not possible on a sleeve valve engine, however, because the piston and sleeve move in different directions and in some systems even rotate in relation to one another. Unlike a traditional design, the imperfections in the piston do not always line up with the same point on the sleeve. In the 1940s this was not a major concern because the poppet valves of the time typically leaked appreciably more than they do today, so that oil consumption was poor in either case.

The high oil consumption problem associated with the Knight double sleeve valve was fixed with the Burt-McCollum single sleeve valve, as perfected by Bristol. At TDC, the single sleeve valve rotates in relation to the piston. This prevents boundary lubrication problems, as piston ring ridge wear at TDC and BDC does not occur. The Hercules overhaul time was rated at 3,000 hr^{[citation needed]} at wide open throttle. An inherent disadvantage may be that the piston in its course partially obscures the ports, thus making it difficult for gases to flow during the crucial overlap between the intake and exhaust valve timing usual in modern engines. The German engineer Max Bentele, after studying a British sleeve valve aero engine (probably a Hercules), complained that the arrangement required more than 100 gearwheels for the engine, too many for his taste.^[4]

[edit] History

[edit] Charles Yale Knight

In 1901 Knight bought an air-cooled, single cylinder three-wheeler whose noisy valves annoyed him. He believed that he could design a better engine and did so, inventing his double sleeve principle in 1904. Backed by Chicago entrepreneur L.B. Kilbourne, a number of engines were constructed followed by the "Silent Knight" touring car which was shown at the 1906 Chicago Auto Show.

Knight's design had two cast-iron sleeves per cylinder, one sliding inside the other with the piston inside the inner sleeve. The sleeves were operated by small connected rods actuated by an eccentric shaft. They had ports cut out at their upper ends. The design was remarkably quiet, and the sleeve valves needed little attention. It was, however, more expensive to manufacture due to the precision grinding required on the sleeves' surfaces. It also used more oil at high speeds and was harder to start in cold weather.^[5]

Although he was initially unable to sell his Knight Engine in the US, a trip to Europe secured several luxury car firms as customers willing to pay his expensive premiums. He first patented the design in Britain in 1908. As part of the licensing agreement, 'Knight' was to be included in the car's name.

Among the companies using Knight's technology were Gabriel Voisin (in his Avions Voisin cars), Daimler (in their V-12 "Double Six", from 1909-1930), Panhard (1911-39), Mercedes (1909-24), Willys (as the Willys-Knight, plus the associated Falcon-Knight), Stearns, Mors, Peugeot, and Belgium's Minerva company, some thirty companies in all.^[6] Itala also experimented with sleeve valves.

Upon Knight's return to America he was able to get some firms to use his design; here his brand name was "Silent Knight" (1905-1907) — the selling point was that his engines were quieter than those with standard poppet valves. The best known of these were the F.B. Stearns Company of Cleveland, which sold a car named the Stearns-Knight, and the Willys firm which offered a car called the Willys-Knight, which was produced in far greater numbers than any other sleeve-valve car.

[edit] Burt-McCollum

The Burt-McCollum sleeve valve consisted of a single sleeve which was given a combination of up-and-down and partial rotary motion. It was developed in about 1909 and was first used in the 1911 Argyll car. Argyll went out of business after high expenses of a litigation with the Knight patent holders. Its greatest success was in Bristol's large aircraft engines, and was also used in the Napier Sabre and Rolls-Royce Eagle aircraft engines. The single valve system also cured the high oil consumption associated with the Knight double sleeve valve.^[7]

A number of sleeve valve aircraft engines were developed following a seminal 1927 research paper from the RAE by Harry Ricardo. This paper outlined the advantages of the sleeve valve, and suggested that poppet valve engines would not be able to offer power outputs much beyond 1500 hp (1,100 kW). Napier and Bristol began the development of sleeve valve engines that would eventually result in two of the most powerful piston engines in the world, the Napier Sabre and Bristol Centaurus.

Potentially the most powerful of all sleeve-valve engines (that never reached production) was the Rolls-Royce Crecy, V-12 (oddly a 90 degree V angle) two-stroke direct injected force-scavenged (turbocharged) aero-engine of 26.1 litres capacity. It achieved a very high specific output, and surprisingly good SFC - in 1945 the single cylinder test-engine (E65) produced the equivalent of 5,000 HP (192 BHP/Litre) when water injected, although the full V12 would probably have been initially type rated at circa 2,500 hp (1,900 kW). Sir Harry Ricardo, who specified the layout and design goals, felt constantly frustrated during the war with Rolls-Royce's (RR) efforts, he and Tizard finally accepting that if it wasn't assigned to a specific aircraft installation, it wouldn't get the development attention it deserved. He felt a reliable 4,000 HP military rating was on the cards, having been bench-running E65 test engines for many years. Hives & RR focused very much on the Merlin, Griffon and then Eagle and then Whittle's jets, which had a clearly defined production purpose. The original 'Spitfire on steroids' rapid-climbing interceptor concept for the lightweight Crecy, had become an aircraft without a purpose by 1945.

Following World War II the sleeve valve disappeared from use, as the previous problems with sealing and wear on poppet valves had been remedied by the use of better materials, and the inertia problems with the use of large valves were reduced by using several smaller valves instead, giving increased flow area and reduced mass. Up to that point, the single sleeve valve won every contest against the poppet valve hands down in comparison of power to displacement. The difficulty of nitride hardening, then finish grinding the sleeve valve for truing the circularity, may be a factor of its lack of commercial applications.

[edit] Modern usage

The sleeve valve has begun to make something of a comeback, due to modern materials and newer and dramatically better engineering tolerances and construction techniques which produce a sleeve valve that leaks very little oil. However, most advanced engine research is concentrated on improving entirely different designs of internal combustion engine such as the Wankel.

It is rumored that^{[citation needed]}both Mike Hewland (Interview in Car & Driver ca 1975) and Keith Duckworth (of Cosworth F1 racing engine fame) experimented with a single-cylinder sleeve-valve test engine when looking at Cosworth DFV replacements. Hewland claimed obtaining 72 hp (54 kW) from a 500 cc single cylinder engine, with a specific fuel consumption of 170 gr/HP/hr, the engine being able to work on creosote, with no specific lubrication supply for the sleeve, Hewland reported also that the highest temperature measured inside the cylinder not surpassed 150ºC.

A recent SAE paper deals on a high speed, small displacement sleeve valve engine, they have calculated, but not experimentally shown, a higher SFC than the poppet valve alternative, a non surprising result considering the difficulty in obtaining the high intake and exhaust overlapping very fast running engines require.

An unusual form of four stroke model engine to use what is essentially a sleeve-valve format is the British RCV series of "SP" model engines, which use a rotating cylinder liner driven through a bevel gear at the cylinder liner's "bottom", and even more unusually has the propeller shaft emerging from what would normally be the cylinder's "top", at the extreme front of the engine, achieving a 2:1 gear reduction ratio compared to the vertically oriented crankshaft's rotational speed.

[edit] Steam engine

Sleeve valves have occasionally been used on steam engines, for example the SR Leader Class.

[edit] See also

• Sleeve valve engines
• D slide valve
• Piston valve
• Corliss valve

[edit] References

• Arnold E. Biermann & Hermann H. Ellerbrock, Jr: "The design of fins for air cooled cylinders", NACA report Nº. 726, 1939 (can be downloaded from NASA website)

• Aircraft Engine Historical Society -AEHS- publication "Torque Meter", Vol 7, issues 2,3,4.

• Robert J. Raymond: "Comparison of Sleeve and Poppet-Valve Aircraft Piston Engines", AEHS 2005

[edit] External links

Wikimedia Commons has media related to: Sleeve valve engines

• Video showing a cutaway Knight Sleeve Valve Engine
• RCV engine website

v • d • e Heat engines Stroke cycles Two-stroke cycle · Four-stroke cycle · Six-stroke cycle Engine types Coomber · Free-piston · Gas turbine · Iris · Jet · Orbital · Piston · Rocket · Rotary · Split-single · Steam (reciprocating) · Steam turbine · Stirling · Swing-piston · Tschudi · Wankel Valves Cylinder head porting · Corliss · Slide · Manifold · Multi · Piston · Poppet · Sleeve · rotary valve · variable valve timing · camless (solenoid operated valves) Engine configuration Single cylinder · Straight · Opposed · Flat · U · V · W · H · Deltic · Radial · Rotary · Stelzer · Controlled Combustion · Bourke · Split cycle Motion mechanisms Cam · Connecting rod · Coomber rotary · Crank · Crank substitute · Crankshaft · Linkages (Evans · Peaucellier–Lipkin · Sector straight-line · Watt) · Scotch Yoke · Swashplate · Rhombic drive · Double acting/differential cylinder Thermodynamic cycle