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Combustion chamber length

Combustion chamber minimum dimensions from EN 303-3. On the x-axis nominal thermal power in kW, on the y-axis combustion chamber diameter or length in m. Curve aj is combustion chamber length in case smoke exits from the back side of the combustion chamber, while curve aj applies in case smoke inverts the path to the chimney inside the combustion chamber and exits from the front side. Lengths are measured from the burner head where the flame is attached to the bottom of the combustion chamber. Curve b is the combustion chamber diameter (or equivalent diameter in case of a noncircular combustion chamber). [Pg.716]

Combustion chamber length versus nominal thermal power for 74 utility boilers for gas and oil application from different suppliers. The red curve and the equation refers to EN 676 suggest length. [Pg.716]

Honzontal-tube cabin heaters position the tubes of the radiant-section-coil horizontally along the walls and the slanting roof for the length of the cabin-shaped enclosure. The convection tube bank is placed horizontally above the combustion chamber. It may be fired From the floor, the side walls, or the end walls. As in the case of its vertical cylindrical counterpart, its economical design and high efficiency make it the most popular horizontal-tube heater. Duties are 11 to 105 GJ/h (10 to 100 10 Btu). [Pg.2402]

The pyrolysis product gas enters the secondary chamber through a burner that is mounted vertically, enabling flow of the product gas into the combustion chamber, ensuring extended flame length. The treated secondary off gas is scrubbed in a shower and ejected into the atmosphere. [Pg.163]

Other processes that have increased importance at small length scales such as thermal creep (transpiration) and electrokinetic effects are also being considered for use in microcombustors. For example, transpiration effects are currently being investigated by Ochoa el al. [117] to supply fuel to the combustion chamber creating an in-situ thermally driven reactant flow at the front end of the combustor. [Pg.253]

Suppose fuel droplets of various sizes are formed at one end of a combustor and move with the gas through the combustor at a velocity of 30m/s. It is known that the 50-pm droplets completely vaporize in 5 ms. It is desired to vaporize completely each droplet of 100 pm and less before they exit the combustion chamber. What is the minimum length of the combustion chamber allowable in design to achieve this goal ... [Pg.375]

The largest RYUSEI rocket is said to be 18 m in length and weighs around 40 kg (sic). Built in three sections the head or payload section holds sequential fireworks and smoke dragons attached externally, while the combustion chamber is made from split pine logs, gouged out and then re-assembled to make a cylinder. [Pg.57]

Many experimental evidences have been obtained for impinging streams intensifying combustion processes. For example, the results obtained by Enyakin [142] and Enyakin-Dvoretskii [143] from their investigations on the combustion of high sulfur-content oil showed that the oil can burn in impinging streams at a very low excess air factor (as low as 1.02), the number of burners can be decreased, and the length of flame is obviously reduced. The latter result implies that a smaller combustion chamber can be used. [Pg.197]

Drost et al. [129] developed an evaporator combined with a micro scale combustion chamber for homogeneous combustion of hydrocarbons (Figure 2.82). The main focus of the work was to maintain a stable combustion of the fuel avoiding NOx formation. Evaporation tests were carried out under isothermal conditions. Fifty-four parallel channels, 270 pm wide and 1 000 pm deep with a length of20.52 mm, were cut into a copper substrate with a diamond saw. [Pg.374]

A steel jacket furnace is shaped like a vertical tower (see Fig. 115) and is lined with acid resisting and refractory bricks. The overall length is 5120 mm, the outside diameter 800 mm at the top and 1200 mm at the bottom, inside diameter 570 mm at the top and 970 mm at the bottom. 3 (500 kg of chlorine can be treated in furnaces of this type daily. Hydrogen and chlorine are brought to the valves by overpressure of 1 atm. and an overpressure of 0.5 atm. is maintained in the combustion chamber. The gas is drawn off through a side pipe which is 100 mm wide and fixed at the top of the furnace. A small safety membrane is also fitted at the top for the ease of explosion. [Pg.319]

Carbon dioxide concentration appears as a maximum about half-way between the wall and the center of the combustion chamber (Fig 6), This maximum diminishes toward the reaction zone and disappears in the tunnel. The carbon dioxide has practically constant concentration across the reactor tunnel, but this concentration decreases with tunnel length. [Pg.288]

Carbon monoxide appears at the entrance of the combustion chamber close to the wall but quickly disappears. Carbon monoxide reappears again with a pattern very similar to hydrogen in the vicinity of the reaction zone (Fig. 9). Beyond this zone the carbon monoxide concentration is essentially constant across the reactor, with increasing concentration with tunnel length. [Pg.288]

The muffle was a horizontal combustion chamber lined with refractory material. The German Norms for the construction and operation offurnaces for the cremation of human corpse enacted in 1937 prescribed the following minimal measures for such a muffle width 900 millimeter height 900 millimeter length 2500 millimeter.52... [Pg.380]

Figure 2.11 schematically shows the pressure profile which is one factor that influences rocket performance. The length of the arrows shows the contribution of the pressure from inside and outside the walls. While the atmospheric pressure outside is constant, the inside pressure of the combustion chamber is at its largest and decreases in the direction of the nozzle end. The pressure term is proportional to the diameter Ae ... [Pg.60]

FIGU RE 11.3. The asymptotic dependence of the combustion efficiency on the dimensionless chamber length Z2 for various values of the exponent 2 the ordinary Rosin-Rammler distribution (/2 = - 2 " hh /C2 = 1-... [Pg.458]

Since the droplets are all of the same size in our present model, they will all disappear simultaneously at a finite distance from the injector, contrary to the results of Section 11.2. Therefore, instead of focusing attention on the combustion efficiency, we shall attempt to determine the minimum chamber length required for complete combustion (f/ = 100%), which will be denoted by x. ... [Pg.467]

The droplets disappear when cj 0. By setting tr = 0 in equation (84), the chamber length required for complete combustion is found to be... [Pg.471]

FIGURE 11.5. The dimensionless minimum chamber length for complete combustion as a function of the drag parameter p2 for various values of the dimensionless injection velocity Pi (from [52]). [Pg.471]

The furnace shown in jig I aadjig 2 is designed for the combustion of wood chips with a maximum chip length of approximately 5 cm. It is composed of a combustion chamber lopped by a heat-exchanger. [Pg.919]


See other pages where Combustion chamber length is mentioned: [Pg.33]    [Pg.33]    [Pg.926]    [Pg.173]    [Pg.251]    [Pg.243]    [Pg.251]    [Pg.456]    [Pg.344]    [Pg.378]    [Pg.672]    [Pg.1448]    [Pg.37]    [Pg.160]    [Pg.152]    [Pg.483]    [Pg.94]    [Pg.133]    [Pg.212]    [Pg.471]    [Pg.208]    [Pg.322]    [Pg.706]    [Pg.211]    [Pg.376]    [Pg.595]   
See also in sourсe #XX -- [ Pg.340 , Pg.467 , Pg.471 ]

See also in sourсe #XX -- [ Pg.340 , Pg.467 , Pg.471 ]




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Combustion chamber

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