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  2. Spray tower - Wikipedia

    en.wikipedia.org/wiki/Spray_tower

    Liquid-to-gas ratio (L/G) Liquid-inlet pressure (p L) Removal efficiency: Applications: Gases: 1.3–7.6 cm of water 0.07–2.70 L/m 3 (0.5–20 gal/1,000 ft 3) 70–2800 kPa 50–90 + % (high efficiency only when the gas is very soluble) Mining industries Chemical process industry Boilers and incinerators Iron and steel industry Particles

  3. Spray (liquid drop) - Wikipedia

    en.wikipedia.org/wiki/Spray_(liquid_drop)

    A spray is a dynamic collection of drops dispersed in a gas. [1] The process of forming a spray is known as atomization. A spray nozzle is the device used to generate a spray. The two main uses of sprays are to distribute material over a cross-section and to generate liquid surface area.

  4. Calcium oxide - Wikipedia

    en.wikipedia.org/wiki/Calcium_oxide

    Calcium oxide (formula: Ca O), commonly known as quicklime or burnt lime, is a widely used chemical compound. It is a white, caustic, alkaline, ...

  5. Dust collector - Wikipedia

    en.wikipedia.org/wiki/Dust_collector

    Spray-tower scrubber wet scrubbers may be categorized by pressure drop as follows: Low-energy scrubbers (0.5 to 2.5 inches water gauge - 124.4 to 621.9 Pa) Low- to medium-energy scrubbers (2.5 to 6 inches water gauge - 0.622 to 1.493 kPa) Medium- to high-energy scrubbers (6 to 15 inches water gauge - 1.493 to 3.731 kPa)

  6. Vermiculite - Wikipedia

    en.wikipedia.org/wiki/Vermiculite

    When vermiculite is used alone, seedlings should be fed with a weak fertilizer solution when the first true leaves appear, e.g. with one teaspoon of 5-10-5 soluble fertilizer per US gallon of water (1:768 ratio), gradually increased to one tablespoon (1:256 ratio) when transplanting. [7]

  7. Liquid-propellant rocket - Wikipedia

    en.wikipedia.org/wiki/Liquid-propellant_rocket

    Liquid rocket engines have tankage and pipes to store and transfer propellant, an injector system and one or more combustion chambers with associated nozzles.. Typical liquid propellants have densities roughly similar to water, approximately 0.7 to 1.4 g/cm 3 (0.025 to 0.051 lb/cu in).

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