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Propeller pitch

Propeller Pitch pitch is the advance of the fluid per revolution on the basis that a propeller is a segment of a screw. Normally "square" pitch is used i.e., a pitch value equal to the propeller diameter. [Pg.454]

Propeller Yes No limitation 0.54 (Npe) - (Np,) --5 45 pitched, four-blade impeller. Fquation is based on limited data with regard to propeller pitch and vessel baffling. Divide hj obtained with this equation by a factor of about 1.3. [Pg.622]

Propeller Pitch =20 Flat Paddle (D/W=4) Propeller Pitch = 0... [Pg.305]

Poddl l/Shoff(D/W = 8) Shrouded Turbin + Stotor Propeller Pitch = 20... [Pg.304]

Figure 10.5. Power number, Np = PgJN3Dsp, against Reynolds number, NR = ND2p/p, for several kinds of impellers (a) helical shape (Oldshue, 1983) (b) anchor shape Oldshue, 1983) (c) several shapes (1) propeller, pitch equalling diameter, without baffles (2) propeller, s = d, four baffles (3) propeller, s = 2d, without baffles (4) propeller, s = 2d, four baffles (5) turbine impeller, six straight blades, without baffles (6) turbine impeller, six blades, four baffles (7) turbine impeller, six curved blades, four baffles (8) arrowhead turbine, four baffles (9) turbine impeller, inclined curved blades, four baffles (10) two-blade paddle, four baffles (11) turbine impeller, six blades, four baffles (12) turbine impeller with stator ring (13) paddle without baffles (data of Miller and Mann) (14) paddle without baffles (data of White and Summerford). All baffles are of width 0.1D [after Rushton, Costich, and Everett, Chem. Eng. Prog. 46(9), 467 (1950)]. Figure 10.5. Power number, Np = PgJN3Dsp, against Reynolds number, NR = ND2p/p, for several kinds of impellers (a) helical shape (Oldshue, 1983) (b) anchor shape Oldshue, 1983) (c) several shapes (1) propeller, pitch equalling diameter, without baffles (2) propeller, s = d, four baffles (3) propeller, s = 2d, without baffles (4) propeller, s = 2d, four baffles (5) turbine impeller, six straight blades, without baffles (6) turbine impeller, six blades, four baffles (7) turbine impeller, six curved blades, four baffles (8) arrowhead turbine, four baffles (9) turbine impeller, inclined curved blades, four baffles (10) two-blade paddle, four baffles (11) turbine impeller, six blades, four baffles (12) turbine impeller with stator ring (13) paddle without baffles (data of Miller and Mann) (14) paddle without baffles (data of White and Summerford). All baffles are of width 0.1D [after Rushton, Costich, and Everett, Chem. Eng. Prog. 46(9), 467 (1950)].
In addition to lubricating the engines, turbine lubricants are also required to lubricate a number of associated systems such as auxiliary power units and constant speed drive units and to act as hydraulic fluids, for instance, in the propeller pitch control units of some turbo-props. [Pg.354]

Curve 5. Propeller pitch = D four baffles each DJJ = 10 olso holds for same propeller in angular off-center position with no baffles. [Pg.145]

Axial flow Propeller, pitched blade turbine, hydrofoils... [Pg.347]

The power number of side-entering propellers depends on the impeller Reynolds number and the pitch. The propeller pitch is defined as the distance traversed by the propeller in one revolution divided by the diameter. For a square pitch (pitch = 1.0), this distance is equal to the diameter. As shown in Figure 6-19, Np is higher for higher-pitch propellers at all values of Re. [Pg.364]

It is important to recognize that at Re < 100, the flow conditions would approach laminar flow and mixing quality with these propellers would be poor. The power number functionality with propeller pitch between 1.0 and 2.0 at Re > 1000 can be approximated by... [Pg.364]


See other pages where Propeller pitch is mentioned: [Pg.1630]    [Pg.623]    [Pg.39]    [Pg.169]    [Pg.127]    [Pg.144]    [Pg.197]    [Pg.1451]    [Pg.315]    [Pg.169]    [Pg.1948]    [Pg.112]    [Pg.351]    [Pg.13]    [Pg.840]    [Pg.1936]    [Pg.1634]    [Pg.187]    [Pg.151]    [Pg.355]    [Pg.365]    [Pg.366]    [Pg.146]   
See also in sourсe #XX -- [ Pg.436 ]

See also in sourсe #XX -- [ Pg.436 ]




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