Document Mb2JZYOQ2JKMLKGbxRBYoVex

754 CHAPTER 32 1956 Guide mately 17 in. (Fig. 3). This is equivalent to a 15 x 16 in. duct, which will be used for Section F. The velocity in Section F will be 1200 fpm. 2. Determine the pressure loss in Section F. Actual length of duct is 10 ft; equiv alent length of elbow take-off is assumed as 10 W, or 12.5 ft. Therefore, the total 22 5 equivalent length is 22.5 ft. The pressure loss in F = 0.13 In. X ^gg- =0.03 in. water. 3. Using Static Regain Chart, Fig. 13, size Section B for a net pressure loss equal to TthheeloospseirnatiFo,noisr 0in.0d3iciant.ewdabtyeraarrsofwolhloewadss: on the dotted line on Fig. 13. On Fig. 13, start at the velocity in Section A (1500 fpm) at left margin. Proceed horizontally to 6000 cfm ordinate, and then run parallel to the curved lines to intersect the di agonal Base Line. From this point, rise vertically to the 0.03 net static pressure loss line, and from this intersection proceed horizontally to the Air Velocity Base Line. Proceed parallel to curved lines to intersect ordinate for 25 ft equivalent duct length, and then move horizontally to left margin and read the velocity (1500 fpm). ` Since Section B carries 6000 cfm, the area required will be jgjjg. = 4 sq. ft, and the4s. izUesionfgdSutcattiwc iRll ebgea3in6 Cx h1a6ritns. (Figs. 12 and 13) determine size of Sections C, D, E and G, but instead of allowing 0.03 in. net loss, which was used for Section 8, proceed from the diagonal Base Line vertically to the no gain or loss diagonal. The procedure for Section E is shown by the dotted line and arrows on Fig. 12: starting from 1040 fpm velocity, which is the velocity in Section D. Duct sizes determined by the given procedure are listed in Table 7. Section Table 7. Tabulation of Results (Example 6) Aib Volume cfm Equiva lent Length ft Velocitt fpm Rectangular Duct in. Diam. in. Fbictjon Peb 100 r* in. HtO A 8000 40 1500 B 6000 25 1500 C 4500 15 1300 D 3000 26* 1040 E 1500 15 860 F 2000 22.5 1200 G 1000 15 900 48 x 16 iff) X if) 31 x 16 26 x 16 16 x 16 15 x 16 10 x 16 29.2 ' ' 17. 0.13 0.13 Includes additional equivalent lenjth oi elbow between ouuew 11 ft e^uiSSntSh of duct. (Based on 3000 cfm at estimated velomty of 1100 fpm). bubs LoM . HiO .05 .03 .0 0 0 .03 0 , 5.8 F, <r Air Duct Design 755 5. Total pressure loss of the system is the loss in Section A, plus the loss in Section F (or B), plus the loss in the outlet as"follows: 40 .........." Loss in Section A = 0.13 in. X -- = 0.05 100 Loss in Section F (or B) = 0.03 . Outlet Loss = 0.12...... Total Pressure Loss = 0.20 in. DUCT CONSTRUCTION DETAILS Straight sections of round duct are usually formed from sheets, rolled to the proper radius with a longitudinal grooved seam. Each section is swaged 1.5 in. from each end and assembled with the larger end of the adjoining section butting against the swage. The sections are held in .place by rivets, sheet metal screws, or by soldering. Rectangular ducts are generally constructed by breaking the comers and grooving the longitudinal seam, although some fabricators still use the standing seam. Elbows and transformation sections are generally formed with Pittsburgh corner seams because this seam is easier to lock in place than the double seam, but complicated' fittings such as double compounded elbows are usually constructed with double seam corners. The construc tions of these various seams, as well as the types of girth connections, are shown in Fig. 15. The application of the various slips and connec tions is outlined in Table 8. The end slip may be used wherever S slips are recommended. Where drive slips are used, the end slip may be ap plied on the narrow side of the duct, and the drive slips on only the maxi mum side. Designs M to P of Fig. 15 are for flush type seams on ductwork where joints are to be concealed. For smooth appearance the seams may be soldered flush or filled with auto body filler. Screws or rivets used should be of flat-head type. Ducts 25 to 30 in. in size should' be reinforced .between the joipts, but not necessarily at the joint. Ducts 31. in. and up should be reinforced at the joint and between the joints; if drive slips are used the angles are usually riveted to the duct about 2 in. from the slips. It is good practice to cross-break or kink all flat surfaces to prevent vibration or buckling due to the air flow and accompanying variations in internal pressure. The construction of elbows and changes of shape cannot be definitely outlined, because of the varied conditions encountered in the field, but in general, long radius elbows and gradual changes in shape tend to maintain uniform velocities accompanied by decreased turbulence, lower resistance end a minimum of noise. Heavy canvas connections (asbestos cloth if there is a fire hazard) are recommended on both the inlet and outlet to all fans. Self-vulcanizing edhesive tapes are available for this purpose and for sealing joints in duct work. The fan discharge connections shown in Fig. 15 are marked good, juir, and poor in the order of the amount of turbulence produced. An respeetion of the heater connections shown in Fig. 15 will readily show that uuiform velocity, through the heater cannot be expected in the diagram uoted poor. When obstructions cannot be avoided, the duct area should Uever be decreased more than 10 percent, and then a streamlined collar ?uuld be used. Larger obstructions require an increase in the duct size re order to maintain as nearly uniform velocity as possible. Branch take-