Document nNRKbJ9daDjgEVorXpynv4ggX

890 CHAPTER 40 1952 Guide of frequencies and does not include the airborne vibrations known as sound, there is one basic formula which is important in the solution of the problem. It is the formula of transmissibility as governed by the equation: where T -- transmissibility of the support. / = frequency of the vibratory force. fn -- natural frequency of the machine unit on its support (damping = 0). Equation 12 showB that the transmissibility approaches unity for disturbing frequencies considerably lower than the natural frequency of the mounting. As the disturbing frequency is increased, the transmis sibility is also increased until at the resonant frequency, where / = /,, the transmissibility becomes infinite. This is not true in practice because all materials have some internal damping effect. However, operating at or very close to the resonant frequency is always serious as forces and stresses may be multiplied 10 to 100 times.. As the disturbing frequency becomes greater than die natural frequency, the transmissibility becomes a smaller quantity, and at the value of ///,, = \/2 it again has the value of unity. Beyond this point true isolation is first accomplished. At a ratio of 3 to 1 for / to./n the isolation is effective enough for practical application, and experience and economical design have shown that a ratio of 5 to 1 is good. For high speeds, higher ratios for / to/,, are easily attained and give better results for effective vibration control, but for the lower speeds as experienced with compressor work the higher ratios become uneconomical. For a given installation, the speed of the compressor is fixed by. the speci fications; therefore the value of / is fixed. That leaves only /,, to be de termined, and that is accomplished by the choice of mounting material and design for the support of the machine. It is well to keep in mind that when trying to isolate vibration, no attempt should be made to isolate the driving and driven piece of equipment separately. The two should be mounted on a rigid frame, and then the entire assembly isolated according to the rules presented in this chapter. The value of/,, can be controlled by the flexibility of the machine support, and when the deflection of the machine support is proportional to the load applied (such as with springs or nearly so with rubber in shear)' the value of /D can be determined by Equation 13: '-hj/i- TM where g = gravitational constant. d -- static deflection of supporting material. / = frequency of the vibratory force. /,, = natural frequency of the machine unit on its support (damping = 0). By the use of Equation 13 a set of curves may be plotted as shown in Fig. 11. The first fine AB, plotted as the critical frequencies for the vari ous static deflections, is a curve showing the worst possible conditions or resonant conditions. Plotting another curve CD, which is \/2 times curve AB, shows the area MCDN in which the resilient material or mounting does more harm Sound Control 891 Fig. 11. Static Deflection fob Various Frequencies than good. Plotting curves EF (3 times curve AB) and GH (5 times curve AB) shows area EGHF which represents efficient and economical isolation. Area GPOH is excellent isolation, but for all except the highest speeds, becomes. rather uneconomical because of the large deflections required. Example 4: An electric motor driven compressor unit is to be isolated. The com pressor is partially balanced and operates at a speed of 360 rpm. The speed of the motor is 1160 rpm, and is belt connected to the compressor. Total weight of the compressor and motor is 4500 lb. Solution: The minimum disturbing frequency to be isolated is 360 cycles per minute. Assume that the desired ratio of forced to natural frequency is 3 as a mini mum, and that 5 is desired. The desired natural frequency of the mounting is 360 + 5 = 72 cycles per minute. From Fig. 11.a deflection of 7 in. is required to attain a natural frequency of 72 cycles per minute. This value may be obtained from critical curve AB for 72 cycles, or from curve GH (5 times critical) for 360 cycles. For the minimum ratio of 3 the deflection would be 2.5 in. The next step is to determine the total weight to be supported by the springs. For low speed partially balanced compressors, it has been found necessary to add a foundation weighing 2 to 3 times the weight of the motor and compressor, in order to maintain the machine movement below 0.03 in. Compressor and motor......................................................................... 4,500 lb Concrete foundation............................................................................. 9,000 lb Total........................................................................ .................... 13,5001b Practical application dictates the number of springs to be used, which is based on the design of the machine foundation and the supporting floor structure. However, it is desirable to design for at least 8 springs and one or two spares for cases of un known weights. As many as 50 springs have been used on one installation. The distribution of the springs must be balanced against the masses to be supported, otherwise the foundation design and supporting structure determine the location of the springs. The choice of the material used in the design of .the resilient mounting is also important. For the slow-speed type compressor, a common speed found in practice is 360 rpm. For speeds below this, isolation should not be attempted except under careful supervision. Referring to Fig. 11, it is