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housing which supports the teeth (as it influences the alignment of the gear axes); the deflections of the housing, shafts, and gear blanks (both elastic and thermal); and the internal clearances in the bearings which support the gears, among others. All these and any other appropriate effects must be evaluated in order to define the total effective alignment error et for the gear pair. Once this is accomplished, the load-distribution factor may be calculated. In some cases it may not be possible to fully define or even estimate the value of et. In such cases an empirical approach may be used. We discuss both approaches in some detail. The empirical approach requires only minimal data, and so it is the simplest to apply. Several conditions must be met, however, prior to using this method: 1. Net face width to pinion pitch diameter ratios must be less than or equal to 2.0. (For double-helix gears, the gap is not included in the face width.) 2. The gear elements are mounted between bearings (not overhung). 3. Face width can be up to 40 in. 4. There must be contact across the full face width of the narrowest member when loaded. 5. Gears are not highly crowned. The empirical expression for the load-distribution factor is Cm = Km = 1.0 + Cmc(CpfCpm + CmaCe) where Cmc = lead correction factor Cpf = pinion proportion factor Cpm = pinion proportion modifier Cma = mesh alignment factor Ce = mesh alignment correction factor The lead correction factor Cmc modifies the peak loading in the presence of slight crowning or lead correction as follows: Cmc = 1.0 0.8 for gear with unmodified leads for gear with leads properly modified by crowning or lead correction (10.21)

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Figure 10.8 shows the pinion proportion factor Cpf, which accounts for deflections due to load. The pinion proportion modifier Cpm alters Cpf based on the location of the pinion relative to the supporting bearings. Figure 10.9 defines the factors S and S1. And Cpm is defined as follows: Cpm = 1.0 1.1 when S1/S < 0.175 when S1/S 0.175

This calls sqlite3_errmsg16, which takes the database handle and returns the error message in plain English. This is then wrapped in an NSException and raised. You then clean up the database connection in the dealloc (along with pathToDatabase):

he Orb-Tracker project is designed to remotely control the azimuth and elevation of a satellite antenna system. Many amateur radio operators and weather satellite enthusiasts need a method to control their high-gain satellite antenna systems. The Orb-Tracker will control two single low-cost antenna rotators such as the Gemini Orbit 360 or the dual-rotator Yeasu 5500 azimuth/elevation (AZ-EL) rotator using a BASIC STAMP 2 microcontroller. In order to track low-earth-orbit satellites, amateur radio and other satellite enthusiasts use satellite tracking software, which is readily available. NASA originates data sets that are used to track the many orbiting satellites that cross the heavens every day and night. These satellite data sets are readily available and can be downloaded every month with updated parameters for many satellites now in the sky. A few satellite tracking programs, such as WISP, NOVA, and The Station Program, send out serial data from the standard serial port of the PC. The EASYCOMM data format from

The mesh alignment factor Cma accounts for factors other than elastic deformations. Figure 10.10 provides values for this factor for four accuracy groupings. For double-helix gears, this figure should be used with F equal to half of the total face width. The mesh alignment correction factor Ce modifies the mesh alignment factor to allow for the improved alignment which may be obtained when a gear set is adjusted at assembly or when the gears are modified by grinding, skiving, or lapping to more closely match their mates at assembly (in which case, pinion and gear

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