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Downloaded from Digital Engineering Library @ McGraw-Hill (www.digitalengineeringlibrary.com) Copyright 2004 The McGraw-Hill Companies. All rights reserved. Any use is subject to the Terms of Use as given at the website.

FIGURE 10.8 Pinion proportion factor Cpf. (From Ref. [10.1].)

become a matched set). Only two values are permissible for Ce either 1.0 or 0.8, as defined by the following requirements: 0.80 Ce = 0.80 1.0 when the compatibility of the gearing is improved by lapping, grinding, or skiving after trial assembly to improve contact when gearing is adjusted at assembly by shimming support bearings and/or housing to yield uniform contact for all other conditions

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these programs can be easily utilized to control the Orb-Tracker s STAMP 2, which in turn controls the AZ-EL rotators. Polar satellites cross the sky in ascending or descending orbits around the globe, crossing over the north and south poles during each revolution around the earth. In order to track these moving satellites and maintain the maximum signal emitted by satellites, amateur radio operators must move their antennas both in elevation and azimuth, meaning one rotator must be able to rotate 360 in the horizontal plane and the second rotator must move up and down from the horizontal plane through at least 90 to pole or vertical. The Orb-Tracker can simultaneously control two rotators, using the data from the serial port, once the proper satellite data set is plugged into the tracking program. The OrbTracker is designed to be used with two inexpensive TV rotators, which use positive and negative drive voltages and variable resistors to indicate position, such as Orbit 360 rotators. The Orb-Tracker, as mentioned earlier, will also drive the dual-rotator Yaesu 5500 AZEL rotator.

- (void) dealloc { [self close]; [pathToDatabase release]; [super dealloc]; }

If enough detailed information is available, a better estimate of the loaddistribution factor may be obtained by using a more analytical approach. This method, however, requires that the total alignment error et be calculated or estimated. Depending on the contact conditions, one of two expressions is used to calculate the load-distribution factor.

FIGURE 10.9 Definition of distances S and S1. Bearing span is distance S; pinion offset from midspan is S1. (From Ref. [10.1].)

Downloaded from Digital Engineering Library @ McGraw-Hill (www.digitalengineeringlibrary.com) Copyright 2004 The McGraw-Hill Companies. All rights reserved. Any use is subject to the Terms of Use as given at the website.

FIGURE 10.10 Mesh alignment factor Cma. For analytical method for determination of Cma , see Eq. (10.21). (From Ref. [10.1].)

The heart of the Orb-Tracker is the BASIC STAMP 2 processor, an A/D converter, a power supply, and a handful of discrete components The diagram in Fig 15-1 illustrates the OrbTracker for use with the Orbit 360 type low-cost TV rotators The serial data output from your PC tracking program (NOVA/WISP) is fed to the DB-9 serial connector at the top left of the diagram The serial port connector also does double duty, since it is also used to program the BASIC STAMP 2 microprocessor The BASIC STAMP 2 serial port connections are on pins 1 through 4, respectively (the TX, RX, ATN, and ground pins) The Orb-Tracker s A/D converter samples the position voltages from both the azimuth and elevation rotators These analog voltages are converted into digital numbers by the LTC1298 converter.

If you compile now, you will see two warnings appear. The first warning is in the init method, as shown in Figure 5-5.

If the tooth contact pattern at normal operating load essentially covers the entire available tooth face, Eq. (10.22) should be used. If the tooth contact pattern does not cover the entire available tooth face (as would be the case for poorly aligned or high-crowned gears) at normal operating loads, then Eq. (10.23) must be used: Cm = 1.0 + and Cm = where GetZF Wt pb (10.23) GetZF 4Wt pb (10.22)

Wt = tangential tooth load, pounds (lb) G = tooth stiffness constant, (lb/in)/in of face Z = length of line of contact in transverse plane et = total effective alignment error, in/in pb = transverse base pitch, in F = net face width of narrowest member, in

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