Документ взят из кэша поисковой машины. Адрес оригинального документа : http://www.atnf.csiro.au/observers/memos/AT40.3.1_102.pdf Дата изменения: Thu Apr 16 08:50:00 2015 Дата индексирования: Sun Apr 10 02:18:40 2016 Кодировка: Поисковые слова: active galaxy

Parkes Counterweight Issues

May 4, 2002

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Background

It became clear, during the course of the study of the windloading on the Parkes reflector (ref: AT/39.3/113) that the counterweight was not optimally fulfilling its function. This note explores the details and possible remedies.

Figure 1: The elevation motor currents as a function of the elevation. Figure 1 is the central evidence: it shows the drive currents in the elevation. The "o" symbols show the current when driving towards towards the horizon. (The difference between UP and DOWN is moving: the counterweight helps in one direction, opposes in the shape of the curves, from large currents (torques) at the zenith to was not the designers' intention. elevation motors as a function of the zenith, the "+" when driving due to the frictional losses while other). The point at issue is the low values near the horizon. This

The solid curve in figure 1 mo dels the torque, following the recipe sketched in figure 2.

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Approximate location of the centre of mass of dish and focus cabin structure

15.5 deg

The centre of mass lies on this line, and gives a zenith torque of 256 T-m

X

Rotating mass = 800 T X = 31 cm.

9.5 m

Locus of the counterweight centre of mass

Figure 2: A geometrical construction showing the lo cation of the various centres of mass

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The Mo del

The mo del (figure 2) is based on : · Mo del fitting of the function T cos(El0 - El) to figure 1 puts the peak current at 17 amps, and El0 = 105.5 degrees. · The calibration of the motor currents-torque relation :15.5 (T-m)/amp (see AT/39.3/112) This translates the peak current of 17. Amps to a torque of 256 T-m · The total mass of the moving structure is 800 T. This sets the lo cation of the centre of mass at 31 cm from the elevation axis.

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Suggestions, Problems, Questions

A response to the present situation is to redistribute the weight below the elevation axis, with two main aims: - To flatten the torque-elevation function, so that there is a healthy backlash reserve at all elevations under windy conditions. - To lower (or at least not increase) the peak torque.

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We have two parameters at our disposal : the amount of weight we add, and where we put it. Increasing the counterweight by 8 - 30 T will move the peak torque elevation into the observers' elevation range, and raise substantially the torque at the horizon. Simply changing El0 from 105.5 to 90 degrees will double the torque at the horizon. The space limitations are more serious: the obvious candidate area is at some distance from the optical axis, and will result in higher currents, in the range 20 to 25 Amp.

3.1

The low current problem

The designers intended the counterweight to provide the "anti-backlash" mechanism. Operation at low elevations under windy conditions is therefore made difficult. Wind from behind the dish could overcome the counterweight. - The pinion gears normally mesh on the lower surface of the rack gears. If the torque reverses the mesh will change, leading to a pointing error. The servo system will correct for this, but it will be a serious disturbance at the higher frequencies. - It is currently held that this gear-mesh reversal has no implications as far as the machinery is concerned. - However, there are operational implications: a wind stow is forced when the currents fall to zero. - Manual stowing of the antenna could be compromised.

3.2

The high current problem

The motors are not stressed at present. Changing the torque-elevation function could raise the power requirements, and possibly overheat the motors.

3.3

Fo cus cabin

Any increase in weight of the fo cus cabin is fundamentally undesirable: it has a strong impact on the torque (a multiplier of 4 compared to weight at the counterweight), and it exacerbates the lo cal deformation of the reflector surface at the feed legs. The problem right now is that small increases will expose the antenna to more wind stows. Flattening the torque-elevation function will help considerably.

3.4

How much weight and where to put it

These details depend on the space available in the counterweight; the points listed below are intended to give an idea of the magnitudes involved, and point to the useful lo cations. The coordinate frame for this discussion has the antenna stowed (as in figure 2, with the elevation axis East-West, tipping to the North. The weight will be added a distance of about 9 m below the elevation axis. A weight of 7.5 T will move El0 to 90 degrees. If the weight is positioned below the current centre of mass (32 cm south of the elevation axis), then the horizon current doubles to 8 A; the peak current (at El0 increases by 0.3%. 3


If the weight is placed at the southern end of the counterweight (where space seems simplest to find), the peak current will rise to 19 A, and the horizon current to 9.5 A.

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Discussion

Do we need to do anything ? The operational constraints are probably the strongest argument: the low torque at the horizon makes the antenna vulnerable to a wind stow when the wind is behind the antenna. The failure of the backlash machinery at low elevations do es not appear to endanger the integrity of the gearbox/rack machinery, but it will certainly compromise the pointing. The elevation bearings are each rated for a static load of 1000 T, so an increment of 10-20 T is unlikely to be a problem. A change is desirable. Next steps - The recommendations of Freeman Fox and Partners and of Connell-Wagner should be reviewed to ensure that there are no other engineering considerations. - The counterweight structure should be examined to identify possible sites for the additional weight. - Andrew Hunt's notes on the heating of the motors under load should be consulted to determine the maximum allowable torque (current).

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