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SERVICE BULLETIN
NOTICE:
The Type of Change and Recommended Compliance specified reflects Solar’s best judgment regarding the
Service Bulletin. All questions should be directed to your Solar Field Service Representative. Solar, Saturn,
Centaur, Taurus, Mercury, Mars, Titan, SoLoNOx, and Turbotronic are trademarks of Solar Turbines Incorporated.
Cat and Caterpillar are trademarks of Caterpillar Inc. Specifications subject to change without notice.
NUMBER:
2.1/103
ISSUED:
May 1987
REVISED:
PRODUCT:
Mars
MODEL(S):
All
Specifics:
Units with Pneumatic Starter Assembly, P/N 124990 through -200
SUBJECT: PNEUMATIC STARTER/CLUTCH ASSEMBLY FIELD
MODIFICATION KIT
Type of Change:
Product Improvement
Recommended
Compliance:
Information
Purpose:
To announce the availability of a Mars pneumatic starter field modification kit and describe the
nature of the improved design.
GENERAL INFORMATION:
Some early model pneumatic start system failures occurred due to starter clutch shaft misalignment
and/or clutch bearing failure due to a marginal lubrication. The start system has been redesigned
and incorporated in new engine products since 1985. The design improvements are available in a
field modification kit for earlier units. The installation of this kit will require some changes to the
package and will generate some displaced parts.
Original Design – See Figure 1
1.
Starter/clutch shaft misalignment
The initial arrangement of the starter/clutch is shown in Figure 1. Spline clearance and
the short distance between the splines, together with high spline eccentricities could
cause the splines to bind. This with high spline eccentricities could cause the splines to
SERVICE BULLETIN
Page 1 of 5
NUMBER: 2.1/103
bind. This would result in high loads on the small bearing and cause the bearing to heat
up, loosen on the shaft, spin and create more heat until failure. Binding of the splines
could also misalign the clutch shaft and housing, which would cause end loading and
wear on the clutch sprags, and possible assembly lockup.
2.
Lubrication
The lubrication of the clutch components is accomplished through a jet as shown in
Figure 1. The oil is caught in the annulus, flows through axial holes to the small bearing
area, through a around the bearing and into the clutch space. Here, the oil is trapped by
an oil dam. Some of this oil is centrifuged out through holes in the clutch housing and
the remainder flows through the large bearing.
The original design did not provide sufficient oil distribution at the small bearing sliding
surfaces (cage/inner race). This could create high friction between the sliding surfaces
and cause heat to warm up the bearing inner race again, contributing to relation of fit
and spin on the shaft, thus creating more heat until failure.
Figure 1
Mars Starter/Clutch Original Design
Page 2 of 5
SERVICE BULLETIN
NUMBER: 2.1/103
Redesign – See Figure 2
To minimize the loads on the small bearing, the starter/clutch splines distance and tooth clearances
were increased. Spline teeth were also crowned. The increased distance and clearances prevent
splines from binding, thus eliminating the load on the small bearing and misaligning the clutch.
Crowning of the spline teeth also minimized thrust loads on the bearing. To ensure lubrication to
the clutch assembly components, the following changes were made:
•
To distribute the oil more efficiently, the single jet was replaced by three, equally spaced.
•
Two oil annuli are now provided. One is for cooling the bearing inner race, the other for
bearing and clutch lubrication. One other jet was added to the large bearing, on the outside
surface for lube and cooling.
•
To ensure oil on the bearing sliding surfaces and clutch shaft surfaces, the oil dam inside
diameter was reduced. This trapped more oil.
•
The small bearing cage was changed from an inner race riding to an outer race riding. This
ensures the sliding surfaces will be lubricated. Internal clearances also were increased to
tolerate a greater differential temperature between the races.
•
To ensure the balls ride in the proper position in the bearing races, shimming of the clutch
assembly is made. This positions the balls and end play is minimized.
•
Air-oil mist cooling holes were added. Holes on the rotating housing pump the air-oil mist
out, and holes on the clutch shaft let the air-oil mist in.
SERVICE BULLETIN
Page 3 of 5
NUMBER: 2.1/103
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Figure 2
Mars Starter/Clutch New Design
ACTION REQUIRED:
1.
Customer determines if turbine package is equipped with pneumatic starter assembly
P/N 124990-100 thru -200. If the package is not equipped with one of these pneumatic
start systems, no action is required. If the package has one of the above assemblies,
review maintenance records to determine if the field modification kit has been installed.
If so, no further action is required.
2.
If the package has an unmodified pneumatic starter assembly P/N 124990 -100 thru -200,
it should be determined if the starter is functioning correctly. This can be done without
any special tools or equipment.
3.
Refer to the Operation & Maintenance Instructions manual to review operating
parameters and sequence of operation associated with pneumatic starter. During the
next scheduled maintenance or other convenient shutdown period, examine the air/gas
inlet strainer (FS 921) and pilot valve inlet filter (FS 922) for condition and cleanliness.
Install 0-200 PSI gage on pressure sensing line on starter housing, Figure 3. Check
starter oil reservoir for correct level.
Page 4 of 5
SERVICE BULLETIN
NUMBER: 2.1/103
4.
Observe starter during next start cycle and rundown; observe installed gage to see if
adequate start pneumatic pressure is achieved; listen for timely starter clutch drop-out
during run-up and for any abnormal sounds or vibration that may indicate starter shaft
binding.
NOTE
Ear protection may be required if package is in confined area.
5.
Contact the Solar Regional Service Office in your area for further recommended action
if any operating abnormalities are found or suspected. Solar Regional Service assistance
is available for the above recommended maintenance inspection.
Figure 3
Typical Turbine Pneumatic Starter Installation
SERVICE BULLETIN
Page 5 of 5
NUMBER: 2.1/103
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