10R1011 TURBOCHARGER GP Caterpillar parts
3306, 350, 615C, 637D, 637E, 65C
Rating:
Alternative (cross code) number:
CA10R1011
10R-1011
10R1011
CA10R1011
10R-1011
10R1011
Weight: 44 pounds 20 kg.
CHALLENGER, WHEEL TRACTOR,
Related part:
2199710
TURBO GP-BASIC
10R1011
R
Cross Reference:
CATERPILLAR
0R6981,
10R1011,
1182284,
2199710,
SCHWITZER
167972,
179581,
Compare Prices: .
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Zuide Turbocharger 2199710 10R-1011 219-9710 For Caterpillar CAT Wheel Tractor 611 615C 615 637D 637E 637G Engine 3306 3306B
Zuide Item name:Turbocharger || Part number:2199710 10R-1011 219-9710 || For Caterpillar CAT Wheel Tractor 611 615C 615 637D 637E 637G Engine 3306 3306B || Please make sure that the product pictures and partnumbers are correct to avoid the parts you purchase not being suitable for your machine || If you are not sure that the parts are suitable for your machine please take pictures of your originalparts for us and we will help you confirm
Zuide Item name:Turbocharger || Part number:2199710 10R-1011 219-9710 || For Caterpillar CAT Wheel Tractor 611 615C 615 637D 637E 637G Engine 3306 3306B || Please make sure that the product pictures and partnumbers are correct to avoid the parts you purchase not being suitable for your machine || If you are not sure that the parts are suitable for your machine please take pictures of your originalparts for us and we will help you confirm
Turbo S3BSL128 Turbocharger 219-9710 10R-1011 for Caterpillar CAT 3306 3306B Engine 350 611 615C 637E 637G
NAOFRIMA Part Numbers:219-9710 || Application:for Caterpillar CAT 3306 3306B Engine 350 611 615C 637E 637G
NAOFRIMA Part Numbers:219-9710 || Application:for Caterpillar CAT 3306 3306B Engine 350 611 615C 637E 637G
VIIKEND Turbocharger 219-9710 10R-1011 Compatible with Caterpillar CAT Excavator 350 350-A Wheel Tractor 611 615C 615 615C II 637D 637E 637G Engine 3306
VIIKEND Part Name: Turbocharger || Part Number: 219-9710 10R-1011 Note: Please check the fitment carefully before purchase. Or just tell us the part number you need. || Engine Model: 3306 || Applicable: Compatible with Caterpillar CAT Excavator 350 350-A Engine 3306 || Compatible with Caterpillar CAT Wheel Tractor 611 615C 615 615C II 637D 637E 637G
VIIKEND Part Name: Turbocharger || Part Number: 219-9710 10R-1011 Note: Please check the fitment carefully before purchase. Or just tell us the part number you need. || Engine Model: 3306 || Applicable: Compatible with Caterpillar CAT Excavator 350 350-A Engine 3306 || Compatible with Caterpillar CAT Wheel Tractor 611 615C 615 615C II 637D 637E 637G
Compatible equipment models: 10R1011:
Information:
Installing Reinforcing Plates
Machine components fail primarily because of a localized overstressed condition. This overstressing is caused either by overloading, which stretches, compresses or bends the member, or by repeated flexing which cracks the member without visible bending. The former may occur, for example, in a track roller frame, the latter in a scraper gooseneck. In either case, the stresses can be reduced by properly applying reinforcements to the weak section. Improper application may have the opposite effect. High stresses usually occur at definite, predictable locations in machine members, although the locations are not always apparent until a failure occurs.The understanding and application of several basic rules will help in the successful design and installation of reinforcing plates: Rule 1 - Avoid sudden changes in cross-sectional area. Notches, sharp corners, and abrupt changes in area give rise to points of stress concentration. Reinforcements should be designed to enable loads to be transmitted smoothly through the reinforcement and from the reinforcement to the machine component (Figure 54). Notches and cracks should be filled with weld metal; corners should be curved with a generous radius; changes in width or thickness of plates should be gradual; ends should be tapered.
Figure 54 - Changes in cross sectional area must be made smoothly and gradually.Several examples of well designed reinforcement plates are shown in Figure 55. Note the tapered ends and rounded corners. In most cases, tapered plates add the same strength to beams subjected to bending stresses as rectangular plates do (Figure 56). The tapered plates weigh about half as much as rectangular plates and require no more time to install.
Figure 55 - Properly designed reinforcements have tapered ends and rounded corners.
Figure 56 - Rectangular reinforcing plates add no more strength than tapered plates. Rule 2 - Place reinforcements as far as possible from the neutral axis for bending loads. The neutral axis of a beam is located on a line of zero stress, which is usually at or near the center of the beam. Reinforcing plates of a given thickness will be most effective when placed as far as possible from the neutral axis (Figure 57). Note that plates added to the top and bottom of a beam parallel to the neutral axis add considerable more strength than plates of the same thickness added to the sides of the beam.
Figure 57 - Bending Load Reinforcements Rule 3 - Use a circular or box section for torsional loads. Reinforcements for shafts subjected to torsional stresses should be continuous around the shaft and should run the full length that is in torsion. (Figure 58). Square sections should be reinforced by adding plates on all sides. Rectangular sections are strengthened by adding plates to the opposite sides that are closest together. I-beams, channels and angles should be reinforced in such a manner that the final section is boxed. In all cases, the circular or boxed section is much stronger in torsion and is preferred for torsional loads.
Figure 58 - Torsional Load Reinforcements Rule 4 -
Machine components fail primarily because of a localized overstressed condition. This overstressing is caused either by overloading, which stretches, compresses or bends the member, or by repeated flexing which cracks the member without visible bending. The former may occur, for example, in a track roller frame, the latter in a scraper gooseneck. In either case, the stresses can be reduced by properly applying reinforcements to the weak section. Improper application may have the opposite effect. High stresses usually occur at definite, predictable locations in machine members, although the locations are not always apparent until a failure occurs.The understanding and application of several basic rules will help in the successful design and installation of reinforcing plates: Rule 1 - Avoid sudden changes in cross-sectional area. Notches, sharp corners, and abrupt changes in area give rise to points of stress concentration. Reinforcements should be designed to enable loads to be transmitted smoothly through the reinforcement and from the reinforcement to the machine component (Figure 54). Notches and cracks should be filled with weld metal; corners should be curved with a generous radius; changes in width or thickness of plates should be gradual; ends should be tapered.
Figure 54 - Changes in cross sectional area must be made smoothly and gradually.Several examples of well designed reinforcement plates are shown in Figure 55. Note the tapered ends and rounded corners. In most cases, tapered plates add the same strength to beams subjected to bending stresses as rectangular plates do (Figure 56). The tapered plates weigh about half as much as rectangular plates and require no more time to install.
Figure 55 - Properly designed reinforcements have tapered ends and rounded corners.
Figure 56 - Rectangular reinforcing plates add no more strength than tapered plates. Rule 2 - Place reinforcements as far as possible from the neutral axis for bending loads. The neutral axis of a beam is located on a line of zero stress, which is usually at or near the center of the beam. Reinforcing plates of a given thickness will be most effective when placed as far as possible from the neutral axis (Figure 57). Note that plates added to the top and bottom of a beam parallel to the neutral axis add considerable more strength than plates of the same thickness added to the sides of the beam.
Figure 57 - Bending Load Reinforcements Rule 3 - Use a circular or box section for torsional loads. Reinforcements for shafts subjected to torsional stresses should be continuous around the shaft and should run the full length that is in torsion. (Figure 58). Square sections should be reinforced by adding plates on all sides. Rectangular sections are strengthened by adding plates to the opposite sides that are closest together. I-beams, channels and angles should be reinforced in such a manner that the final section is boxed. In all cases, the circular or boxed section is much stronger in torsion and is preferred for torsional loads.
Figure 58 - Torsional Load Reinforcements Rule 4 -
Caterpillar SIS machinery equipment:
Caterpillar parts catalog:
Parts turbocharger Caterpillar catalog:
1111653
TURBOCHARGER GP
3306, 3306B
3306, 3306B
2199710
TURBOCHARGER GP
3306, 3306B, 350, 611, 615C, 637D, 637E, 637G, 972G
3306, 3306B, 350, 611, 615C, 637D, 637E, 637G, 972G
7N2515
TURBOCHARGER GP
3306, 571G, 572G, D398, D398B, D7G
3306, 571G, 572G, D398, D398B, D7G
7C7582
TURBOCHARGER GP
3306, 3306B, D25D, D300D
3306, 3306B, D25D, D300D
7C7581
TURBOCHARGER GP
3306, 65C, 70C
3306, 65C, 70C
7C7577
TURBOCHARGER GP
235C, 235D, 637E
235C, 235D, 637E
1106979
TURBOCHARGER GP
3306, 3306C
3306, 3306C
2199711
TURBOCHARGER GP
3306, 545, 627B, 627E, 627F, 627G, 966G
3306, 545, 627B, 627E, 627F, 627G, 966G
9N0111
TURBOCHARGER GROUP
3306, 572G, 621R, 815B, 966D, 972G, 973, 980B, D379, D379A, D379B, D398B, D7G
3306, 572G, 621R, 815B, 966D, 972G, 973, 980B, D379, D379A, D379B, D398B, D7G
5P8773
TURBOCHARGER MOUNTING
1673C, 3306, 3306B, 615, 615C, 621E, 637D, 637E, 639D, 65, D25D, D300D
1673C, 3306, 3306B, 615, 615C, 621E, 637D, 637E, 639D, 65, D25D, D300D
8N1852
TURBOCHARGER GP
3512, 3516
3512, 3516
1771064
TURBOCHARGER GP
938G, 950G, 962G, IT38G
938G, 950G, 962G, IT38G
4P6171
TURBOCHARGER GP
3116, CB-634, CB-634C
3116, CB-634, CB-634C
4N7070
TURBOCHARGER
776, 777
776, 777
7W7195
TURBOCHARGER GP
3406B
3406B
1397741
TURBOCHARGER GP
938G, IT38G
938G, IT38G
1137540
TURBOCHARGER GP
3512B
3512B
3N4834
TURBOCHARGER SHIELD GROUP
D379A, D398A
D379A, D398A