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Published: 30 September 2015
Fig. 11 Spur gear tooth strength test. Source: Ref 17 More
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Published: 30 September 2015
Fig. 7 High-strength gas metal arc weldment between an FN-0205 steering gear (6.9 g/cm 3 ) and an AISI 1035 steel shaft using an E70S-type filler wire More
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Published: 01 January 1996
Fig. 8 Bending strength curve for gear life rating of normal industry quality material (Grade 1 per Ref 2 ) More
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Published: 09 June 2014
Fig. 33 Bending fatigue strength of gear teeth at (a) tooth gap hardening and (b) flank hardening for various steels. Broken lines denote confidence limit according to DIN 3990. Source: Ref 34 , 42 More
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Published: 09 June 2014
Fig. 55 Factors affecting contact fatigue strength of gear tooth flank surface. Source: Ref 50 More
Series: ASM Handbook Archive
Volume: 11
Publisher: ASM International
Published: 01 January 2002
DOI: 10.31399/asm.hb.v11.a0001815
EISBN: 978-1-62708-180-1
... conditions and stresses that effect gear strength and durability. The article provides information on different gear materials, the common types and causes of gear failures, and the procedures employed to analyze them. Finally, it presents a chosen few examples to illustrate a systematic approach...
Series: ASM Handbook
Volume: 4C
Publisher: ASM International
Published: 09 June 2014
DOI: 10.31399/asm.hb.v04c.a0005867
EISBN: 978-1-62708-167-2
... Abstract Induction hardening is a prominent method in the gear manufacturing industry due to its ability of selectively hardening portions of a gear such as the flanks, roots, and/or tips of teeth with desired hardness, wearing resistance, and contact fatigue strength without affecting...
Series: ASM Handbook
Volume: 7
Publisher: ASM International
Published: 30 September 2015
DOI: 10.31399/asm.hb.v07.a0006114
EISBN: 978-1-62708-175-7
... inspection mechanical properties powder metallurgy quality control surface durability POWDER METALLURGY (PM) is a flexible metalworking process for the production of gears. The PM process is capable of producing close tolerance gears with ultimate tensile strengths up to 1445 MPa (210 ksi...
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002375
EISBN: 978-1-62708-193-1
... on the gear tooth surface as a function of the surface speed. This secondary film is very thin, has a very high shear strength, and is only slightly affected by compressive loads as long as constant temperature is maintained. Certain rules about a lubricant should be remembered in designing gearing...
Series: ASM Handbook
Volume: 4D
Publisher: ASM International
Published: 01 October 2014
DOI: 10.31399/asm.hb.v04d.a0005952
EISBN: 978-1-62708-168-9
... of a beam. Complete gear design should include determination of the following factors: Diametral pitch to provide the necessary static strength and stiffness Compressive stress at the lowest point of single-tooth contact (often referred to as Hertz stress) on the driving gear Bending stress...
Series: ASM Handbook
Volume: 4C
Publisher: ASM International
Published: 09 June 2014
DOI: 10.31399/asm.hb.v04c.9781627081672
EISBN: 978-1-62708-167-2
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Published: 01 October 2014
Fig. 4 Determinations of shear yield strengths (top curve) and net stresses at various depths below the surface of a carburized gear indicate where the gear will fail by case crushing. In this instance, the case would fail in the zone below 1.3 mm (0.050 in.) from the surface because More
Series: ASM Handbook
Volume: 8
Publisher: ASM International
Published: 01 January 2000
DOI: 10.31399/asm.hb.v08.a0003327
EISBN: 978-1-62708-176-4
... of the contact surface. Gear specimens should be measured at the tooth half height (or lowest point of single-tooth contact) for surface durability tests and at the midpoint of the root fillet for bending strength tests. Tests Simulating Gear Action Tests that simulate gear action are the RCF test...
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Published: 01 January 2006
Fig. 4 Pit-initiated in-service failure of a landing gear due to dynamic stresses. The collapse of the high-strength 300M steel main landing gear load barrel was due to severe all-around pitting. More
Series: ASM Handbook
Volume: 4C
Publisher: ASM International
Published: 09 June 2014
DOI: 10.31399/asm.hb.v04c.a0005870
EISBN: 978-1-62708-167-2
... affecting their magnitude and distribution as well as their effects on longevity of heat-treated components. The residual stresses of the induction-hardened part are often produced by microstructural transformation, thermal shrinking, distortion, and quenching. Fatigue strength is the main property...
Series: ASM Handbook
Volume: 5A
Publisher: ASM International
Published: 01 August 2013
DOI: 10.31399/asm.hb.v05a.a0005739
EISBN: 978-1-62708-171-9
... metals in airframe structures. This article summarizes the results of materials and component testing. It also presents a cost/benefit analysis of HVOF WC/17Co and WC/10Co4Cr coatings on aircraft landing gear components. aircraft landing gears corrosion cost assessment fatigue hard chrome...
Series: ASM Handbook
Volume: 4D
Publisher: ASM International
Published: 01 October 2014
DOI: 10.31399/asm.hb.v04d.a0005987
EISBN: 978-1-62708-168-9
.... The total case depth for a carburized tooth should be adjusted based on the diametral pitch, with schematic representation shown in Fig. 5 . Table 3 provides the recommended case depth as a function of diametral pitch. Core hardness of the gears imparts the appropriate bending strength during service...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006553
EISBN: 978-1-62708-210-5
... castings 354.0 Premium-strength castings for the aerospace industry 355.0 Sand: air compressor pistons; printing press bedplates; water jackets; crankcases. Permanent: impellers; aircraft fittings; timing gears; jet engine compressor cases 356.0 Sand: flywheel castings; automotive transmission...
Series: ASM Handbook
Volume: 4D
Publisher: ASM International
Published: 01 October 2014
DOI: 10.31399/asm.hb.v04d.a0005951
EISBN: 978-1-62708-168-9
... Resistance to scuffing or seizing Bending or torsional strength Bending fatigue strength Resistance contact fatigue, pitting, or case crushing Case-hardening processes and their characteristics Table 1 Case-hardening processes and their characteristics Process Characteristics...
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Published: 01 January 1987
Fig. 968 Pieces of the hub of a forged aircraft main-landing-gear wheel half, which broke by fatigue. The material is aluminum alloy 2014-T6. Tensile specimens from elsewhere in the wheel had tensile strength of 493.7 MPa (71.6 ksi) and 8.9% elongation in the transverse direction, and tensile More