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Actuators

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Series: ASM Failure Analysis Case Histories
Volume: 1
Publisher: ASM International
Published: 01 December 1992
DOI: 10.31399/asm.fach.v01.c9001029
EISBN: 978-1-62708-214-3
... Abstract Two investment-cast A356 aluminum alloy actuators used for handles on passenger doors of commercial aircraft fractured during torquing at less than the design load. Visual examination showed that cracking had occurred through a machined side hole. Fractography revealed that the cracks...
Series: ASM Failure Analysis Case Histories
Volume: 2
Publisher: ASM International
Published: 01 December 1993
DOI: 10.31399/asm.fach.v02.c9001361
EISBN: 978-1-62708-215-0
... Abstract A 17-4 PH steering actuator rod end body broke during normal take-off. Results of failure analysis revealed that the wall thickness of the race was much below the design limits, thus causing the race to rest on the body's swaged edges rather than on the load carrying centerline of the...
Series: ASM Failure Analysis Case Histories
Volume: 2
Publisher: ASM International
Published: 01 December 1993
DOI: 10.31399/asm.fach.v02.c9001363
EISBN: 978-1-62708-215-0
... the pitch control thrust bearing set, head bolts, hub fork, and actuator rod end, were examined in more detail The thrust bearing set (52100 steel) was identified as the probable source of the uncommanded pitch angle change. A complete failure analysis of the bearing indicated that failure was...
Series: ASM Failure Analysis Case Histories
Volume: 1
Publisher: ASM International
Published: 01 December 1992
DOI: 10.31399/asm.fach.v01.c9001132
EISBN: 978-1-62708-214-3
...-dispersive spectroscopy (EDS). The solder in the failed head cups showed some discoloration, and the presence of iron contamination was detected. The solder chemistries in all four heads were similar, containing bismuth, lead, tin, and cadmium. The demo unit, after being intentionally actuated using a...
Series: ASM Failure Analysis Case Histories
Volume: 3
Publisher: ASM International
Published: 01 December 2019
DOI: 10.31399/asm.fach.v03.c9001759
EISBN: 978-1-62708-241-9
... diameter. Heat treatment: liquid nitriding Furnace used: Deck India Engineering Pvt Ltd. Push-out load was measured by resting the bearing cup on locator. Load was applied gradually through rotary actuator. The bearing cup tested by push-out load test. Bearing cup was found to...
Series: ASM Failure Analysis Case Histories
Volume: 3
Publisher: ASM International
Published: 01 December 2019
DOI: 10.31399/asm.fach.v03.c9001793
EISBN: 978-1-62708-241-9
... FPP design is cheaper and easy to maintain, but a poor dynamic actuator. The CPP design, on the other hand, is an alternative for improved efficiency, especially in the need of a wide range of thrust and load levels, while maintaining an optimum shaft speed, as in the case of diesel or gas turbines...
Series: ASM Failure Analysis Case Histories
Volume: 1
Publisher: ASM International
Published: 01 December 1992
DOI: 10.31399/asm.fach.v01.c9001114
EISBN: 978-1-62708-214-3
... wellhead by a hydraulically actuated connector. Failure of the clamp resulted in the BOP stack dropping to the seafloor. The clamp had been in use for approximately 7 years. Fig. 1 Riser system for a floating drilling ridge. The clamp was purchased to API type 2 material. There are no specified...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.power.c9001473
EISBN: 978-1-62708-229-7
... fractured rim and portion of dislodged gantry crane. The turbine of the set that sustained the accident was also seriously damaged, the rotor being bent so that it fouled the casing; the column supporting the actuating cylinder for the control valve was broken and the oil feed pipes fractured. The...
Series: ASM Failure Analysis Case Histories
Volume: 1
Publisher: ASM International
Published: 01 December 1992
DOI: 10.31399/asm.fach.v01.c9001026
EISBN: 978-1-62708-214-3
... mode cannot be correlated consistently with elongation or notch strength properties. The flap supports constitute the attachment points to which the actuators for the wing leading edge flap are fastened ( Fig. 1 ). The outboard and inboard supports had fractured, leading to loss of the flap...
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006791
EISBN: 978-1-62708-295-2
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006785
EISBN: 978-1-62708-295-2
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006782
EISBN: 978-1-62708-295-2
Series: ASM Handbook
Volume: 11
Publisher: ASM International
Published: 15 January 2021
DOI: 10.31399/asm.hb.v11.a0006829
EISBN: 978-1-62708-295-2
... m ∗ ), using, for example, a hydraulic electromagnetic actuator. The latter alternated displacement results in a tangential force, Q (amplitude Q * ). The measured displacement, δ m , is obtained from an external extensometer (linear variable differential transformer, laser, etc.), while the...