Search Results

Training / Education

Design for Manufacturing & Assembly

Design for Manufacturing and Assembly (DFM+A), pioneered by Boothroyd and Dewhurst, has been used by many companies around the world to develop creative product designs that use optimal manufacturing and assembly processes.  Correctly applied, DFM+A analysis leads to significant reductions in production cost, without compromising product time-to-market goals, functionality, quality, serviceability, or other attributes.  This course will include information on how DFM+A fits in with QFD, Concurrent Engineering, Robust Engineering, and other disciplines.

Training / Education

Introduction to Airframe Engineering Design for Manufacturing, Assembly and Automation

This course is verified by Probitas Authentication as meeting the AS9104/3A requirements for continuing Professional Development. Why is a design for manufacturing, assembly and automation so important? This introductory course on airframe engineering will cover the importance of design for manufacturing, assembly and automation in aerospace. It will review what the key drivers are for a “good” design and some of the key points for manufacturing and assembly of aircraft components. It will look at how an engineer can combine traditional technologies with new, cutting-edge technologies, to determine the best scenario for success.

Training / Education

Design for Manufacturing & Assembly (DFM/DFA)

2024-05-13

Design for Manufacturing and Assembly (DFM+A), pioneered by Boothroyd and Dewhurst, has been used by many companies around the world to develop creative product designs that use optimal manufacturing and assembly processes. Correctly applied, DFM+A analysis leads to significant reductions in production cost, without compromising product time-to-market goals, functionality, quality, serviceability, or other attributes. In this two-day course, you will not only learn the Boothroyd Dewhurst Method, you will actually apply it to your own product design!

Standard

Alloy Sheet and Strip, Corrosion and Heat Resistant Cobalt Base 25.5cr 20ni 4mo 2w 2(Cb+Ta)

2002-12-16

CURRENT

AMS5535

Standard

STEEL, NITRIDING .65 Ni 1 Cr 1 Mo

1946-04-01

HISTORICAL

AMS6480

Standard

STEEL TUBING (WELDED) Chromium Molybdenum (.27 - .33 Carbon) (Normalized)

1942-06-01

HISTORICAL

AMS6510

Standard

STEEL Nickel Molybdenum

1939-12-04

HISTORICAL

AMS6310

Standard

STEEL Nickel Molybdenum

1942-03-01

HISTORICAL

AMS6315A

Standard

STEEL 1.8 Ni - .25 Mo (.38 - .43C) Heat Treated (105,000 TS)

1945-07-01

HISTORICAL

AMS6315B

Standard

Steel Corrosion and Heat Resistant 19cr 12ni 3.2w 1cb 0.15n

2002-12-16

CURRENT

AMS5730

Standard

Alloy, Corrosion and Heat Resistant 37ni 20co 18cr 3mo 2.9ti

1949-01-01

CURRENT

AMS5760

Parts, such as bolts, turbine wheels, discs, buckets, and blades, for high strength and oxidation resistance up to 1500 F when suitably heat treated.

Standard

STEEL COTTER PINS, GALVANIZED Low Carbon

1942-12-01

CURRENT

AMS7212

Standard

NUTS, SELF-LOCKING, STEEL High Strength, Prevailing-Torque, All Metal 450 F (232 C) Use, Unified "J" (MIL-S-8879) Thread Form

1969-11-01

HISTORICAL

AMS7252

Standard

NUTS, SELF-LOCKING, STEEL High Strength, All Metal 450° F (230° C) Use, Unified "J" (MIL-S-8879) Thread Form

1980-01-15

HISTORICAL

AMS7252B

This specification covers all-metal, self-locking nuts, plate nuts, and gang channel nuts made of a carbon or low-alloy steel.

Standard

NUTS, SELF-LOCKING, STEEL High Strength, Prevailing Torque, All Metal 450° F (232° C) Use, Unified "J" (MIL-S-8879) Thread Form

1973-05-15

HISTORICAL

AMS7252A

This specification covers all-metal, self-locking, prevailing-torque nuts, plate nuts, and gang channel nuts made of a carbon or low-alloy steel.

Standard

Vehicle Electronic Identification

2002-07-23

CURRENT

J1724_200207

Standard

Nickel Alloy, Corrosion and Heat Resistant, Sheet, Strip, and Plate 72Ni - 15.5Cr - 0.95 (Cb + Ta) - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode or Vacuum Induction Melted Solution Heat Treated, Precipitation Hardenable

2000-05-01

HISTORICAL

MAM5598B

This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate procured in SI (metric) units.

Standard

NICKEL ALLOY, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE 72Ni - 15.5Cr - 0.95(Cb + Ta) - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode or Vacuum Induction Melted Solution Heat Treated, Precipitation Hardenable

1993-07-01

HISTORICAL

MAM5598A

This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate procured in SI (metric) units.

Standard

ALLOY SHEET, STRIP, AND PLATE, CORROSION AND HEAT RESISTANT 72Ni - 15.5Cr - 0.95(Cb + Ta) - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode or Vacuum Induction Melted Solution Heat Treated, Precipitation Hardenable

1991-10-01

HISTORICAL

MAM5598

This specification covers a corrosion and heat resistant nickel alloy in the form of sheet, strip, and plate procured in SI (metric) units. AMS 5598 is the equivalent, specified in inch/pound units, of this MAM.

Video

Business Model for Successful Commercialization of Aircraft Designs

2012-03-21

This article characterizes the special features of drilling of CFRP/Titanium and -Aluminium stacks. Simplified theoretic models will show how CFRP/Titanium stacks should be machined without scratches and burn marks contacting carbon. Low axial forces and smart chip removal technology are the main characteristics of the drilling tool technology, optimized to reach H8 quality in one shot operation. Presenter Peter Mueller-Hummel, Cutting Tools Inc.