Find the standard you are looking for at Engineering360. Documents are available for purchase from the IHS Standards Store.

1 - 20 of 617 results

SAE AIR4566 - CRASHWORTHY LANDING GEAR DESIGN Organization: SAE
Date: 2010-05-01
Description: The intent of this SAE Aerospace Information Report (AIR) is to document the design requirements and approaches for the crashworthy design of aircraft landing gear. This document covers the field of commercial and military airplanes and helicopters.
SAE AE-15 - GEAR DESIGN, MANUFACTURING AND INSPECTION MANUAL - ***TO PURCHASE: CONTACT IHS AT 1-800-854-7179 USA/CANADA OR 303-397-7956 WORLDWIDE*** Organization: SAE
Date: 1990-01-01
Description: The gear design section of this handbook provides state-of-the- art information in the form of technical papers and articles.
SAE AIR1494 - VERIFICATION OF LANDING GEAR DESIGN STRENGTH Organization: SAE
Date: 2010-04-01
Description: Verification of landing gear design strength is accomplished by dynamic and static test programs. This is essentially a verification of the analytical procedures used to design the gear.
AGMA 10FTM17 - SELF-LOCKING GEARS: DESIGN AND POTENTIAL APPLICATIONS Organization: AGMA
Date: 2010-10-01
Description: The paper describes the design approach as well as potential applications of the parallel axis self-locking gears. These gears, unlike the worm gears don't have such application limitations.
AGMA 05FTM01 - FINE PITCH, PLASTIC FACE GEARS: DESIGN AND MANUFACTURE Organization: AGMA
Date: 2005-10-01
Description: More applications could benefit, justifying the need formore information on the special features of face gears, their design and manufacture, in comparison to other non--parallel--shaft gears. A description of manufacturing methods, particularly in plastic molding is given with inter--related design and gear performance issues.
AGMA 02FTM11 - A GEAR DESIGN OPTIMIZATION PROCEDURE THAT IDENTIFIES ROBUST, MINIMUM STRESS AND MINIMUM NOISE GEAR PAIR DESIGNS Organization: AGMA
Date: 2002-10-01
Description: Gear Design Optimization Procedure that Identifies Robust, Minimum Stress and Minimum Noise Gear Pair Designs By: Donald R.
AGMA 12FTM16 - GEAR DESIGN OPTIMIZATION FOR LOW CONTACT TEMPERATURE OF A HIGH-SPEED, NON-LUBRICATED SPUR GEAR PAIR Organization: AGMA
Date: 2012-10-01
Description: This paper presents a gear design optimization approach that was applied to reduce both tooth contact temperature and noise excitation of a high­speed spur gear pair running without lubricant. The optimum gear design search was done using the RMC (Run Many Cases) program from The Ohio State University.
AGMA 10FTM08 - CALCULATION OF LOAD DISTRIBUTION IN PLANETARY GEARS FOR AN EFFECTIVE GEAR DESIGN PROCESS Organization: AGMA
Date: 2010-10-01
Description: The design of gears - especially planetary gears - can just be carried out by the consideration of influences of the whole drive train and the analysis of all relevant machine elements.
AGMA 93FTM5 - OPTIMAL GEAR DESIGN FOR EQUAL STRENGTH TEETH USING ADDENDUM MODIFICATION COEFFICIENTS Organization: AGMA
Date: 1993-10-01
Description: Defines the addendum modification coefficient (shift factor) and explains it in terms of gear design terminology. Shows the derivation of two types of helical gear design equations, one with the true generating shift factor, and the other with an addendum modification factor.
AGMA 10FTM13 - GEAR DESIGN FOR WIND TURBINE GEARBOXES TO AVOID TONAL NOISE ACCORDING TO ISO/IEC 61400-11 Organization: AGMA
Date: 2010-10-01
Description: The paper will give recommendations regarding a gear design process that is considering tonal noise in the design stage and will compare an, regarding tonal noise, improved gear set with an older one.
AGMA 14FTM10 - INVOLUTE SPIRAL FACE COUPLINGS AND GEARS: DESIGN APPROACH AND MANUFACTURING TECHNIQUE Organization: AGMA
Date: 2014-10-01
Description: It also explains a hobbing method of these gears and tool design specifics, and then illustrates gear and tool design with numerical examples.
AGMA 13FTM11 - STRIVING FOR HIGH LOAD CAPACITY AND LOW NOISE EXCITATION IN GEAR DESIGN Organization: AGMA
Date: 2013-09-01
Description: Defining the macrogeometry of the teeth regarding load capacity calculation according to standards leads to a reasonable gear design. On that basis, the micro geometry of the teeth is specified and load distribution as well as noise excitation is calculated.
FORD W-GG1 - MASTER GEAR DESIGN STANDARD Organization: FORD
Date: 1999-12-01
AGMA 05FTM17 - INFLUENCES OF BEARING LIFE CONSIDERATIONS ON GEAR DRIVE DESIGN Organization: AGMA
Date: 2005-10-01
Description: Historically, catalog gear drives have been designed with 5000 hours of L10 bearing life at service factor 1.0 power.
TECHNOMIC - HANDBOOK OF PRACTICAL - HANDBOOK OF PRACTICAL GEAR DESIGN Organization: TECHNOMIC
ESDU 77002 - DESIGN OF PARALLEL AXIS STRAIGHT SPUR AND HELICAL GEARS: GEOMETRIC DESIGN. Organization: ESDU
Date: 1981-07-01
Description: ESDU 77002 provides data for geometric gear design for gear ratios up to 10:1. Guidance on the choice between spur and helical gears is provided by considering the factors of noise, end-thrust and cost.
AGMA 911 - DESIGN GUIDELINES FOR AEROSPACE GEARING Organization: AGMA
Date: 1994-01-01
Description: Covers current gear design practices as they are applied to air vehicles and spacecraft. Goes beyond the design of gear meshes.
AGMA ISO 22849 - DESIGN RECOMMENDATIONS FOR BEVEL GEARS Organization: AGMA
Date: 2012-05-07
Description: It provides additional information on the application, manufacturing, strength and efficiency of bevel gears for consideration in the design stage of a new bevel gear set. It is intended to supplement ANSI/AGMA ISO 23509, Bevel and Hypoid Gear Geometry, and is an identical adoption of ISO/TR 22849.
DS/ISO/TR 22849 - DESIGN RECOMMENDATIONS FOR BEVEL GEARS Organization: DS
Date: 2011-07-15
Description: This Technical Report provides additional information on the application, manufacturing, strength and efficiency of bevel gears for consideration in the design stage of a new bevel gear set. The term "bevel gear" is used to mean straight, spiral, zerol bevel and hypoid gear designs.
ISO TR 22849 - DESIGN RECOMMENDATIONS FOR BEVEL GEARS - FIRST EDITION; INCLUDES ACCESS TO ADDITIONAL CONTENT Organization: ISO
Date: 2011-04-15
Description: This Technical Report provides additional information on the application, manufacturing, strength and efficiency of bevel gears for consideration in the design stage of a new bevel gear set. The term "bevel gear" is used to mean straight, spiral, zerol bevel and hypoid gear designs.

1 - 20 of 617 results