Criteria

Text:
Sector:
Display:

Results

Viewing 1 to 30 of 1908
2015-12-01
Magazine
Uncertainty quantification The technique is a must for next-generation simulation tools. Oil-pump sizing Researchers from Hinduja Tech investigate options for low friction and power consumption. The future of Indian commercial aviation The growth in traffic that airport modernization has supported has also made a significant contribution to the local and national economies, while the improved infrastructure has been positive for the perception of India in the global market. Driving EVs toward lower cost The race ison to reduce battery and electric-drive systems cost while improving efficiency. Powering on Rolls-Royce's Chief Engineer discusses new technologies that inspire current R&D design and evaluation work as part of its strategic roadmap for future big commercial programs. HMIs extend beyond the cab Telematic functions are being integrated into multi-function user interfaces.
2011-10-26
Magazine
An icy reception Next-generation propulsion systems for next-generation aircraft still have to address an (ice) age old problem.
2017-01-24
WIP Standard
AIR7999
This SAE Aerospace Information Report (AIR) presents metrics for assessing the performance of diagnostic and prognostic algorithms applied to Engine Health Management (EHM) functions. This document consolidates and expands upon the metric information previously contained in AIR4985 and AIR5909. The emphasis is entirely on metrics and as such is intended to provide an extension and complement to such documents as ARP4176, which provides insight into how to create a cost benefit analysis to determine the justification for implementing an EHM system.
2017-03-14
WIP Standard
AIR5317A
The SAE Guide to APU health management establishes the foundation for developing a successful APU health management program at any aircraft or APU operator, such as an airline, an OEM, an equipment supplier, or a military transport unit. This guide identifies the best practices for using an APU health management program to improve dispatch reliability and to satisfy Extended Operations (ETOPS) availability requirements.
2013-04-24
WIP Standard
AIR6247
This document is intended to serve two purposes: (1) provide a list of topics for potential customers to ask of the facility to aid their selection decision-making, and (2) provide a list of icing wind tunnel and engine test stand facilities that simulate flight through icing or ice crystal clouds.
2016-05-17
WIP Standard
AIR6245
This document is applicable to military aircraft where stakeholders are seeking guidance on the development and approval of Structural Health Monitoring (SHM) technologies and on the integration of these technologies into encompassing maintenance and operational support systems. The document will refer to those guidelines prepared under SAE ARP6461 that are relevant and applicable to military applications.
2015-07-09
WIP Standard
AIR6341
The purpose of this AIR is to compile in one definitive source, commonly accepted calibration, acceptance criteria and procedures for simulation of Supercooled Large Droplet (SLD) conditions within icing wind tunnels. Facilities that meet the criteria for either some or all of the recognized conditions will have known SLD icing simulation capability.
2014-09-30
WIP Standard
AIR6334
This SAE Aerospace Information Report (AIR) examines the need for and the application of a power train usage metric that can be used to more accurately determine the TBO for helicopter transmissions. It provides a formula for the translation of the recorded torque history into mechanical usage. It provides examples of this process and recommends a way forward. This document of the SAE HM-1 IVHM Committee is not intended as a legal document and does not provide detailed implementation steps, but does address general implementation concerns and potential benefits.
2013-10-31
WIP Standard
AIR6287
The purpose of this SAE Aerospace Information Report (AIR) is to provide information regarding the basic requirements for environmental effects of composite materials used in ULDs. Material variances related to raw materials and manufacturing processes is not part of this information, nor is damage tolerance.
2014-12-05
WIP Standard
AIR1869D
This SAE Aerospace Information Report (AIR) covers information relative to ULDs (Unit Load Devices) container and pallet configurations, maximum usable container, pallet and bulk compartment volumes and tare weights for the lower deck of various wide-body aircraft. Bulk compartment volumes are also included for standard-body aircraft. This document brings together data concerning the lower deck capacity of wide-body and standard- body airplanes. The information includes airplanes manufactured by Airbus, Boeing, British Aerospace, British Aircraft, Fokker-VFW, Hawker Siddeley, Ilyushin, Lockheed and McDonnell- Douglas.
2000-04-01
Magazine
Looking to new aircraft configurations Researchers at Cranfield University's College of Aeronautics discuss the needs and benefits of studying different aircraft configurations such as the blended-wing body. Leading edge deicing Shape memory alloys, which can be trained to generate a compressive strain upon application of an electric current, show promise for deicing applications.
2001-07-01
Magazine
Giving ice the boot Atmospheric icing was for many years one of the majoy threats to aircraft safety- and it potentially still is. Researchers at Dunlop Aviation Ice Protection and Composites continue their development of deicing and anti-icing technologies. The art of wing assembly Airbus Industries investigates new technologies and techniques for improving quality and reducing cost of its wing box assemblies. Affordable engines for small aircraft A look into the new technologies developed for small-aircraft engines as extensions to the cooperative agreements under the NASA General Aviation Propulsion program conclude.
HISTORICAL
1981-10-01
Standard
AMS1427
This specification covers a propylene-glycol base, deicing/anti-icing fluid in the form of a concentrated liquid.
CURRENT
2010-07-14
Standard
AMS1427B
This specification covers a propylene-glycol base, deicing/anti-icing fluid in the form of a concentrated liquid.
HISTORICAL
1995-01-01
Standard
AMS1427A
HISTORICAL
1990-04-01
Standard
AMS1425B
This specification covers an ethylene glycol base deicing fluid in the form of a concentrated liquid.
HISTORICAL
1982-04-01
Standard
AMS1425A
This specification covers an ethylene glycol base deicing fluid in the form of a concentrated liquid.
CURRENT
2010-05-26
Standard
AMS1425D
This specification covers an ethylene glycol base deicing fluid in the form of a concentrated liquid.
HISTORICAL
1995-01-01
Standard
AMS1425C
HISTORICAL
1981-04-01
Standard
AMS1425
This specification covers an ethylene glycol base deicing fluid in the form of a concentrated liquid.
CURRENT
2016-05-05
Standard
AMS1424/2
The foundation specification (AMS1424M) and the category specifications (AMS1424/1 and AMS1424/2) cover deicing/anti-icing materials in the form of a fluid.
2016-05-18
WIP Standard
AMS1424/3
This detail specification AMS1424/3 covers the use of In-Truck Manufacturing of a deicing SAE Type I deicing/anti-icing fluid. This detailed specification contains technical and other requirements that apply for the In-Truck Manufacturing of Type I deicing/anti-icing fluid.
HISTORICAL
1991-10-01
Standard
AMS1731A
HISTORICAL
1979-10-15
Standard
AMS1731
CURRENT
1994-03-01
Standard
AMS1730B
This specification has been designated as "SUPERSEDED" by the Aerospace Materials Division, SAE, as of May 17, 1993. The requirements of this specification are embodied in the latest issue of AMS 1431.
HISTORICAL
1991-10-01
Standard
AMS1730A
Viewing 1 to 30 of 1908

Filter

  • Range:
    to:
  • Year: