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Aerospace & Defense™ Technology (11) Off-Highway Engineering® (4) MOBILITY ENGINEERING™ AUTOMOTIVE, AEROSPACE, OFF-HIGHWAY (3) Automotive Engineering® (2) Mobility Engineering Automotive, Aerospace, Off-Highway (1)

Series

General Industry (3) Spotlight on Design (3)

Reliability Case Analysis of an Autonomous Air Cooling System (AACS) for Aerospace Applications

  • IHI Corporation-Naoki Seki
  • University of Strathclyde-Chung Man Fong, Patrick Norman
  • Technical Paper
  • 2018-01-1916
To be published on 2018-10-30 by SAE International in United States
Current More Electric Aircraft (MEA) utilize Liquid Cooling Systems (LCS) for cooling on-board power electronics. In such LCS, coolant pipes around the structure of the aircraft are used to supply water glycol based coolant to sink heat from power electronics and other heat loads in the electronic bay. Subsequent extracted heat is then transferred to ram air through downstream heat exchanger/s. This paper presents a reliability examination of a proposed alternative Autonomous Air Cooling System (AACS) for a twin engine civil MEA case study. The proposed AACS compared to the LCS, utilizes cabin air as the coolant which is in turn supplied using the electric Environmental Control System (ECS) within the MEA. The AACS consist of electrical blowers allocated to each heat load which subsequently drive the outflow cabin air through the heat sinks of the power electronics for heat extraction. No additional heat exchanger is required after this stage in which the heated air is directly expelled overboard. One key advantage is that higher levels of control are possible for the attainment of higher system efficiency. The other key advantage is the avoidance of liquid coolant leakage risks with the removal of liquid coolant from the MEA. However, to justify the potential application of this new approach, the reliability is required to be in line with FAA/JAA reliability limits. As such, the provided reliability analysis in this paper covers the reliability of such AACS as well as the subsequent operation of safety critical components of the ECS and Electrical Power System (EPS) that the AACS is cooling. The case study results show such a proposed AACS can provide comparable reliability and within FAA/JAA reliability limits.

Power Quality Test Data Analysis for Aircraft Subsystem

  • UTC Aerospace Systems-Shobha Ramanjani
  • Technical Paper
  • 2018-01-1932
To be published on 2018-10-30 by SAE International in United States
Aircraft subsystem development involves various combinations of testing and qualification activities to realize a flight worthy system. The subsystem needs to be verified for a massive number of customer requirements. Power Quality (PQ) testing is also an important testing activity carried out as a part of the environmental qualification test. It is intended to verify the functionality of subsystem with various power disturbances, to determine the ability of a subsystem to withstand power quality disturbances. The subsystem being designed should be reliable enough to handle power quality anomalies. Power quality test generates an enormous amount of test result data for analysis with millions of data samples depending on the test, and can be identified as Big Data. The engineer needs to analyze each set of test data as a part of post processing to ensure the power disturbances during testing are as per the standard requirements and functional performance of the subsystem is met. Manually analyzing the test data with classical methods and generating the report requires more time and effort, as it needs analysis of millions of test data samples, also leading to the possibility of errors. Hence it is required to have automated methods to perform unsupervised data analysis in a faster way and generate the post processed report as required by the end user. This paper presents the testing of aircraft subsystem, for power quality with various power input disturbances involved, mainly focusing on test data analysis techniques using script based analysis tools. Also, it discusses on the utilization of options available in various tools for automation of test data analysis and presentation.
new

Air and Air/Surface (Platform) Cargo Pallet Nets

  • AGE-2 Air Cargo
  • Aerospace Standard
  • AS1131C
  • Current
Published 2018-10-18 by SAE International in United States
This SAE Aerospace Standard (AS) provides dimensional, structural and environmental requirements for pallet nets to be used in conjunction with 2.44 m (8 ft) wide pallets described in AS1130. The pallet/net combination are used in freighter versions of certificated aircraft equipped to provide restraint to pallets tested to the requirements of NAS 3610 Class II restraint system. The minimum essential criteria are identified by use of the key word "shall". Recommended criteria are identified by use of the key word "should", and while not mandatory, are considered to be primary importance in providing serviceable, economical, and practical air transport pallet nets. Deviation from recommended criteria should occur only after careful consideration, extensive testing, and thorough service evaluation have shown alternate methods to be satisfactory.
new

Air Cargo Pallets and Nets Compatibility

  • AGE-2 Air Cargo
  • Aerospace Standard
  • ARP36104A
  • Current
Published 2018-10-18 by SAE International in United States
This SAE Aerospace Recommended Practice (ARP) provides the criteria to be applied in order to determine compatibility with each other of an air cargo pallet and air cargo pallet net airworthiness approved under either NAS 3610 [TSO C90c] or AS36100A [TSO pending] performance and testing requirements.
new

Certified Containers for Lower Deck Compartments

  • AGE-2 Air Cargo
  • Aerospace Standard
  • AS5896
  • Current
Published 2018-10-18 by SAE International in United States
This SAE Aerospace Standard (AS) covers the design, fabrication, performance, and testing requirements for general-purpose, base-restrained, containers requiring airworthiness approval for installation/use in aircraft lower deck compartments. See 10.1 and 10.2.
new

Nickel Alloy, Corrosion and Heat-Resistant, Wire 74Ni - 15.5Cr - 8.0Fe Cold Reduced, Spring Temper

  • AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5961A
  • Current
Published 2018-10-10 by SAE International in United States
This specification covers a corrosion and heat-resistant nickel alloy in the form of wire.
new

Nickel Alloy, Corrosion and Heat-Resistant, Welding Wire 78Ni - 20Cr

  • AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5682E
  • Current
Published 2018-10-10 by SAE International in United States
This specification covers a corrosion and heat-resistant nickel alloy in the form of rods and wire.
new

Nickel Alloy, Corrosion and Heat-Resistant, Welding Wire 62Ni - 21.5Cr - 9.0Mo - 3.7Cb(Nb)

  • AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5837G
  • Current
Published 2018-10-10 by SAE International in United States
This specification covers a corrosion and heat-resistant nickel alloy in the form of welding wire.
new

Steel Castings, Vacuum Melted, Vacuum Cast, Investment, Corrosion-Resistant 13Cr - 8.0Ni - 2.2Mo - 1.1Al (195 ksi (1344 MPa) Tensile Strength (Condition H1000) Homogenized, Solution, and Precipitation Heat Treated

  • AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5412A
  • Current
Published 2018-10-10 by SAE International in United States
This specification covers a corrosion-resistant steel in the form of investment castings.
new

INSTALLING AND REMOVAL TOOLS, CONNECTOR ELECTRICAL CONTACT, TYPE I, CLASS 1, COMPOSITION C

  • AE-8C2 Terminating Devices and Tooling Committee
  • Aerospace Standard
  • AS81969/18
  • Current
Published 2018-10-10 by SAE International in United States
No Abstract Available.