Browse Topic: Stop / start technology

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This document covers the requirements for SAE implementations based on ISO 17987:2016. Requirements stated in this document will provide a minimum standard level of performance to which all compatible ECUs and media shall be designed. This will assure full serial data communication among all connected devices regardless of supplier.The goal of SAE J2602-1 is to improve the interoperability and interchangeability of LIN devices within a network by adding additional requirements that are not present in ISO 17987:2016 (e.g., fault tolerant operation, network topology, etc.).The intended audience includes, but is not limited to, ECU suppliers, LIN controller suppliers, LIN transceiver suppliers, component release engineers, and vehicle system engineers.The term “master” has been replaced by “commander” and term “slave” with “responder” in the following sections.
Vehicle Architecture For Data Communications Standards
This SAE Aerospace Recommended Practice (ARP) defines a means of assessing the credibility of computer models of aircraft seating systems used to simulate dynamic impact conditions set forth in Title 14, Code of Federal Regulations (14 CFR) Parts 23.562, 25.562, 27.562, and 29.562. The ARP is applicable to lumped mass and detailed finite element seat models. This includes specifications and performance criteria for aviation specific virtual anthropomorphic test devices (v-ATDs). This document provides a recommended methodology to evaluate the degree of correlation between a seat model and dynamic impact tests. This ARP also provides best practices for testing and modeling designed to support the implementation of analytical models of aircraft seat systems. Supporting information within this document includes procedures for the quantitative comparison of test and simulation results, as well as test summaries for data generated to support the development of v-ATDs and a sample v-ATD
Aircraft SEAT Committee
In recent years, start-stop systems have been implemented by many OEMs for improvement of fuel economy. When the engine stops, the occupant comfort typically deteriorates. Hence, the climate and fuel economy engineers are struggling to combine the passenger comfort and fuel economy. Especially in a vehicle cabin where the thermal environment becomes unsteady and highly non-uniform due to a start-stop. It is difficult to adapt any comfort evaluation index that have already been well established for a stationary/uniform space in building type environment in comparison to a vehicle cabin interior. The existing standard of ISO-14505-2 does not consider this for vehicle cabin interior condition. Hence, the authors have developed the occupant’s comfort prediction method under highly non-uniform condition and unsteady conditions and have established a new methodology [1].
Morishita, MasahiroUchida, ToshiyaMathur, Gursaran D.Kato, TakenaoMatsunaga, Kazuhiko
ABSTRACT Condition (Usage) Based Maintenance (CBM) function is becoming a standard and classical investigation topic for Original Equipment Manufacturers (OEM) for many reasons. Significant benefits can be earned by developing and using such functions: Better knowledge of the customer's usage of the helicopters, improvements in the building of the Design Usage Spectrums (DUS) for both high cycle fatigue mode (time ratio spent and occurrences of flight regimes) and low cycle fatigue mode (start/stop cycles, landing/take-off cycles, torque cycles, -), better understanding of the customer's own fleet's management, and of course maintenance optimization. In order to achieve this target and in particular the maintenance burden reduction, AH has developed a complete end-to-end CBM function proven to be efficient for customers. This paper intends to describe briefly the general concept already published, recall the expected benefits previously evaluated on H225, and focus deeper on the
Laillet, EmmanuelMaisonneuve, Pierre-LoicReveillon, Damien
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