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Book

Honda R&D Technical Review April 2021

2021-04-01

Honda R&D Technical Review is a periodical containing research papers related to Honda R&D Center activities worldwide that cover automobile, motorcycle, power products, aircraft engine, and other fundamental technologies. Honda Motor offers a book for the April 2021 issue with 104 pages containing 12 papers focusing on the following latest topics: Technology for Prediction of Contactor Noise for Electric-powered Vehicle Batteries Reduction of Internal Resistance in High Capacity Lithium-ion Batteries with 3D Lattice-structured Electrode Predictive Technique for Seat Belt Submarining Injury by Triaxial Iliac Load Cell

Event

Contact - Hybrid and Electric Vehicle Technologies Symposium

2022-03-17

Event

Exhibit - Hybrid and EV Symposium, an SAE Sustainability Event

2022-03-17

Standard

J1349 Certified Power Engine Data for Ford as used in 2009 Ford Expedition / Lincoln Navigator - Level 1

2008-04-10

CURRENT

CPFD1_09EXPNAV

This product includes information on the manufacturer, engine, application, testing location, certified maximum horsepower, certified maximum torque along with the certified curves of horsepower and torque over a wide range of engine RPM speeds.

Standard

J1349 Certified Power Engine Data for Ford Expedition / Lincoln Navigator - Level 2

2008-04-10

CURRENT

CPFD2_09EXPNAV

This product includes information on the manufacturer, engine, applications, testing location, certified maximum horsepower, certified maximum torque along with the certified curves of horsepower and torque over a wide range of engine RPM speeds. In addition, this product contains complete engine information such as displacement, cylinder configuration, valve train, combustion cycle, pressure charging, charge air cooling, bore, stroke, cylinder numbering convention, firing order, compression ratio, fuel system, fuel system pressure, ignition system, knock control, intake manifold, exhaust manifold, cooling system, coolant liquid, thermostat, cooling fan, lubricating oil, fuel, fuel shut off speed, etc. Also included are all measured test parameters outlined in J2723.

Standard

J1349 Certified Power Engine Data for GM LNF as used in 2007 Pontiac Solstice/Saturn Sky Level 1

2006-08-01

CURRENT

CPGM1_07LNF

This product includes information on the manufacturer, engine, application, testing location, certified maximum horsepower, certified maximum torque along with the certified curves of horsepower and torque over a wide range of engine RPM speeds.

Standard

J1349 Certified Power Engine Data for GM LLT as used in 2010 Cadillac CTS Wagon - Level 2

2008-12-10

CURRENT

CPGM2_10CADWAG

This product includes information on the manufacturer, engine, applications, testing location, certified maximum horsepower, certified maximum torque along with the certified curves of horsepower and torque over a wide range of engine RPM speeds. In addition, this product contains complete engine information such as displacement, cylinder configuration, valve train, combustion cycle, pressure charging, charge air cooling, bore, stroke, cylinder numbering convention, firing order, compression ratio, fuel system, fuel system pressure, ignition system, knock control, intake manifold, exhaust manifold, cooling system, coolant liquid, thermostat, cooling fan, lubricating oil, fuel, fuel shut off speed, etc. Also included are all measured test parameters outlined in J2723.

Standard

J1349 Certified Power Engine Data for GM LE5 as used in 2007 Chevrolet HHR

2006-08-01

CURRENT

CPGM1_LE5HHR

This product includes information on the manufacturer, engine, application, testing location, certified maximum horsepower, certified maximum torque along with the certified curves of horsepower and torque over a wide range of engine RPM speeds.

Standard

Fuel Fired Engine Preheaters and Their Application

2002-12-16

CURRENT

J1327_200212

Standard

Combination Tail and Floodlamp for Industrial Equipment

2003-05-15

CURRENT

J94_200305

This SAE Standard provides performance and general design requirements and related test procedures for a combination tail and floodlamp for use on industrial wheeled equipment that may be operated on public roads.

Standard

TOLERANCES, METRIC Aluminum Alloy Drawn Tubing

1994-09-01

MAM2203B

Standard

TOLERANCES, METRIC Aluminum Alloy Drawn Tubing

1994-04-01

MAM2203A

This specification covers established metric manufacturing tolerances applicable to aluminum alloy drawn tubing ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" applies only to the higher figure of the specified range.

Standard

TOLERANCES, METRIC Aluminum Alloy Drawn Tubing

2002-07-23

MAM2203

This specification covers established metric manufacturing tolerances applicable to aluminum alloy drawn tubing ordered to metric dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "excl" applies only to the higher figure of the specified range.

Standard

COMMUNICATIONS MANAGEMENT UNIT (CMU) MARK 2

2019-11-26

CURRENT

ARINC758-4

This ARINC Standard specifies the ARINC 758 Mark 2 Communications Management Unit (CMU) as an on-board message router capable of managing various datalink networks and services available to the aircraft. Supplement 4 adds Ethernet interfaces, per ARINC Specification 664 Part 2. This will allow the CMU to communicate with IP based radio transceivers (e.g., L-Band Satellite Communication Systems (Inmarsat SwiftBroadband (SBB) and Iridium Certus), ACARS over IP, AeroMACS, etc.).

Standard

CABIN CONNECTORS AND CABLES PART 2 SPECIFICATION OF CONNECTORS, CONTACTS, AND BACKSHELLS

2018-11-28

CURRENT

ARINC800P2-1

This specification describes the general connectors, contacts, and backshells in their shape and characteristic for cabin systems for commercial aircrafts. ARINC 600, ARINC 404, and ARINC 801 connector specifications are published as independent standards.

Standard

CABIN CONNECTORS AND CABLES PART 2 SPECIFICATION OF CONNECTORS, CONTACTS, AND BACKSHELLS

2021-09-09

CURRENT

ARINC800P2-2

This specification describes the general connectors, contacts, and backshells in their shape and characteristic for cabin systems for commercial aircrafts. ARINC 600, ARINC 404, and ARINC 801 connector specifications are published as independent standards.

Standard

Manufacturing Message Specification – Service Definition and Protocol

2016-06-28

CURRENT

EIA511

The Manufacturing Message Specification is an application layer Standard designed to support messaging communications to and from programmable devices in a Computer Integrated Manufacturing (CIM) environment. This environment is referred to in this Standard as the manufacturing environment. This Standard does not specify a complete set of services for remote programming of devices, although provision of such a set of services may be the subject of future standardization efforts.

Standard

AIRCRAFT DATA NETWORK, PART 1, SYSTEMS CONCEPTS AND OVERVIEW

2019-06-20

CURRENT

ARINC664P1-2

The purpose of this document is to provide an overview of data networking standards recommended for use in commercial aircraft installations. These standards provide a means to adapt commercially defined networking standards to an aircraft environment. It refers to devices such as bridges, switches, routers and hubs and their use in an aircraft environment. This equipment, when installed in a network topology, can optimize data transfer and overall avionics performance.

Standard

GUIDANCE FOR DISTRIBUTED RADIO ARCHITECTURES

2021-07-15

CURRENT

ARINC678

The purpose of this document is to evaluate Communication, Navigation, and Surveillance (CNS) Distributed Radio architectures and the feasibility of distributing the RF and systems processing sections to ensure the following: Reduce cost of equipment Reduce Size, Weight, and Power (SWaP) Ease of aircraft integration Growth capability built into the design Maintain or improve system availability, reliability, and maintainability It provides a framework to determine whether it is feasible to develop ARINC Standards that support CNS distributed radio architectures.

Standard

AIRCRAFT AUTONOMOUS DISTRESS TRACKING (ADT)

2019-08-26

CURRENT

ARINC680

This document describes the technical requirements, architectural options, and recommended interface standards to support an Autonomous Distress Tracking (ADT) System intended to meet global regulatory requirements for locating aircraft in distress situations and after an accident. This document is prepared in response to International Civil Aviation Organization (ICAO) and individual Civil Aviation Authorities (CAAs) initiatives.