Browse Topic: Interiors, Cabins, and Cockpits
In order to improve the efficiency of verification and optimization of control strategies for air-conditioning systems, a thermal management platform is established based on a rapid control prototyping (RCP) approach in the article. The platform is composed of a HVAC hardware bench, a real-time control system, and a control software model. This article describes the overall architecture of the platform, the control strategy, and an efficient method for development and optimization of air-conditioning control strategies. The cooling and heating modes of the air conditioner are tested. The results show that the control strategy can be directly modified via the platform to improve the performance of the whole system. The experimental results show that after modifying the control strategy, the cooling effect of the air conditioner is optimized and the cooling time is reduced by 10.6%. The CLTC cycle is also tested in this work to verify the dynamic control performance of the air
Electrification of vehicles plays an important role in the transformation process towards sustainable mobility in the individual and transport sector. As a result, new challenges must be met during the development process regarding the vehicles overall energy management system. A key challenge is the development of thermal management systems to optimize overall vehicle efficiency and to minimize ageing effects of the powertrain components while maintaining passenger comfort. Efficiency and ageing effects are highly dependent on the conditioning state of the powertrain components due to their high thermal sensitivity with simultaneously narrow thermal operating limits. Comfort functions like cabin air conditioning must be fulfilled as well, which must be considered by the thermal management system. To develop innovative solutions for thermal management systems at an early stage of the development process, thermal emulation can be used to substitute hardware components. Therefore
This SAE Aerospace Recommended Practice (ARP) contains methods used to measure the optical performance of airborne electronic flat panel display (FPD) systems. The methods described are specific to the direct view, liquid crystal matrix (x-y addressable) display technology used on aircraft flight decks. The focus of this document is on active matrix, liquid crystal displays (LCD). The majority of the procedures can be applied to other display technologies, however, it is cautioned that some techniques need to be tailored to different display technologies. The document covers monochrome and color LCD operation in the transmissive mode within the visual spectrum (the wavelength range of 380 to 780 nm). These procedures are adaptable to reflective and transflective displays paying special attention to the source illumination geometry. Photometric and colorimetric measurement procedures for airborne direct view CRT (cathode ray tube) displays are found in ARP1782. Optical measurement
This SAE Aerospace Recommended Practice (ARP) provides criteria for design and location of power supplies, controls, light fixtures, and associated equipment which are used to provide emergency illumination in transport aircraft, designed to comply with 14 CFR Part 25 (see Reference 1) for operation under 14 CFR Part 91 (see Reference 11) and 14 CFR Part 121 (see Reference 2), and also in compliance with FAA Advisory Circulars AC 25.812-1A (see Reference 3) and AC 25.812-2 (see Reference 10). It is not the purpose of an ARP to specify design methods to be followed in the accomplishment of the stated objectives.
ACT Expo 2025 had a fleet of new commercial vehicle launches as well as displays for models already on the market. One such existing chassis was the Workhorse W56, an electric step van designed for Class 5/6 last-mile delivery. Unlike many of its competitors, Workhorse did not set out to be a technological leader with the W56. Rather, the company took the approach of leveraging the best of the currently available and applicable technologies to produce a durable, reliable and producible product that just happened to be powered by electrons.
This document is a tool for the certifying authority, flight deck crew station designers, instrument suppliers, lighting suppliers, and component suppliers. It is an aid to understanding and meeting relevant regulatory requirements, particularly those relating to pilot compartment view (refer to 14 CFR § 25.773[a][2]) and instrument lights (refer to 14 CFR § 25.1381[a][2]) for glare arising from visible electromagnetic radiation.
This standard is intended to apply to portable compressed gaseous oxygen equipment. When properly configured, this equipment is used either for the administration of supplemental oxygen, first aid oxygen or smoke protection to one or more occupants of either private or commercial transport aircraft. This standard is applicable to the following types of portable oxygen equipment: a Continuous flow 1 Pre-set 2 Adjustable 3 Automatic b Demand flow 1 Straight-demand 2 Diluter-demand 3 Pressure-demand c Combination continuous flow and demand flow.
Current regulations (e.g., Title 14 of the United States Code of Federal Regulations, or 14 CFR) define design requirements for oxygen system provisions for protection of crewmembers and passengers following emergency events such as in-flight decompression. This aerospace information report (AIR) addresses the operational oxygen system requirements for a decompression incident that may occur at any point during a long-range flight, with an emphasis for a decompression at the equal time point (ETP). This AIR identifies fuel and oxygen management contingencies and presents possible solutions for the efficient, safe, and optimum fuel/oxygen flight continuation. Oxygen management is a critical concern for all aircraft, ranging from single-engine types operating above 10000 feet to complex, high-performance aircraft equipped with supplemental oxygen systems. Proper planning ensures compliance with regulations and supports pilot and passenger safety at higher altitudes. This document
This document recommends design and performance criteria for aircraft lighting systems used to illuminate flight deck controls, luminous visual displays used for transfer of information, and flight deck background and instrument surfaces that form the flight deck visual environment. This document is for aircraft, except for applications requiring night vision compatibility.
This SAE Aerospace Standard (AS) provides design criteria for onboard stairways intended for use by passengers aboard multi-deck transport category airplanes. It is not intended for stairways designed for use only by crewmembers, supernumeries, or maintenance personnel. Additionally, this AS does not apply to fuselage mounted or external stairways used for boarding passengers, which are covered by ARP836.
This SAE Recommend Practice establishes for passenger cars, light trucks, and multipurpose vehicles with GVW of 4500 kg (10000 pounds) or less, as defined by the EPA, and M1 category vehicles, as defined by the European Commission:
This SAE Standard applies to equipment to be used with R-1234yf refrigerant only. It establishes requirements for equipment used to recharge R-1234yf to an accuracy level that meets Section 9 of this document and purity levels defined in SAE J2099. Refrigerant service equipment is required to ensure adequate refrigerant recovery to reduce emissions and provide for accurate recharging of mobile air-conditioning systems. Equipment shall be certified to meet all performance requirements outlined in this document and international/regional construction and safety requirements as outlined in this document.
The sustainability trend continues to grow in the off-highway sector. Wherever possible, manufacturers rely on electric vehicles to contribute to climate protection goals. Therefore, heating and cooling solutions need to fit these given circumstances. Eliminating the traditional waste heat from the combustion engine requires new strategies for temperature regulation, for the cabin as well as for the battery. The aim is to efficiently control all thermally relevant areas in the vehicle.
Last summer, SAE Media was invited to Eaton's proving grounds in Marshall, Michigan, to test drive an electric truck the company had built in collaboration with BAE Systems. The truck was a showcase not only of BAE's powertrain control technology, but also of Eaton's new multi-speed heavy-duty EV transmission. That truck was on display at the 2025 ACT Expo, as was Eaton's transmission. SAE Media spoke with Scott Adams, SVP of technology and global products for Eaton, in Anaheim, California, about the company's portfolio of multi- and single-speed medium- and heavy-duty transmissions as well as other upcoming driveline offerings.
The desert landscapes of the western United States have changed since Mr. Duke and Dr. Gonzo blazed a trail across them in a drug-infused haze. But their advice to buy the ticket and take the ride is still a wise mantra - especially in the serene comfort of a modern full-size pickup. As inhospitable as southern Nevada can be outside Sin City, the amenities within the climate-controlled and leather-lined cabin of the latest Ram pickups insulate you from those realities. SAE Media was invited to sample the latest heavy haulers in Ram's portfolio, including the new 2500 and 3500 models with the high-output version of the Cummins B6.7 diesel.
This SAE Aerospace Standard (AS) defines minimum performance standards, qualification requirements, and minimum documentation requirements for passenger and crew seats in civil rotorcraft, transport aircraft, and general aviation aircraft. The goal is to achieve comfort, durability, and occupant protection under normal operational loads and to define test and evaluation criteria to demonstrate occupant protection when a seat/occupant/restraint system is subjected to statically applied ultimate loads and to dynamic impact test conditions set forth in Title 14, Code of Federal Regulations (14 CFR) parts 23, 25, 27, or 29 (as applicable to the seat type). Two formats of this standard (MS Excel and Adobe PDF) are available. The standards provided in both formats (MS Excel and Adobe PDF) contain the same text.
This SAE Standard provides testing and functional requirements to meet specified minimum performance criteria for electronic probe-type leak detectors, so they will identify smaller refrigerant leaks when servicing all motor vehicle air conditioning systems, including those engineered with improved sealing and smaller refrigerant charges to address environmental concerns and increase system efficiency. This document does not address any safety issues concerning their design or use.
In the early days of computers, interfaces were paper printouts or blinking lights, but as the technology matured, the graphical user interface (GUI) quickly became the standard.
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