Browse Topic: Fire detection
This document is reissued for application to helicopters.
A new device known as MC-TENG — short for multilayered cylindrical triboelectric nanogenerator — generates electrical power by harvesting energy from the sporadic movement of the tree branches from which it hangs. The self-powered sensing system could continuously monitor the fire and environmental conditions without requiring maintenance after deployment.
Solar or photovoltaic (PV) cells fixed to roofs convert sunlight into electricity. Bringing that technology indoors could further boost the energy efficiency of buildings and energize swaths of wireless smart technologies such as smoke alarms, cameras, and temperature sensors.
This SAE Aerospace Standard (AS) describes the test methods to determine the flammability performance and capability to control the passage of, and effects from, fire on aircraft firewall sealing compounds. The methods are based requirements of FAR Part 25 Sections 25.865, 25.867, 25.1191, and 25.1193 and may be used to demonstrate compliance with the requirements established by FAA AC 20-135. This standard shall be used in conjunction with applicable material specifications.
Wildfires that start in backcountry areas sometimes burn for hours before being detected and reported. Satellites offer a vantage point from which infrared sensors can detect fires. Individual satellites in low Earth orbit (LEO) offer infrequent overpasses, making the delay from ignition to detection unacceptably long. Geostationary satellites offer a platform from which to maintain a round-the-clock vigil, but lack geographic precision, and cannot detect a rather small fire within a large pixel definitively above noise.
The National Aeronautics and Space Administration (NASA) uses large quantities of liquid hydrogen and has expended significant effort in the development, testing, installation, and maintenance of hydrogen fire detectors based on ultraviolet, near-infrared, mid-infrared, and/or far-infrared flame emission bands. Yet, prior to this work, there was no intensity-calibrated broadband hydrogen-air flame spectrum in the literature, making it difficult to compare the merits of different radiation-based hydrogen fire detectors.
This SAE Aerospace Standard (AS) describes the procedures for the flammability testing of aircraft firewall sealants in accordance with the requirements of FAR Part 25 Sections 25.865, 25.867, 25.1191, and 25.1193. This test method is intended to determine the capability of sealant materials to control the passage of and effects from fire.
Traditional smoke opacity measurement, performed on diesel engines during regular emissions inspections, sensitive primarily to larger particles of elemental carbon, is very little sensitive to nanoparticles and to semi-volatile “organic carbon” particles. For this reason, it no longer suffices as a high emitter detection tool for modern vehicles with a particle filter or for advanced low-emissions technology where semi-volatile organic particles are the dominant fraction of particulate matter. This paper investigates the potential of common low-cost ionization type smoke detectors, produced in mass quantities for fire detection in buildings, as a tool to measure particle emissions in vehicular exhaust. Two ionization chambers were used to measure both raw and diluted exhaust of various engines powered by diesel fuel and biofuels under laboratory conditions as well as on the road. Laboratory results suggest that the ionization chamber signal correlates best to total particle length, with correlation to number and mass dependent on particle size distribution. Particle filter regeneration events were clearly discerned from the ionization chamber readings. With detection limits on the order of 0.1 mg/m3 and 106 particles/cm3 in raw exhaust, the method appears to be sufficiently sensitive for inspection of vehicles equipped with particle filters and for preliminary measurements of particle emissions from modern engines.
This SAE Aerospace Standard (AS) describes the procedures for the flammability testing of aircraft firewall sealants in accordance with the requirements of FAR Part 25 Sections 25.865, 25.867, 25.1191, and 25.1193. This test method is intended to determine the capability of sealant materials to control the passage of and effects from fire.
A document discusses an optical carbon monoxide sensor for early fire detection. During the sensor development, a concept was implemented to allow reliable carbon monoxide detection in the presence of interfering absorption signals.
This paper presents the results achieved, to date, through a collaborative technology project of Bell Helicopter Textron Inc. and AAI Corporation, an operating unit of Textron Systems Inc., to develop and demonstrate a hostile fire detection system (HFDS) for rotorcraft. This includes an assessment of the potential application of an airborne gunshot detection system for rotorcraft conducting parapublic operations. Law enforcement (LE) can locate and react to gunshot incidences with increased urgency and decreased response times by using an HFDS. This project leverages the AAI Projectile Detection and Cueing® (PDCue®) gunshot detection system originally developed for ground vehicles. The HFDS enables solutions providing azimuth, elevation, and range information. The HFDS can provide continuous target location information and target tracking when coupled with a remote weapon system, camera, or other sensor device. Flight tests have confirmed the ability of the HFDS to detect, identify, and locate hostile fire in a rotorcraft downwash environment.
Distinctly different fire hazards exist within the engine compartment of a transit vehicle and various detection methodologies may be employed to detect fire events arising from these hazards. The engine compartment presents a particularly challenging environment and it is important to select the correct methodology to ensure timely detection response in the early stages of the development of a fire whilst minimizing nuisance alarms. The choice of the correct detection methodology for a specific fire hazard is therefore determined by the suitability of the methodology for the detection of the anticipated fire event within the environment in which it is required to operate. This paper presents experimental data to demonstrate the variation in the response times of different detection methodologies in the presence of common fire events in the form of simulated flaming fuel fires and a simulated electrical fault in the form of an overheated electrical cable. The data presented relates to experiments conducted within a simulated transit vehicle engine compartment and includes the impact of environmental parameters, such as cooling due to high airflow rates, on detection response times. The paper will conclude with the lessons learned from this testing, and provide insight into key aspects for successful detection of the different fire hazards in this demanding application.
Automakers and suppliers are relying on new testing equipment and facilities to evaluate the performance of today's class of electric and plug-in hybrid-electric vehicles. With American Recovery and Reinvestment Act of 2009 funds of $2.4 billion being invested into advanced battery and electric drive projects, the automotive industry has undergone a significant transformation over the past year and a half. And while hybrid and electric vehicle development has grown exponentially since those funds were allocated, public concern over the safety of electric vehicles (EVs), lithium-ion batteries, and EV charging stations has also increased. To help alleviate buyers' concerns-as well as their own-automakers and suppliers have invested heavily into new test equipment and facilities to learn as much about these new advanced energy systems as possible. With the added weight of battery systems in EVs and plug-in hybrid-electric vehicles (PHEVs), many companies are being forced to re-examine their test requirements, which are written for smaller, lighter components, as well as their test equipment, which is intended to handle much lower masses.
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