Development and Testing of an Ignition Physics Test Facility and an Oxygen/methane Swirl Torch Igniter

Development and Testing of an Ignition Physics Test Facility and an Oxygen/methane Swirl Torch Igniter PDF Author: Jesús Roberto Flores
Publisher:
ISBN:
Category : Internal combustion engines
Languages : en
Pages :

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Design, Fabrication, and Test of a Lox/Lch4 Rcs Igniter at Nasa

Design, Fabrication, and Test of a Lox/Lch4 Rcs Igniter at Nasa PDF Author: Nasa Technical Reports Server (Ntrs)
Publisher: BiblioGov
ISBN: 9781289235215
Category :
Languages : en
Pages : 22

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A workhorse liquid oxygen-liquid methane (LOX/LCH4) rocket igniter was recently tested at NASA Glenn Research Center s (GRC) Research Combustion Laboratory (RCL). These tests were conducted in support of the Reaction Control Engine (RCE) development task of the Propulsion and Cryogenics Advanced Development (PCAD) project. The igniter was a GRC in-house design used to evaluate the ignition processes for LOX/LCH4. The test matrix was developed to examine the flammability of LOX/LCH4 over a range of oxidizer-to-fuel mixture ratios, both in the core fuel flow and total flow. In addition, testing also examined the durability of the hardware by accumulating ignition pulses. Over the course of testing, a total of 1402 individual ignition pulses were successfully demonstrated over the range of mixture ratios. Testing was halted after the failure of the ceramic in the igniter spark plug.

Design and Testing of an OX/CH4 Swirl Torch Ignition System

Design and Testing of an OX/CH4 Swirl Torch Ignition System PDF Author: Gabriel Ricardo Trujillo
Publisher:
ISBN:
Category : Liquid methane
Languages : en
Pages : 85

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Experimentelle und numerische Untersuchung der Flammenentwicklung bei Laserentzündung von Methan/Sauerstoff-Gemischen in Modellbrennkammern

Experimentelle und numerische Untersuchung der Flammenentwicklung bei Laserentzündung von Methan/Sauerstoff-Gemischen in Modellbrennkammern PDF Author: Michael Wohlhüter
Publisher:
ISBN:
Category :
Languages : de
Pages :

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Development and Use of Hydrogen-air Torches in an Altitude Facility

Development and Use of Hydrogen-air Torches in an Altitude Facility PDF Author: Roy A. Lottig
Publisher:
ISBN:
Category :
Languages : en
Pages : 18

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Preparing for Ignition Experiments on the National Ignition Facility

Preparing for Ignition Experiments on the National Ignition Facility PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 12

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The National Ignition Facility (NIF) is a 192-beam Nd-glass laser facility presently under construction at Lawrence Livermore National Laboratory (LLNL) for performing ignition experiments for inertial confinement fusion (ICF) and experiments studying high energy density (HED) science. NIF will produce 1.8 MJ, 500 TW of ultraviolet light ([lambda] = 351 nm) making it the world's largest and most powerful laser system. NIF will be the world's preeminent facility for the study of matter at extreme temperatures and densities for producing and developing ICF. The ignition studies will be an essential step in developing inertial fusion energy (IFE). the NIF Project is over 93% complete and scheduled for completion in 2009. Experiments using one beam have demonstrated that NIF can meet all of its performance goals. A detailed plan called the National Ignition Campaign (NIC) has been developed to begin ignition experiments in 2010. The plan includes the target physics and the equipment such as diagnostics, cryogenic target manipulator and user optics required for the ignition experiment. Target designs have been developed that calculate to ignite at energy as low as 1 MJ. Plans are under way to make NIF a national user facility for experiments on HED physics and nuclear science, including experiments relevant to the development of IFE.

Relevance of the U.S. National Ignition Facility for Driver and Target Options to Next-step Inertial Fusion Test Facilities

Relevance of the U.S. National Ignition Facility for Driver and Target Options to Next-step Inertial Fusion Test Facilities PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 9

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Achievement of inertial fusion ignition and energy gain in the proposed U.S. National Ignition Facility is a prerequisite for decisions to build next-step U.S. inertial fusion facilities for either high yield or high pulse-rate. There are a variety of target and driver options for such next-step inertial fusion test facilities, and this paper discusses possible ways that the NIF, using a 1.8 MJ glass laser in both direct and indirect-drive configurations, can provide target physics data relevant to several next-step facility options. Next step facility options include the Engineering Test Facility (ETF), which needs several-Hz pulse-rates for testing relevant to Inertial Fusion Energy (IFE) development. An option for high yield, called the Laboratory Microfusion Facility (LMF), does not require such high pulse-rates, but may still benefit from driver technologies capable of much higher shot rates than possible with glass lasers. A high-pulse-rate driver could also be used for a combined ETF/LMF facility, driving multiple target chambers with a common driver. Driver technologies that could support high-pulse rates for next-step options include heavy-ion and light-ion accelerators, diode-pumped solid-state lasers (DPSSL), and krypton-flouride gas lasers. The NIF could be used to provide important data for IFE in generic areas of target chamber damage and materials responses, neutron activation and heating, tritium recovery and safety, and in performance tests of prototypical IFE targets and injection systems. In the study of ignition in both direct and indirect-drive, the NIF would explore generic ICF fuel capsule implosion physics common to all driver and target options for next-step facilities. In the following, we point out specific ways in which the NIF could be used to study target physics specifically relevant to the above-mentioned driver options for such next-step facilities, as well as how the NIF laser system itself could be relevant to the DPSSL option.

Experimental Investigation Into Combustion Torch Jet Ignition of Methane-air, Ethylene-air, and Propane-air Mixtures

Experimental Investigation Into Combustion Torch Jet Ignition of Methane-air, Ethylene-air, and Propane-air Mixtures PDF Author: Ukwatte Lokuliyanage Indika Upendra Perera
Publisher:
ISBN:
Category : Combustion
Languages : en
Pages : 260

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Ignitability and the ignition delay time of a combustible mixture in a long combustion chamber, ignited by a hot combustion torch jet generated in a pre-chamber was investigated experimentally in relation to application as a viable igniter method for wave rotor combustors. Methane-air, ethylene-air, and propane-air in varying equivalence ratios were investigated as the combustible mixture in the combustion chamber. The effects of variation in the torch jet fuel, initial equivalence ratio in the pre-chamber, and nozzle geometry on the ignitability and the ignition delay time of combustible mixtures were observed and analyzed. The single-channel wave-rotor combustion rig at Combustion and Propulsion Research Laboratory at the Purdue School of Engineering and Technology at Indiana University-Purdue University, Indianapolis was used for this study. High-speed video imaging techniques to observe the ignition and flame propagation in the combustion chamber and fast-response pressure transducers to measure the dynamic pressure fluctuations in the combustion chambers were used in the current study. The present work explains how the experimental procedure and preliminary testing was carried out in order to conduct the necessary testing to find the ignitability and ignition delay time of a combustible mixture. Ignitability of methane, ethylene, and propane were much broader in range compared to conventional spark ignitable lean and rich limit equivalence ratios. The methane and propane ignition lean limits were similar to radical activated ignition lean limits found in previous studies of the same fuels. Ethylene exhibited the widest range in equivalence ratios from 0.4 to 2.4, while methane had the narrowest ranging from equivalence ratio 0.4 to 1.4. The ignition delay studies indicated both chemical kinetics and mixing between the combustion torch jet and the combustible mixture were critical. The mixing phenomena dominated chemical kinetics; unlike in ignition delay studies conducted using shock heated ignition techniques. Ethylene-air mixtures had the shortest ignition delay times ~1 ms for lean but near-stoichiometric mixtures. Methane and propane indicated similar ignition delay time characteristics with lean near-stoichiometric mixtures. The fuel-air equivalence ratio which was used to generate the combustion torch jet and the torch jet nozzle geometry had a direct influence over the ignition delay time in the main chamber combustible mixture. The slightly rich fuel-air ratios used to generate the combustion torch jet had the lowest delay times in igniting the main chamber fuel-air mixtures.

Test System to Study the Ignition of Metals by Polymers in Oxygen

Test System to Study the Ignition of Metals by Polymers in Oxygen PDF Author: J. Stoltzfus
Publisher:
ISBN:
Category : Fire hazards
Languages : en
Pages : 13

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A new test system that uses laser energy to ignite a polymer promoter has been developed at the NASA White Sands Test Facility (WSTF). It will facilitate the study of kindling chain ignition, such as the spread of fire from a burning polymer material to surrounding metal. The test system can be used to answer questions regarding configurational effects on ignition and combustion.

אמרי בנימן

אמרי בנימן PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages :

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