34 research outputs found

    Case Histories Of Specialized Turbomachinery Problems

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    PaperPg. 33-50.Vibration problems in turbomachinery occur due to many factors. Some of the problems could have been prevented if more detailed design analyses were performed. Other times the problems occur due to design extrapolations which are pushing the state of the art. The case histories of excessive vibrations and failures that will be discussed in this presentation are examples of those where additional design analyses would not necessarily have predicted or anticipated the problem that occurred because the analytical models are not sufficient to take into account all the variables

    Refrigerants Containing Fluoroiodocarbons (FICs)

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    Energy Efficient, Environmentally Friendly Refrigerants

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    This paper describes a new family of safe, environmentally friendly, high performance substitute refrigerants for application in manufacturing and facilities operations. Due to the Montreal Protocol and subsequent environmental regulations, CFC refrigerants have become expensive or unavailable. A safe, environmentally friendly, high performance refrigerant mixture for replacement of R-12 and R-134a has been developed. The mixture, designated Ikon B, is nonflammable, has zero ozone depletion potential, low global warming potential, relatively low toxicity, is compatible with most common refrigeration system materials of construction, and is thermally stable. Ikon B was used as a drop-in replacement for R-12 in an instrumented 1.5 ton chiller. Operating pressures for Ikon B were essentially the same as for R-12. Analysis of test runs showed that Ikon B gave approximately 2% higher energy efficiency than R-12 with 16% greater capacity, and 17% higher energy efficiency than R-134a with 2% greater capacity

    Applications Tests of Energy Efficient, Environmentally Friendly Refrigerants

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    This paper describes performance demonstrations of two members of the Ikon® family of safe, environmentally friendly, high performance substitute refrigerants for replacement of R-12 and R-134a in manufacturing and facilities operations. Preliminary development efforts for Ikon® C, an energy efficient R-22 replacement, will also be described. The Ikon® refrigerants are nonflammable, non-ozone-depleting, have low global warming, relatively low toxicity, are thermally stable, and are compatible with most common refrigeration system materials of construction. This paper presents (1) results of performance demonstration of Ikon® B in an instrumented spare of the Space Shuttle Cabin cooling system at NASA KSC; (2) results from performance demonstration of Ikon® A and Ikon® B in a domestic refrigerator; and (3) a brief update on the development status of lkon® C including predicted capacities and energy efficiencies of candidates. Results confirm the 10-20% increased energy efficiency of the refrigerants, due to greater volumetric capacity

    Applications Tests of Energy Efficient, Environmentally Friendly Refrigerants

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    This paper describes performance demonstrations of two members of the Ikon® family of safe, environmentally friendly, high performance substitute refrigerants for replacement of R-12 and R-134a in manufacturing and facilities operations. Preliminary development efforts for Ikon® C, an energy efficient R-22 replacement, will also be described. The Ikon® refrigerants are nonflammable, non-ozone-depleting, have low global warming, relatively low toxicity, are thermally stable, and are compatible with most common refrigeration system materials of construction. This paper presents (1) results of performance demonstration of Ikon® B in an instrumented spare of the Space Shuttle Cabin cooling system at NASA KSC; (2) results from performance demonstration of Ikon® A and Ikon® B in a domestic refrigerator; and (3) a brief update on the development status of lkon® C including predicted capacities and energy efficiencies of candidates. Results confirm the 10-20% increased energy efficiency of the refrigerants, due to greater volumetric capacity

    Nonflammable, Nonaqueous, Low Atmospheric Impact, High Performance Cleaning Solvents

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    For many years, chlorofluorocarbon (CFC) and chlorocarbon solvents have played an important part in aerospace operations. These solvents found extensive use as cleaning and analysis (EPA) solvents in precision and critical cleaning. However, CFCs and chlorocarbon solvents have deleterious effects on the ozone layer, are relatively strong greenhouse gases, and some are suspect or known carcinogens. Because of their ozone-depletion potential (ODP), the Montreal Protocol and its amendments, as well as other environmental regulations, have resulted in the phaseout of CFC-113 and 1,1,1-trichloroethane (TCA). Although alternatives have been recommended, they do not perform as well as the original solvents. In addition, some analyses, such as the infrared analysis of extracted hydrocarbons, cannot be performed with the substitute solvents that contain C-H bonds. CFC-113 solvent has been used for many critical aerospace applications. CFC-113, also known as Freon (registered) TF, has been used extensively in NASA's cleaning facilities for precision and critical cleaning, in particular the final rinsing in Class 100 areas, with gas chromatography analysis of rinse residue. While some cleaning can be accomplished by other processes, there are certain critical applications where CFC-113 or a similar solvent is highly cost-effective and ensures safety. Oxygen system components are one example where a solvent compatible with oxygen and capable of removing fluorocarbon grease is needed. Electronic components and precision mechanical components can also be damaged by aggressive cleaning solvents

    Highly Effective, Low Toxicity, Low Environmental Impact Total Flooding Fire Suppressants

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    Halon 1301 (CF3Br) has been used for decades as the primary fire suppression agent for areas where powder agents cannot be used because of concerns for sensitive equipment. Halon 1301 is an excellent extinguishing agent, effective at about 3% in air and quite non-toxic. It has an effective exposure limit much greater than its extinguishing concentration, so it can be used in normally occupied areas. The ability of a chemical to destroy stratospheric ozone is its ozone-depletion potential (ODP). ODP is the amount of ozone destroyed per pound of a chemical, relative to the standard CFC-11 with an ODP = 1.0. Because halons have been implicated in stratospheric ozone depletion, their production was stopped at the end of 1995 under the provisions of the Montreal Protocol plus later amendments. In the US, the Clean Air Act Amendments of 1990, Presidential directives, and DoD Directive 6050.9 implemented this phaseout. These regulations and penalties have provided strong incentives for US businesses to decrease CFC use. The Omnibus Budget Reconciliation Act of 1989 mandates high Federal taxes on CFCs and halons, designed to price them out of the market. The taxes also capture for the government the windfall profits that would otherwise go to producers as scarcity drives up prices. Several replacements have been developed for Halon 1301. One is carbon dioxide, which has been used as a firefighting agent for many years. However, a high concentration of carbon dioxide is necessary to inert fuels. The effective concentration for inerting with carbon dioxide is approximately 29%, which is above the concentration lethal to humans. HFC-227ea is being used extensively to replace Halon 1301 systems in nominally occupied areas and some normally unoccupied areas. However, since the effective concentration of HFC-227ea is about three to four times that of Halon 1301 the extinguishing systems have to be larger and new extinguishing systems have to be installed. HFC-125 is also being sold as an extinguishing agent (Nimitz). It has problems similar to HFC-227ea, with a greater concentration needed for effectiveness and the need to use a larger system. This is a particularly onerous penalty in aircraft and spacecraft, where weight and space are extremely important, and substitution is often impossible in existing aircraft due to space limitations
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