104,276 research outputs found
Powder metallurgy Rene 95 rotating turbine engine parts, volume 2
A Rene 95 alloy as-HIP high pressure turbine aft shaft in the CF6-50 engine and a HIP plus forged Rene 95 compressor disk in the CFM56 engine were tested. The CF6-50 engine test was conducted for 1000 C cycles and the CFM56 test for 2000 C cycles. Post test evaluation and analysis of the CF6-50 shaft and the CFM56 compressor disk included visual, fluorescent penetrant, and dimensional inspections. No defects or otherwise discrepant conditions were found. These parts were judged to have performed satisfactorily
The formation of planetary disks and winds: an ultraviolet view
Planetary systems are angular momentum reservoirs generated during star
formation. This accretion process produces very powerful engines able to drive
the optical jets and the molecular outflows. A fraction of the engine energy is
released into heating thus the temperature of the engine ranges from the 3000K
of the inner disk material to the 10MK in the areas where magnetic reconnection
occurs. There are important unsolved problems concerning the nature of the
engine, its evolution and the impact of the engine in the chemical evolution of
the inner disk. Of special relevance is the understanding of the shear layer
between the stellar photosphere and the disk; this layer controls a significant
fraction of the magnetic field building up and the subsequent dissipative
processes ougth to be studied in the UV.
This contribution focus on describing the connections between 1 Myr old suns
and the Sun and the requirements for new UV instrumentation to address their
evolution during this period. Two types of observations are shown to be needed:
monitoring programmes and high resolution imaging down to, at least,
milliarsecond scales.Comment: Accepted for publication in Astrophysics and Space Science 9 figure
Dynamics of line-driven disk winds in Active Galactic Nuclei
We present the results of time-dependent hydrodynamic calculations of line-
driven winds from accretion disks in AGN. To calculate the radiation force, we
take into account radiation from the disk and the central engine. The gas
temperature and ionization state in the wind are calculated self-consistently.
We find that a disk accreting onto a 10^8 MSUN black hole at the rate of 1.8
MSUN/YR can launch a wind at about 10^16 cm from the central engine. The X-rays
from the central object are attenuated by the disk atmosphere so they cannot
prevent the local disk radiation from pushing matter away from the disk. For a
reasonable X-ray opacity, the disk wind can be accelerated by the central UV
radiation to velocities of up to 15000 km/s at a distance of about 10^17 cm
from the central engine. The covering factor of the disk wind is .
The wind is unsteady and consists of an opaque, slow vertical flow near the
disk that is bounded on the polar side by a high-velocity stream. A typical
column density through the fast stream is a few 10^23 cm^-2. The fast stream
contributes nearly 100% to the total wind mass loss rate of 0.5 MSUN/YR.Comment: LaTeX, 20 pages, contains color figures, to appear in Ap
Disk formation in the collapse of supramassive neutron stars
Short gamma-ray bursts (sGRBs) show a large diversity in their properties.
This suggests that the observed phenomenon can be caused by different "central
engines" or that the engine produces a variety of outcomes depending on its
parameters, or possibly both. The most popular engine scenario, the merger of
two neutron stars, has received support from the recent Fermi and INTEGRAL
detection of a burst of gamma rays (GRB170817A) following the neutron star
merger GW170817, but at the moment it is not clear how peculiar this event
potentially was. Several sGRBs engine models involve the collapse of a
supramassive neutron star that produces a black hole plus an accretion disk. We
study this scenario for a variety of equations of states both via angular
momentum considerations based on equilibrium models and via fully dynamical
Numerical Relativity simulations. We obtain a broader range of disk forming
configurations than earlier studies but we agree with the latter that none of
these configurations is likely to produce a phenomenon that would be classified
as an sGRB.Comment: accepted by MNRA
Application of a flight-line disk crack detector to a small engine
A disk crack detector was developed and applied to a small military engine for use as a flight-line turbine crack monitor. The system consists of an eddy current type sensor and its cables within the engine, external connecting cables, and a remotely located electrical capacitance-conductance bridge and signal analyzer. As the turbine spins, the rotor is monitored by the sensor for radial surface cracks emanating from the interblade region of the rotor
Experimental Flow Investigation of a Truncated Ideal Contour Nozzle
Various tests showed a significant side load peak for low nozzle pressure ratios during engine start-up and shut down phase. DLR Lampoldshausen carried out tests to examine the flow field in a truncated ideal contour nozzle for low NPR. For NPR20 a slight concave shaped Mach disk was found. Its curvature is limited to the centre and its height trend correlates with measured side loads. A concave shaped Mach disk being responsible for re-attached flows at low NPR could be excluded. The experiments were accompanied by numerical simulations of the flow field on various pressure ratios with regards on the shock pattern. The predicted Mach disk shape compares well with the experiments
A Geometrical Relationship between Broad-Line Clouds and an Accretion Disk around Active Galactic Nuclei
Recent hard X-ray spectroscopy of active galactic nuclei has strongly
suggested that double-peaked, very broad Fe K emission arises from an accretion
disk around the central engine. Model fitting of the observed Fe K emission
line profile makes it possible to estimate a probable inclination angle of the
accretion disk. In order to study the geometrical relationship between the
accretion disk and broad emission-line regions (BLRs), we investigate the
correlation between the inclination angle of the accretion disk and the
velocity width of BLRs for 18 type-1 Seyfert galaxies. We found that there may
be a negative correlation between them, i.e., Seyfert nuclei with a more
face-on accretion disk tend to have larger BLR velocity widths, suggesting that
the BLRs are not coplanar with respect to the accretion disk. The most probable
interpretation may be that the BLRs arise from outer parts ({\it r} 0.01
pc) of a warped accretion disk illuminated by the central engine.Comment: 11 pages, 3 figures; accepted for Publications of the Astronomical
Society of Japa
Evaluation of Cyclic Behavior of Aircraft Turbine Disk Alloys
An evaluation of the cyclic behavior of three aircraft engine turbine disk materials was conducted to compare their relative crack initiation and crack propagation resistance. The disk alloys investigated were Inconel 718, hot isostatically pressed and forged powder metallurgy Rene '95, and as-hot-isostatically pressed Rene '95. The objective was to compare the hot isostatically pressed powder metallurgy alloy forms with conventionally processed superalloys as represented by Inconel 718. Cyclic behavior was evaluated at 650 C both under continuously cycling and a fifteen minute tensile hold time cycle to simulate engine conditions. Analysis of the test data were made to evaluate the strain range partitioning and energy exhaustion concepts for predicting hold time effects on low cycle fatigue
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