Cost/benefit assessment of the application of composite materials to subsonic commercial transport engines

Results from a number of studies concerned with the cost and benefits of applying advanced composite materials to commercial turbofan engines are summarized. For each application area the optimistic and pessimistic benefit projections were averaged to arrive at a projected yearly percentage fuel savings for a commercial fleet of advanced technology transport aircraft. Engine components included in the summary are the fan section which includes fan blades, fan frame/case, and the blade containment ring; the nacelle; and the high pressure turbine blades and vanes. The projected fuel savings resulting from the application of composites are 1.85 percent for the fan section, 1.75 percent for the nacelle, and 2.35 percent for the high pressure turbine

Tungsten fiber-reinforced nickel superalloy

Tungsten fiber-reinforced nickel superalloy combines the strength of refractory metals with the oxidation resistance of superalloys. Knowledge of the relationship between fabrication technique, matrix compositions and fiber sizes minimized fiber-matrix reaction. Potential application includes high temperature turbine components

Performance of rocket nozzle materials with several solid propellants

Erosion resistance and thermal stress cracking tests of rocket nozzle materials with solid propellant

Interpreting Attention-Based Models for Natural Language Processing

Large pre-trained language models (PLMs) such as BERT and XLNet have revolutionized the field of natural language processing (NLP). The interesting thing is that they are pre- trained through unsupervised tasks, so there is a natural curiosity as to what linguistic knowledge these models have learned from only unlabeled data. Fortunately, these models’ architectures are based on self-attention mechanisms, which are naturally interpretable. As such, there is a growing body of work that uses attention to gain insight as to what linguistic knowledge is possessed by these models. Most attention-focused studies use BERT as their subject, and consequently the field is sometimes referred to as BERTology. However, despite surpassing BERT in a large number of NLP tasks, XLNet has yet to receive the same level of attention (pun intended). Additionally, there is an interest in their field in how these pre-trained models change when fine-tuned for supervised tasks. This paper details many different attention-based interpretability analyses and performs each on BERT, XLNet, and a version of XLNet fine-tuned for a Twitter hate-speech-spreader detection task. The purpose of doing so is 1. to be a comprehensive summary of the current state of BERTology 2. to be the first to do many of these in-depth analyse on XLNet and 3. to study how PLMs’ attention patterns change over fine-tuning. I find that most identified linguistic phenomenon present in the attention patterns of BERT are also present in those of XLNet to similar extents. Further, it is shown that much about the internal organization and function of PLMs, and how they change over fine-tuning, can be understood through attention

Reinforced metallic composites Patent

High strength reinforced metallic composites for applications over wide temperature rang

Preliminary Investigation of Guy Alloy as a Turbojet-engine Bucket Material for Use at 1650 Degrees F

As-cast buckets of Guy alloy, a cast nickel-base material, were run in a J33-9 turbojet engine for cycles of 15 minutes at rated speed and 5 minutes at idle speed. Stress rupture, impace and engine-performance data indicate that Guy alloy may be considered for bucket use at a temperature of 1650 degrees F. Ductility and impact strength of Guy alloy is limited but appears to be adequate for bucket applications

Performance of Two Boron-Modified S-816 Alloys in a Turbojet Engine Operated at 1650 F

S-816+B and modified S-816+B cast cobalt-base alloys were evaluated as turbine-bucket materials at 16500 F. Stress-rupture and tensile data obtained from these alloys had indicated satisfactory strength for engine operation at 1650 F. Although both alloys exhibited a limited ductility in room-temperature laboratory impact tests, there was a significant increase in impact resistance in the 1650 F tests. Bucket failures began after 10 hours of engine testing and continued at various intervals during the 107.5-hour test. Bucket lives were short relative to the predicted lives based on stress-rupture considerations (280 hr for S-816+B and 1750 hr for modified S-816+B). No significant difference was apparent in the performance of the two alloy groups. The primary cause of bucket failures in both alloys was mechanical fatigue. Impact damage occurred as a direct result of bucket tip fatigue failures and was a secondary cause of bucket failures. The impact of small pieces of fractured bucket tips on surrounding buckets caused a relatively large amount of impact damage to buckets of both alloys. The amount of impact damage from induced fractures at the bucket midspan, which provided relatively large failed fragments, was no greater than that which occurred as a result of tip failures