454 research outputs found

    Custom software for the 3D printing of patient specific plate bending templates in pelvic fracture repair.

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    The purpose of this work is to reduce the operative time and blood loss incurred during open reduction and internal fixation (ORIF) of traumatic pelvic injuries through the creation of patient specific bending templates for reconstruction plates. These templates are 3D printed in a resin capable of being sterilized and taken into the operating room so that bending may be performed by the surgeon before the patient is opened or by another team member in parallel with the surgeon. A novel software extension was created in 3D modeling software to allow a surgeon to individually position screws on a pelvic model to create a virtual plate. The software constrains the locations of placed screws so that the virtual plate is dimensionally identical to common reconstruction plates. The user is then able to export a bending template that includes the section of the pelvis the virtual plate was located on as well as screw location landmarks. The user can then flash sterilize the template and use it intraoperatively to obtain a plate that is accurately bent to the patient’s anatomy and the surgeon’s specifications. We produced a bending template representative of the most complex plating location on the pelvis, the posterior wall. A surgeon then accurately bent reconstruction plate to match the bending template, proving that the software produced a dimensionally accurate output. Other work has shown that the pre-bending of plates can shorten operative time, reduce blood loss, and allow for less invasive procedures. However, methods currently available for pre-bending patient specific plates involve the lengthy process of printing the patient’s pelvis and then a lengthy sterilization process of the implant itself. Our method allows the template to be printed and processed in as little as 3 hours and sterilized by autoclave in less than 10 minutes. Further work needs to be done to evaluate how the process works when used in a patient case, to statistically prove that our method reduces operative time and blood loss, and show that plates bent using our method are similar between all members of the surgical team

    A Review of National Ozone and Particulate Matter Air Quality Standards in Light of Long-Standing California Air Quality Standards

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    Identification and Field Evaluation of Grape Shoot Volatiles Attractive to Female Grape Berry Moth ( Paralobesia viteana )

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    Solid-phase microextraction (SPME) and gas chromatography coupled with electroantennographic detection (GC-EAD) were used to identify volatile compounds from shoots of riverbank grape (Vitis riparia) that attract the female grape berry moth (GBM, Paralobesia viteana). Consistent EAD activity was obtained for 11 chemicals: (Z)-3-hexen-1-yl acetate, (E)-linalool oxide, (Z)-linalool oxide, nonanal, linalool, (E)-4,8-dimethyl-1,3,7-nonatriene, methyl salicylate, decanal, β-caryophyllene, germacrene-D, and α-farnesene. In flight-tunnel tests that involved female GBM and rubber septa loaded with subsets of these 11 compounds, we found that both the 11-component blend and a seven-component blend, composed of (E)-linalool oxide, (Z)-linalool oxide, nonanal, (E)-4,8-dimethyl-1,3,7-nonatriene, decanal, β-caryophyllene and germacrene-D, elicited equivalent levels of upwind flight as freshly cut grape shoots. The removal of any of the seven compounds from the seven-component blend resulted in a significant decrease in female upwind flight responses. In a field trial with these two synthetic blends, traps equipped with either blend captured more female GBM compared to traps baited with hexane only (control), although the number of females caught was generally low. There were no differences in the number of males captured among treatments. Although in flight-tunnel trials, moths readily flew upwind to both grape shoots and rubber septa loaded with the best lures, they landed on shoots but not on rubber septa. Coupled with relatively low field catches, this suggests that additional host finding cues need to be identified to improve trap efficac

    Prospectus, October 23, 1996

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    https://spark.parkland.edu/prospectus_1996/1026/thumbnail.jp

    Prospectus, September 11, 1996

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    https://spark.parkland.edu/prospectus_1996/1020/thumbnail.jp

    A classroom management technique: Preparing the classroom as an effective learning environment -- one means of preventive disciplines

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    A smooth-running classroom, free from disruption and chronic misbehavior but full of students involved in learning activities, does not just happen. Such classrooms exist because the teachers work at making it happen. These teachers give careful consideration to preparation of the classroom before the first day of the school year. Classroom management is one area the Educational Testing Service is working on to place in the teacher competency examinations they are preparing (Weber, et al., 1983). Because of this emphasis, classroom management may soon be a required class for graduation in the field of education

    Prospectus, November 13, 1996

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    https://spark.parkland.edu/prospectus_1996/1029/thumbnail.jp

    Technical and Regulatory Factors of Adopting Electric Training Aircraft in a Collegiate Aviation Setting

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    Electric-powered aircraft have entered the market. The arrival of the Pipistrel Velis Electro and other developmental efforts by companies such as Bye Aerospace, Piper, and eViation, have signaled to the aviation community that more electric-powered aircraft can be expected in the coming years. But how useful are they for training pilots in a Federal Aviation Administration (FAA) approved Part 141 collegiate aviation environment? To identify candidate flight courses and lessons, the authors examine flight hour distributions of a one-year window of invoiced flights (N = 52,728), including flight hour data cut-points at 60 minutes (n = 6,050) and 90 minutes (n = 25,439). The data distribution suggests that approximately 11.5% of the candidate flights would fall within a 60-minute expected flight duration, whereas 48% of flights would fall within a 90-minute flight duration. These calculations provide realistic targets for designed minimum flight duration (plus the inclusion of required FAA reserve) in order to be determined a feasible trainer in many high-volume FAA Part 141 training environments. Detailed course-level analysis suggests the Instrument Flight Instructor (CFII) flight course as a potential launch point for electric flight due to the relatively lower flight hour per lesson. In addition to minimum flight duration, other feasibility questions are included in this analysis, such as regulatory requirements, battery duration, aircraft turnaround time, multiple charge-discharge cycles per day, environmental factors, airport charging infrastructure, and maintenance factors. Additional research will benefit this developing area of electric aircraft in flight training environments
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