| Integrated Engine Instrument System. Appendix IV. |
AUG 1971 |
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| Authors:
R. L. Skovholt; R. E. Glusick; GENERAL ELECTRIC CO WILMINGTON MA AEROSPACE INSTRUMENTS AND ELECTRICAL SYSTEM S DEPT
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 | The activity performed during this period of time was dedicated to the final design, fabrication, and debugging of the hardware. The lab model type of hardware includes a specially designed and programmable display generator and an off-the-shelf CRT terminal. (Author) |
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| Integrated Engine Instrument System. Appendix II. |
AUG 1971 |
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| Authors:
R. L. Skovholt; G. J. Carlson; J. F. Moran; G. J. Nolan; GENERAL ELECTRIC CO WILMINGTON MA AEROSPACE INSTRUMENTS AND ELECTRICAL SYSTEM S DEPT
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 | This Appendix covers the work performed in the area of sensor investigation. The sensor investigation includes a discussion of the parametric requirements, a description of technical approaches and sensor candidates, and appropriate discussions of tradeoffs, analyses and conclusions. As an outcome of the sensor investigation in which a number of improved sensing capabilities for an IEIS were recognized, work statements were written outlining recommended sensor development activities for consideration in ... |
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| Integrated Engine Instrument System. Appendix I. |
AUG 1971 |
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| Authors:
R. L. Skovholt; D. P. Allen; M. E. Douglass; K. B. Kochanski; H. L. McManus; GENERAL ELECTRIC CO WILMINGTON MA AEROSPACE INSTRUMENTS AND ELECTRICAL SYSTEM S DEPT
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 | This Appendix covers the work performed regarding the areas of parameter selection for engine condition and status monitoring, parameter simulation, energy management system study, and thrust/power measurement investigation. In addition, a preliminary discussion is also presented on an overall IEI System investigation. (Author) |
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| Integrated Engine Instrument System. |
AUG 1971 |
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| Authors:
R. L. Skovholt; D. P. Allen; W. A. Doerle; M. E. Douglass; G. J. Carlson; GENERAL ELECTRIC CO WILMINGTON MA AEROSPACE INSTRUMENTS AND ELECTRICAL SYSTEM S DEPT
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 | The Integrated Engine Instrument System is an adaptive computer driven display system. This concept replaces conventional cockpit instrumentation systems that employ a myriad of individual instruments, with an intregated display enhancing flight crew capability. Numerous technologies are involved in IEIS. The report documents the work conducted on this program. (Author) |
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| Integrated Engine Instrument System. Appendix III. |
AUG 1971 |
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| Authors:
R. L. Skovholt; W. A. Doerle; R. E. Glusick; F. P. Johnson; G. J. Nolan; GENERAL ELECTRIC CO WILMINGTON MA AEROSPACE INSTRUMENTS AND ELECTRICAL SYSTEM S DEPT
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 | The contents of this Appendix primarily deal with the display aspects of the IEIS Program. This activity has included a number of tasks which are required to determine the most appropriate means of communicating status and condition information to the flight crew. (Author) |
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