Part 1 gives a general discussion of the uses, principles, construction, and operation of airplane tachometers. Detailed description of all available instruments, both foreign and domestic, are given. Part 2 describes methods of tests and effect of various conditions encountered in airplane flight such as change of temperature, vibration, tilting, and reduced air pressure. Part 3 describes the principal types of distance reading thermometers for aircraft engines, including an explanation of the physical principles involved in the functioning of the instruments and proper filling of the bulbs. Performance requirements and testing methods are given and a discussion of the source of error and results of tests. Part 4 gives methods of tests and calibration, also requirements of gauges of this type for the pressure measurement of the air pressure in gasoline tanks and the engine oil pressure on airplanes. Part 5 describes two types of gasoline gauges, the float type and the pressure type. Methods of testing and calibrating gasoline depth gauges are given. The Schroeder, R. A. E., and the Mark II flowmeters are described.


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    Titel :

    Aeronautic Instruments. Section V : Power Plant Instruments


    Beteiligte:
    Washburn, G E (Autor:in) / Sylvander, R C (Autor:in) / Mueller, E F (Autor:in) / Wilhelm, R M (Autor:in) / Eaton, H N (Autor:in) / Warner, John A C (Autor:in)

    Erscheinungsdatum :

    01.01.1923


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



    Aeronautic instruments. Section V : power plant instruments

    Washburn, G.E. | Engineering Index Backfile


    Aeronautic Instruments. Section IV : Direction Instruments

    Franklin, W S / Stillman, M H / Sanford, R L et al. | NTRS | 1923



    Aeronautic instruments. Section III : aircraft speed instruments

    Hunt, Franklin L. | Engineering Index Backfile | 1923


    Aeronautic Instruments. Section III : Aircraft Speed Instruments

    Hunt, Franklin L / Stearns, H O | NTRS | 1923