FIG. 2 shows a schematic left side view of the right turbojet of FIG. 1, and FIG. 3 shows a schematic front view of the two turbojets of FIG. 1, with the fan cowls open. FIG. 1 shows two turbojets10installed on the aft section of the fuselage1of an aircraft, in upper position...
FIG. 2 is a schematic illustration of another embodiment of an engine system according to the present invention. While the above-identified drawing figures set forth embodiments of the invention, other embodiments are also contemplated, as noted in the discussion. In all cases, this disclosure pres...
10 is a schematic representation of a nacelle according to the invention, the opening is mechanically assisted. Une nacelle 1 selon l'invention telle que représentée sur les figures A nacelle 1 according to the invention as shown in Figures 1à 7 est destinée àêtre rattachée sous une ...
Above these is an instrumentation and control panel with schematic diagram. The clearly labelled front panel with mimic diagram includes the instrument displays, controls and warning lights. Air passes into an air box, into a compressor, then into the combustion chamber. A pump transfers fuel from...
Schematic diagramsNO ABSTRACT DUE TO ILLEGIBILITY OF REPORT (KAR).Pinkel, BNational Aeronautics and Space AdministrationKarp, I. MPinkel, B. and Karp, 1. M. A thermodynamic study of the turbojet engine. NACA Report No. 891, 1947Pinkel, Benjamin and Irving M. Karp: A Thermodynamic Study...
[0031] Figure 3 shows, the present invention is speed signal processing circuit schematic. 该转速信号处理电路3由差分放大电路4和滞回比较电路5构成,其中的差分放大电路4由第一运算放大器10、第二运算放大器11、第一电阻13、第二电阻14、第三电阻15、第四电阻16以及第八电阻20构成,滞回比较电路5由第三运算...
The schematic of Min–Max selection strategy in the controller structure is shown in Figure 2. Figure 2. Schematic of engine fuel controller with min–max selection strategy. After formation of the Min–Max control algorithm, many studies have done for performance improvement of this strategy....
FIG. 1 is a partial, perspective schematic view of a turbofan engine incorporating the thrust reverser according to the invention. FIG. 2 is a partial, longitudinal sectional schematic diagram showing the thrust reversing door according to the invention in the forward thrust position. ...
Other features, aims and advantages of the present invention will appear more clearly upon reading the detailed description that follows, and with reference to the appended drawings given by way of non-limiting example and in which FIGS. 1ato 3lare schematic section views of different embodiments ...
The single FIGURE is a schematic, cross-section of a small gas turbine contemplated by the present invention. DESCRIPTION OF THE PREFERRED EMBODIMENT The single figure depicts a gas turbine engine in the form of a counterflow, single rotor turbojet generally denoted by the reference numeral 10....