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Modern Engineering Thermodynamics

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494 CHAPTER 13: Vapor and Gas Power Cycles<br />

The fuel-air mixture was ignited by an electric spark inside the cylinder. The spark was generated by a battery<br />

and an induction coil, which was basically the same technique used with all spark ignition engines through the<br />

middle of the 20th century.<br />

The Lenoir engine ran smoothly, but because the air-fuel mixture was not compressed before ignition, the<br />

engine had a very low actual thermal efficiency (less than 4%). 9 Consequently, Lenoir engines became popular<br />

only in small sizes (0.5 to 3 hp) because their fuel consumption was very high.<br />

The thermal efficiency of the Lenoir cycle is given by<br />

ðη T Þ Lenoir<br />

= ð _W out Þ net Q<br />

= _ H − j _Q L j<br />

_Q H<br />

_Q H<br />

= 1 − j _Q L j<br />

_Q H<br />

where, from Figure 13.42a, for a cold ASC with an isentropic expansion from 1 to 2s, we have<br />

j _Q L j = j 2s<br />

_Q 3 j = _m ðu 2s − u 3 Þ + _mpðv 2s − v 3 Þ<br />

= _m ðh 2s − h 3 Þ = _mc p ðT 2s − T 3 Þ<br />

and<br />

_Q H = 4<br />

_Q 1 = _mc v ðT 1 − T 4 Þ<br />

Because the intake air comes from an isothermal source (the atmosphere), T 3 = T 4 . However, the exhaust gas is<br />

confined to a fixed mass, so the condition p 2s = p 3 requires that T 2s /T 3 = v 2s /v 3 ,wherev 2s /v 3 is the isentropic<br />

compression ratio, CR. Then, the thermal efficiency becomes<br />

ðη T Þ Lenoir<br />

cold ASC<br />

<br />

ð Þ = 1 − kT T 2s /T 3 − 1<br />

3<br />

T 1 − T 4<br />

(13.21)<br />

v 2s /v 3 − 1<br />

= 1 − kT 3 = 1 − kT<br />

CR − 1<br />

3<br />

T 1 − T 4<br />

T 1 − T 4<br />

= 1 − c pðT 2s − T 3 Þ<br />

c v T 1 − T 4<br />

EXAMPLE 13.11<br />

The small model airplane jet engine shown in Figure 13.43 operates on the Lenoir cycle. It has a maximum temperature of<br />

T 1 = 800. R and an intake temperature of T 3 = T 4 = 530. R. The expansion, exhaust, and intake pressures are all p 2s = p 3 =<br />

p 4 = 14.7 psia, and the engine contains 1.00 × 10 –3 lbm of air. For this engine, determine<br />

a. The combustion pressure p 1 .<br />

b. The isentropic compression ratio CR = v 2s /v 3 .<br />

c. The Lenoir cold ASC thermal efficiency.<br />

FIGURE 13.43<br />

Example 13.11.<br />

9 These engines were often called atmospheric gas engines for the same reason.

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