The adiabatic flame temperature in combustion of hydrocarbon fuels in refinery heaters comes down with an increase in excess air. One must consider that the xs air acts as an additional heat sink. See, for example, the adiabatic temperatures for a refinery fuel with a lower calorific value of 9,750 kcal/kg, with varying xs air %:
xs air,% adiab. temp., oC
0 2,000
20 1,800
40 1,640
60 1,480
80 1,360
100 1,250
In practice, these temperatures aren't attainable because of the immediate flame heat release "in status nascendi" by radiation.
If we assume that this "loss" is, say 35%, the above temperatures would come down to something as 1,450, 1,265, 1,140, 1,010, 920, and 850oC, respectively.
Higher flame heat "losses", of around 50%, can be attained in refinery furnaces by preheating the air to combustion and having a low % of xs air which, as we saw, affects the flame temperature, and thus the flame radiation heat flux.