An aircraft engine compartment simulation device for fire extinguishing agent concentration measurement experiments
A concentration measurement and simulation device technology, applied in the direction of aircraft component testing, etc., can solve the problems of infeasibility, complex internal structure, high cost, etc., and achieve the effects of convenient scientific research and testing, small size and simple structure
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[0025] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
[0026] figure 1 It is a structural schematic diagram of the present invention, figure 2 , image 3 are the top view and front view of the middle measurement section, respectively, such as Figure 1-3 As shown, the present invention is an aircraft nacelle simulation device used for fire extinguishing agent concentration measurement experiments, including a fire extinguishing agent release section, an intermediate measurement section, a wind generation sectio...
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