Method and system for authenticating safety of alternative fuel in aircraft engine
An engine system and aero-engine technology, applied in the fields of aviation safety, airworthiness technology, and alternative energy, which can solve the problems of high fuel refining cost, high fuel testing cost, and inability to verify the safety of alternative fuels.
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no. 1 example
[0051] figure 1 is a schematic flow chart of a method for authenticating the safety of alternative fuels in aero-engines according to the first embodiment of the present invention, figure 2 It is a detailed block diagram of each step in the method for verifying the safety of alternative fuels in aero-engines according to the first embodiment of the present invention.
[0052] Such as figure 1 As shown, the authentication method includes the following steps.
[0053] Step S110, based on the historical experience data of aviation fuel and the structural characteristics of the aeroengine, obtain the key safety parameters related to the safety of the engine system, and obtain the key safety parameter space of the engine system based on the key safety parameters (such as figure 2 indicated by the number 10 in).
[0054] In the present embodiment, the aviation fuel is preferably aviation kerosene. However, it is easy to understand that it is not limited to aviation kerosene. Th...
example 1
[0081] The following is the certification process for the safety of Fischer-Tropsch aviation fuel in aero-engines, for reference below figure 2 The security authentication process will be described.
[0082] 1. Establish the basic physical and chemical properties and compositional space database of aviation kerosene, and establish the basic physical and chemical properties and compositional space database of aviation kerosene through collection, statistics, and discrete analysis of a large number of basic physical and chemical properties and compositional space of aviation kerosene.
[0083] 2. Bring the basic physical and chemical test data space of aviation kerosene into the standard combustion chamber model, and bring the output combustion chamber performance parameters into the integrated model to obtain the safe operating range of the engine key safety parameter group. Taking the safety boundary and margin of the key safety parameter group as the target, and taking the b...
example 2
[0087] The following is the certification process for the safety of hydrogenated renewable aviation kerosene in aeroengines, refer to the following figure 2 The side explains the security authentication process:
[0088] 1. Establish the basic physical and chemical properties and composition spatial database of aviation kerosene. Through the collection, statistics, and discrete analysis of a large number of basic physical and chemical properties and composition space of aviation kerosene, a database of basic physical and chemical properties and composition space of aviation kerosene is established.
[0089] 2. Bring the basic physical and chemical test data space of aviation kerosene into the standard combustion chamber model, and bring the output combustion chamber performance parameters into the integrated model to obtain the safe operating range of the engine key safety parameter group. Taking the safety boundary and margin of the key safety parameter group as the target,...
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