本SAE航空航天标准（AS）为飞机推进系统及其衍生产品提供了经典的推进系统性能参数名称，并描述了构建新名称的逻辑框架。本文件的内容最初是AS755E的一个子集。由于AS755中描述的站点编号方案越来越复杂，并且希望扩展原始文档的命名部分，以包括更完整的“经典”（遗留使用）名称表示，因此决定将其“站点编号”和“命名”内容分为两个单独的文档。因此，本文档是使用AS755E的“命名法”创建的。根据行业需求，这两份文件将继续改进和修订。本文提出的参数命名约定适用于与推进系统性能有关的所有通信，如计算机程序、数据简化、设计活动和发布的文件。 它们旨在促进程序用户的计算，而不会过度限制程序供应商使用的计算方法。本文提供的符号列表将用于识别输入和输出参数。这些符号不需要用作引擎子程序内的内部参数名称。

This SAE Aerospace Standard (AS) provides classical propulsion system performance parameter names for aircraft propulsion systems and their derivatives, and describes the logical framework by which new names can be constructed. The contents of this document were, originally, a subset of AS755E. Due to the growing complexity of station numbering schemes described in AS755, and a desire to expand the original document’s nomenclature section to include a fuller representation of “classical” (legacy use) names, a decision was made to separate its “station numbering” and “nomenclature” content into two separate documents. This document, then, was created using the “nomenclature” half of AS755E. Both documents will continue to be improved and revised as industry needs dictate. The parameter naming conventions presented herein are for use in all communications concerning propulsion system performance such as computer programs, data reduction, design activities, and published documents. They are intended to facilitate calculations by the program user without unduly restricting the method of calculation used by the program supplier. The list of symbols presented herein will be used for identification of input and output parameters. These symbols are not required to be used as internal parameter names within the engine subprogram.