|Table of Contents|

Analysis of typical scheme and test technique development of TBCC engine(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2022年06期
Page:
26-34,68
Research Field:
目次
Publishing date:

Info

Title:
Analysis of typical scheme and test technique development of TBCC engine
Author(s):
LI Junjie;  HU Qiuchen;  LIU Pengchao;  XUE Yongguang;  GUAN Zhenyu
(Beijing Power Machinery Research Institute, Beijing 100074, China)
Keywords:
TBCC research progress test technique mode transition free steam
PACS:
V236
DOI:
-
Abstract:
Turbine based combined cycle engine expands the working envelope of traditional turbine engine and ramjet engine through the effective combination of turbine engine and ramjet engine, which is an important research and development direction in the field of aviation and aerospace.The maximum working Mach number is above 4.0.Based on the operational requirements of hypersonic aircraft in near space, this paper studied the typical cases and development trend of TBCC engine abroad in recent ten years, and analyzed the main progress of TBCC engine test technique.The results show that foreign countries have a good foundation of direct connection test and free steam test technology, and have completed the integrated ground machine and mode transition test, and technical maturity have reached TRL 4-5, and planned the flight test verification work.It is suggested that China should pay attention to the combination of theory and test technology, gradually improve the maturity of key technologies, and create social and economic benefits.

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