JPH01166735U - - Google Patents

Info

Publication number
JPH01166735U
JPH01166735U JP6161888U JP6161888U JPH01166735U JP H01166735 U JPH01166735 U JP H01166735U JP 6161888 U JP6161888 U JP 6161888U JP 6161888 U JP6161888 U JP 6161888U JP H01166735 U JPH01166735 U JP H01166735U
Authority
JP
Japan
Prior art keywords
compressor
combustor
detection means
turbine
means detects
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP6161888U
Other languages
Japanese (ja)
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed filed Critical
Priority to JP6161888U priority Critical patent/JPH01166735U/ja
Publication of JPH01166735U publication Critical patent/JPH01166735U/ja
Pending legal-status Critical Current

Links

Description

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本考案によるガスタービンエンジンを
示す構成図、第2図は空気流量計算と燃料量の計
算を行うフローチヤート、第3図はコンプレツサ
の出口圧力とタービンの入口温度に対する空気流
量の関係を示す図である。 10……ガスタービンエンジン、12……コン
プレツサ、14……コンプレツサタービン、16
……パワータービン、18……燃焼器、22……
バリアブルノズル、40……圧力センサ、42,
44……温度センサ。
Figure 1 is a configuration diagram showing the gas turbine engine according to the present invention, Figure 2 is a flowchart for calculating air flow rate and fuel amount, and Figure 3 is the relationship between air flow rate and compressor outlet pressure and turbine inlet temperature. FIG. 10... Gas turbine engine, 12... Compressor, 14... Compressor turbine, 16
...Power turbine, 18...Combustor, 22...
Variable nozzle, 40... Pressure sensor, 42,
44...Temperature sensor.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] コンプレツサと、燃焼器と、タービンとを有す
るガスタービンエンジンにおいて、コンプレツサ
の出口圧力を検出する圧力検出手段と、タービン
の入口温度を検出する温度検出手段と、該圧力検
出手段及び温度検出手段からの出力に基づいて燃
焼器を通る空気流量を求める手段とを備えたガス
タービンエンジンの空気流量検出装置。
In a gas turbine engine having a compressor, a combustor, and a turbine, pressure detection means detects the outlet pressure of the compressor, temperature detection means detects the turbine inlet temperature, and and means for determining the air flow rate through the combustor based on the output.
JP6161888U 1988-05-12 1988-05-12 Pending JPH01166735U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6161888U JPH01166735U (en) 1988-05-12 1988-05-12

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6161888U JPH01166735U (en) 1988-05-12 1988-05-12

Publications (1)

Publication Number Publication Date
JPH01166735U true JPH01166735U (en) 1989-11-22

Family

ID=31287276

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6161888U Pending JPH01166735U (en) 1988-05-12 1988-05-12

Country Status (1)

Country Link
JP (1) JPH01166735U (en)

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