JPS59188956U - jet engine - Google Patents

jet engine

Info

Publication number
JPS59188956U
JPS59188956U JP8289983U JP8289983U JPS59188956U JP S59188956 U JPS59188956 U JP S59188956U JP 8289983 U JP8289983 U JP 8289983U JP 8289983 U JP8289983 U JP 8289983U JP S59188956 U JPS59188956 U JP S59188956U
Authority
JP
Japan
Prior art keywords
jet engine
figures
radial turbofan
turbofan
radial
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
JP8289983U
Other languages
Japanese (ja)
Inventor
秀一 川崎
Original Assignee
三菱重工業株式会社
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 by 三菱重工業株式会社 filed Critical 三菱重工業株式会社
Priority to JP8289983U priority Critical patent/JPS59188956U/en
Publication of JPS59188956U publication Critical patent/JPS59188956U/en
Pending legal-status Critical Current

Links

Landscapes

  • Control Of Turbines (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

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

第１図、第２図及び第３図は従来の３つの異なるジェッ
トエンジンを示す図、第４ａ図は本考案によるジェット
エンジンの一例を示す図、第４ｂ図は第４ａ図の４ｂ−
４ｂ線矢視図、第５ａ図及び第５ｂ図は本考案ジェット
エンジンによって下方推力を得ている状態を示す、第４
ａ図及び第４ｂ図と同様な図、第６ａ図及び第６ｂ図は
本考案ジェットエンジンによって後方推力を得ている状
態を示す、第４ａ図及び第４ｂ図と同様な図、第７図は
そのシャッター弁の開度などを調整するためのコンピュ
ータを示す図である。 ４１・・・タービン、４２・・・燃焼室、４３・・・圧
縮機、４４・・・ジェットノズル、４６・・・輻流ター
ボファン、５２．５３・・・シャッター弁。 「“、２ ／！（乎６ゞＳ ４９　　目４ｂ ”４９１1, 2, and 3 are views showing three different conventional jet engines, FIG. 4a is a view showing an example of a jet engine according to the present invention, and FIG. 4b is a view 4b--
4b, 5a, and 5b show the fourth jet engine in which downward thrust is obtained by the jet engine of the present invention.
Figures 6a and 6b are views similar to Figures 4a and 4b, Figures 6a and 6b are views similar to Figures 4a and 4b, and Figures 6a and 6b are views similar to Figures 4a and 4b. It is a diagram showing a computer for adjusting the opening degree of the shutter valve. 41... Turbine, 42... Combustion chamber, 43... Compressor, 44... Jet nozzle, 46... Radiation turbo fan, 52.53... Shutter valve. ““, 2 /! (乎6ゞS 49 目4b ”491

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 輻流ターボファンを備えたジェットエンジンにおいて、
該輻流ターボファンの回転により発生する気流を下方又
は後方若しくはその両方に流すように切替自在な一対の
シャッター弁を具備することを特徴とするジェットエン
ジン。In a jet engine equipped with a radial turbofan,
A jet engine characterized by comprising a pair of shutter valves that can be switched to allow airflow generated by the rotation of the radial turbofan to flow downward, backward, or both.
JP8289983U 1983-06-02 1983-06-02 jet engine Pending JPS59188956U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP8289983U JPS59188956U (en) 1983-06-02 1983-06-02 jet engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP8289983U JPS59188956U (en) 1983-06-02 1983-06-02 jet engine

Publications (1)

Publication Number Publication Date
JPS59188956U true JPS59188956U (en) 1984-12-14

Family

ID=30212856

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8289983U Pending JPS59188956U (en) 1983-06-02 1983-06-02 jet engine

Country Status (1)

Country Link
JP (1) JPS59188956U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006083856A (en) * 2004-09-15 2006-03-30 General Electric Co <Ge> Gas turbine engine having improved core system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006083856A (en) * 2004-09-15 2006-03-30 General Electric Co <Ge> Gas turbine engine having improved core system

Similar Documents

Publication Publication Date Title
JPS59188956U (en) jet engine
JPS59172254U (en) radiant fan jet engine
JPS58118215U (en) internal combustion engine
JPS606836U (en) Variable displacement turbo charger
JPS59157539U (en) turbo supercharger
JPS5956329U (en) engine exhaust turbo charger
JPS60149831U (en) Variable capacity turbocharger
JPS58165220U (en) Internal combustion engine intake system
JPS5873919U (en) Silencer for internal combustion engines
JPS5962233U (en) Internal combustion engine exhaust turbocharger device
JPS58186224U (en) Cooling devices for internal combustion engines, etc.
JPS60134834U (en) Turbo gear
JPS595725U (en) Exhaust turbocharger with variable nozzle
JPS58100223U (en) Heat shield device for turbocharger
JPS58158125U (en) turbo supercharger
JPS59114431U (en) gas turbine plant
JPS59184327U (en) Shaft seal structure of exhaust turbine type supercharger
JPS62193139U (en)
JPS59193954U (en) Engine-driven heat pump with turbo charger
JPH01149532U (en)
JPS6015918U (en) Engine-driven generator cooling system
JPS59144320U (en) rotary cup burner
JPS6010835U (en) axial turbine turbocharger
JPS608425U (en) Control device for turbocharger
JPS6032526U (en) Diesel engine with exhaust supercharger