F7-10 エンジンの Design of F7-10 High Bypass Turbofan Engine for P-1 Maritime Patrol Aircraft 空 部 ス 部 空エンジン 部 空 部 ス 部 空エンジン 部 F7-10 エンジン の P-1 の ファン エンジン 部
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1 F7-0 Design of F7-0 High Bypass Turbofan Engine for P- Maritime Patrol Aircraft 空 空 空 空 F7-0 P- ファ ( : ) 00 量 量 F7-0 6 tf F7-0 The F7-0, a turbofan engine for the P- maritime patrol aircraft operated by the Japanese Maritime Self-Defense Force ( JMSDF ), was developed by the Ministry of Defense Technical Research & Development Institute ( Current Acquisition, Technology & Logistics Agency ) and service entry of the production of the F7-0 engine commenced in 00. IHI is in charge of designing and producing the F7-0 engine ( including the prototype engine ). The F7-0 engine has achieved excellent fuel efficiency among the existing six-ton class engines. This paper presents the design overview of the F7-0 engine and its components.. 緒言 F7-0 ( 第 図 ) P- ( ) ( 第 図 ) ファ 000 ( : ) 00 量 ( XF7-0 XP- ) 量 P- P-C 第 図 P- ( ) Fig. P- maritime patrol aircraft ( ) 空 F7-0 6 tf バイパファ ファ. F7-0 設計および特徴 第 図 F7-0 Fig. External view of the F7-0 engine. に求められる特性 空 0 IHI Vol.57 No. ( 07 )
2 空 量 量 バイパ ファ ( XF5- ) コア ア MIL-E- 5007D ( ) イ JSSG-007A ( ) バイパファ FAR Part. ( 4 ) ICAO( International Civil Aviation Organization: 空 ) ( 5 ) ( 6 ). 熱サイクルおよび構成検討.. バイパ比と SFC 関係バイパ空気 コア空気 第 図 バイパ ファ 気 バイパ空気量 気 コア空気量 気 SFC( Specific Fuel Consumption: ) パ 量 SFC U 気 V ファ バイパ空気量 ( コア空気量 8 倍 ) * コア コア空気量 ( 注 ) *:F7-0 場合 第 図バイパ空気 コア空気 Fig. Bypass and core flow h th F n 量 Wf 空気量 m Fn = mv ( U ) ( ) h th エ 量 Q h th = mv ( U ) ( Wf Q) ( ) SFC ( ) ( ) ( ) Wf V + U SFC = = ( ) F h th Q n SFC 気 バイパ.. F7-0 熱サイクルおよび構成 F7-0 量 バイパ 8 気 SFC バイパ ファ コア ファ ファ ファ ファ ファ F7-0 コア XF5- ( LPC ) ( 7 ) ファ イ F7-0 NO x 量 F7-0 第 表 F7-0 第 4 図 F7-0 6 tf バイパ SFC ( 8 ) ( 9 ) IHI Vol.57 No. ( 07 )
3 第 表 F7-0 Table Specifications for the F7-0 engine ファ * kn ( tf ). ファ設計 60 ( 6 ) S F C * kg/h/dan 0.4 空 気 * 量 kg/s 40 バイパ 8 ファ ( 注 ) *: 気 ファ 量 量空気 イ 場合 F7-0 ファ イ.6 空 ファ空 量 第 5 図 ファ ( LPC ) ( ) ( ) ( LPT ) 第 4 図 F7-0 Fig. 4 F7-0 engine cross-section ( a ) 解析モデル ( b ) 解析モデル ( 外径側から見る ) ファ ( c ) 解析結果 第 5 図 ファ ( 0 ) Fig. 5 Transient analysis of deformation of fan blade impacted by foreign object ( 0 ) IHI Vol.57 No. ( 07 )
4 ファ ( 0 ) ファ ファ ファ 場合 ファ 量 第 6 図 ファ. 4 低圧圧縮機 ( LPC ) 設計 バイパ ファ F7-0 LPC ( ) LPC ファ LPC ファ ファ 合.7 第 7 図 LPC バイパ 場合 LPC ( ) LPC ファ空 LPC LPC 気 第 7 図 LPC Fig. 7 Low Pressure Compressor cross-section LPC LPC 量 量 LPC LPC 場合 LPC 量 量 LPC ( )ジ F7-0 LPC 量 バイパ 気バ. 5 高圧圧縮機 ( ) 設計 イ 7 LPC 6 量 8 アイ ( IGV ) ( SV ) ( a ) ( b ) ( c ) ファ ファ ファ 第 6 図ファ Fig. 6 Fan section IHI Vol.57 No. ( 07 )
5 ( SV ) アイ 第9図 量 気 バイパ 気 エジ 第 F7-0 バイパ 0 図 6 tf 8 空気量 空 ア. 6 燃焼器設計 CFD NOx ( Computational Fluid Dynamics ) 空 F7-0 第8図 CFD (a) イ 気 空気 コ イ モ F * モ (b) モ -S * モ 量 + 注 * F パ -S 第 8 図 CFD Fig. 8 multistage simulation by CFD ( Mach number distributions ) (a) (b) S パ 第 0 図 blade vibration mode analysis by FEM ( Displacement distributions ) (c) Fig. 9 4 Fig. 0 第 9 図 High Pressure Compressor section IHI Vol.57 No. ( 07 )
6 第 図 F7-0 イ 第 図 イ. 8 低圧タービ ( LPT ) 設計 500 LPT エ 量ファ 量 NOx ファ ICAO エ 量 (5) F 高圧タービ ( ) 設計 8 量 空 ジ 合 空気 空気 LPT LPT ジ フ パ LPT 第 図 LPT (a) (b) (c) 空気 イ 第 図 Fig. Combustion section (a) (b) (c) 注 Fig. 第 図 High Pressure Turbine section IHI Vol.57 No. ( 07 ) 5
7 LPT ジ 第 図 LPT Fig. Low Pressure Turbine cross-section. 9 制御 補機設計 イ イ ア エ 第 表 F7-0 第 4 図 F7-0 イ 場合 7 EMI ( Electromagnetic Interference: ) ぎ. 0 艤装設計. 9 節 気 空気 合 イ フ 量 ア CAD イ フ 合 CAD 第 5 図 CAD. 適用材料 量 第 表 F7-0 Table Controls and external components list of the F7-0 engine No. 量 イ イ イ イ 4 空気 イ 空気 VSV ア エ ア エ VBV ア エ LPC 気バ 気バ 気バ ECU NF T 4 T5 5 T45 LPT 6 パイ LPT EGT LPT イ イ 4 イ イ 量 5 ( 注 )VSV : VBV : 気バ ECU : NF : EGT : 6 IHI Vol.57 No. ( 07 )
8 フ ア イ イ 第 4 図 F7-0 Fig. 4 Controls and external components of the F7-0 engine ( a ) か ( b ) か ( c ) 側 ( ) アコ ( 注 ) アコ : 第 5 図 CAD Fig. 5 External design with D-CAD IHI Vol.57 No. ( 07 ) 7
9 :合 : ア 合 : 合 :FRP : 合 第 6 図 F7-0 Fig. 6 F7-0 engine materials 第 6 図 F7-0 ファ LPC 合 ア 合 ( FRP ) 合. 低騒音化設計 バイパ 気 ジ ファ ファ ファ ICAO ( 6 ) ア. 結言 F7-0 F7-0 6 tf バイパファ P- 謝辞 F7-0 量 ( : ) 参考文献 ( ) JMSDF ジ :( イ ) < > ( 05-- ) ( ) MIL-E-5007D:Engine, Aircraft, Turbojet and Turbofan, General Specification For US Military Specification ( ) ( ) JSSG-007A:Joint Service Specification Guide- Engines, Aircraft, Turbine ( 004. ) ( 4 ) FAR Part : Airworthiness Standards : Aircraft Engines Section. 76 ( 999 ) ( 5 ) ICAO ANNEX6:Volume II nd Edition Part III Chapter ( 99 ) ( 6 ) ICAO ANNEX6:Volume I 4th Edition Part II Chapter 4 ( 00 ) (7) : バイパ ファ Vol. 40 No. 0 5 pp (8) : ( XF7 ) GTSJ ( 7 ) 009 pp (9) : ( XF7-0 ) ( ) GTSJ ( 4 ) 0 pp ( 0 ) : ( XF7-0 ) ジ( 5 ) F0 ( JSASS ) 0 8 IHI Vol.57 No. ( 07 )
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