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11. 发明专利

JP2021031021A クロスフローファン、これを備えた揚力発生装置およびこれを備えた航空機审中-公开
公开(公告)号：JP2021031021A
公开(公告)日：2021-03-01
申请号：JP2019156887
申请日：2019-08-29
申请人：三菱重工業株式会社
发明人：今井和宏 , 森崎雄貴 , 小田雅之 , 齋木康寛
IPC分类号： B64C9/38 , B64C21/06
摘要：【課題】流体損失を低減することができるクロスフローファンを提供する。【解決手段】回転軸線O1の回りに周方向に所定間隔を空けて配置された複数のベーン15と、ベーン15の外周側に配置された舌部17と、各ベーン15から流体が排出される排出流路の壁面に沿って流体を噴出する噴出部32,34,36と、を備えている。各ベーン15を挟んで舌部17に対向する位置に設けられた対向壁部23を備え、対向壁部23は、各ベーン15が回転する際に形成する軌跡の外周における曲率半径と同等とされた上流壁部28と、上流壁部28に接続されるとともに上流壁部28よりも曲率半径が徐々に大きくなる下流壁部29と、下流壁部29に接続されるディフューザ壁部30とを備えている。第1噴出部32は、下流壁部29に設けられている。【選択図】図2

12. 发明专利

JPH04501159A 失效
公开(公告)号：JPH04501159A
公开(公告)日：1992-02-27
申请号：JP51054189
申请日：1989-08-21
IPC分类号： B63H11/10 , B63H11/14 , B63H25/46 , B64C9/38 , B64C15/02 , F02K1/00 , F02K1/08 , F02K1/12 , F02K1/78 , F02K9/80 , F02K9/84 , F42B10/66

13. 发明专利

JPS647920B2 失效
公开(公告)号：JPS647920B2
公开(公告)日：1989-02-10
申请号：JP16844379
申请日：1979-12-26
申请人： BOEING CO
发明人： PIITAA KEI SHII RUDORUFU
IPC分类号： B64C9/38 , B64C3/50 , B64C9/02 , B64C9/16 , B64C9/18 , B64D27/18
摘要： A trailing edge flap moveable from a stowed position behind a wing to a downwardly and rearwardly extending position to deflect jet exhaust from an upper surface blowing jet engine downwardly and rearwardly to augment lift. The actuating mechanism rotates the flap about a variable radius which maintains the upper surface of the flap in contact with and generally in tangential alignment with the trailing edge of the upper surface of the wing. This mechanism comprises forward and rear radius links pivotally mounted at their lower ends to a stationary mounting arm, and extending upwardly and divergently therefrom to attach to the flap. In two embodiments, the rear radius link has its pivot end mounted to a moveable member which in turn enables the flap to be rotated so that its forward end moves downwardly. Thus, in its fully deployed position, the flap can be rotated to form a slot between the aft end of the wing and the leading edge of the flap.

14. 实用新型

JPS5586000U 失效
公开(公告)号：JPS5586000U
公开(公告)日：1980-06-13
申请号：JP16900478
申请日：1978-12-11
IPC分类号： B64C9/38

15. 发明专利

JPS4918397B1 失效
公开(公告)号：JPS4918397B1
公开(公告)日：1974-05-09
申请号：JP522769
申请日：1969-01-23
IPC分类号： F02K1/78 , B64C9/38 , B64C15/00

16. 发明专利

JPH0911991A COANDA EFFECT-HIGH DYNAMIC LIFT GENERATOR 失效
公开(公告)号：JPH0911991A
公开(公告)日：1997-01-14
申请号：JP16739695
申请日：1995-07-03
申请人： MITSUBISHI HEAVY IND LTD
发明人： NAGAHATA MASASHI
IPC分类号： B64C9/34 , B64C9/38 , B64C21/04
摘要： PROBLEM TO BE SOLVED: To generate a high dynamic lift needed for takeoff and landing in jetting a jet stream in the circumferential direction of an outer peripheral sur face of a cylindrical body by providing a shift mechanism to shift the cylindrical body from an operating position disposed in a rear edge of a main blade to a housing position in the main blade. SOLUTION: A coanda effect-high dynamic lift generator disposed in a rear edge of a main blade 1 moves a cylindrical body 4 by a link mechanism 2 driven by an actuator 5. Namely, in a cruise or the like needing no generation of the high dynamic lift, the cylindrical body 4 is housed in the tip of the link mechanism 2 collapsed into a fair ring 7 of the main blade. On the other hand, in the takeoff/landing needing the high dynamic lift, the cylindrical body 4 is shifted to the rear edge side to be projected below the rear edge of the main wing 1. Engine exhaust introduced through a duct in the main blade 1 is jetted circumferentially of the outer peripheral surface of the cylindrical body 4, so that a stream on the main blade is induced to generate a circulating stream and generate a large dynamic lift even in low speed.

17. 发明专利

JPS5813397B2 失效
公开(公告)号：JPS5813397B2
公开(公告)日：1983-03-14
申请号：JP14860879
申请日：1979-11-16
申请人： KOKU UCHU GIJUTSU KENKYU SHOCHO
发明人： MAITA MASATAKA , MATSUKI MASAKATSU , TORISAKI TADAO
IPC分类号： B64C9/38 , B64C15/02 , B64D27/18

18. 发明专利

JPS5671699A HIGH LIFTING DEVICE ACCORDING TO USB SYSTEM 失效
公开(公告)号：JPS5671699A
公开(公告)日：1981-06-15
申请号：JP14860879
申请日：1979-11-16
申请人： NAT AEROSPACE LAB
发明人： MAITA MASATAKA , MATSUKI MASAKATSU , TORISAKI TADAO
IPC分类号： B64C9/38 , B64C15/02 , B64D27/18

19. 发明专利

JPS5594895A WORKING MECHANISM MANUFACTURED SO THAT IT BE USED WITH UPPER SURFACE SPRAYING TYPE POWER SYSTEM LIFT SYSTEM OF AIRCRAFT 失效
公开(公告)号：JPS5594895A
公开(公告)日：1980-07-18
申请号：JP16844379
申请日：1979-12-26
申请人： BOEING CO
发明人： PIITAA KEI SHII RUDORUFU
IPC分类号： B64C9/38 , B64C3/50 , B64C9/02 , B64C9/16 , B64C9/18 , B64D27/18
摘要： A trailing edge flap moveable from a stowed position behind a wing to a downwardly and rearwardly extending position to deflect jet exhaust from an upper surface blowing jet engine downwardly and rearwardly to augment lift. The actuating mechanism rotates the flap about a variable radius which maintains the upper surface of the flap in contact with and generally in tangential alignment with the trailing edge of the upper surface of the wing. This mechanism comprises forward and rear radius links pivotally mounted at their lower ends to a stationary mounting arm, and extending upwardly and divergently therefrom to attach to the flap. In two embodiments, the rear radius link has its pivot end mounted to a moveable member which in turn enables the flap to be rotated so that its forward end moves downwardly. Thus, in its fully deployed position, the flap can be rotated to form a slot between the aft end of the wing and the leading edge of the flap.

20. 发明专利

JPS54114631A APPARATUS FOR CONTROLLING EXHAUST NOISE FROM JET ENGINE 失效
公开(公告)号：JPS54114631A
公开(公告)日：1979-09-06
申请号：JP809979
申请日：1979-01-26
申请人： BOEING CO
发明人： RATSUSERU RUIZU SOONNOTSUKU , CHIYAARUZU PERII RAITO
IPC分类号： B64C9/38 , F02K1/40 , F02K1/48

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