| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 321 | High lift device in supersonic zone | JP15444987 | 1987-06-23 | JPS641699A | 1989-01-06 | YAMADA YOSHIO |
| PURPOSE: To easily obtain high lift through increase in a pushing-up force from under by providing a shock wave generating device on a lower face of a flying object flying in a supersonic zone and by obtaining the high lift through pressure rise of a shock wave rear flow generated on the lower face of the flying object. CONSTITUTION: By providing a projection 2 constituting a shock wave generating device on a lower face of a flying object 1, a shock wave 3 is generated on a lower face of the flying object 1 flying at a supersonic speed, and pressure of a rear flow of the shock wave 3 is raised. This pressure rise increases a pushing-up force 4 from the lower face of the flying object 1 and generates high lift. When a high lift device is constituted merely by the projection 2 in this way, the pressure rise on the downstream side is determined by the speed of the flying object 1 or the shape of the projection 2. By movably arranging the projection on the lower face of the flying object 1 and by fluctuating it according to the flight state of the flying object 1, the pressure rise of the rear flow can be controlled according to the flight state. COPYRIGHT: (C)1989,JPO | ||||||
| 322 | Extendible airfoil track assembly | EP81200792.0 | 1981-07-08 | EP0045988A1 | 1982-02-17 | Cole, James Byron |
An actuation and extension mechanism for aerodynamic high-lift devices such as a wing leading edge slat or a wing trailing edge flap; wherein an aerodynamic panel (20) is connected to one end of an extendible track member (23) that is supported and guided by its other end through rollers (26) fixedly mounted to wing rib structure (15). The track member incorporates a separate rack gear segment (24) internally thereof as part of the extension or retraction mechanism and this combination of track and gear segment provides the primary support and drive means to the high-lift device. without compromising the structural strength, safety, or operational reliability of said combination. |
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| 323 | Extendible airfoil cable drum track assembly | EP81200789.6 | 1981-07-07 | EP0045987A1 | 1982-02-17 | Cole, James Byron |
An actuation and extension mechanism for aerodynamic high-lift devices such as a wing leading edge slat or a wing trailing edge flap; wherein an aerodynamic panel (14) is connected to one end of an extendible track member (20) that is supported and guided by its other end through rollers (22) fixedly mounted to wing rib structure (10). The track member incorporates a cable (18) and drum (19) arrangement as part of the extension or retraction mechanism; and this combination of track, cable and drum provides the primary support and drive means for the high-lift device, without compromising the structural strength or the stress safety of said combination. |
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| 324 | VARIABLE VALVE LIFT APPARATUS | KR20070131565 | 2007-12-14 | KR20090064010A | 2009-06-18 | KWAK YOUNG HONG; KWON KI YOUNG; SHIN KI UK; KONG JIN KOOK |
| A variable valve lift device is provided decrease fabrication cost through a simple configuration because there is no need to process the shape of the contact unit with a cam in a curvature. A variable valve lift device comprises low lift cams: a high lift cam which is equipped between the low lift cams; a low lift tappet body(200) which selectively contacts with the low lift cam; a high lift tappet body(300) which always contacts the high lift cam between the low lift tappet bodies; a guide unit(400) which reciprocates vertically the low lift tappet body and the high lift tappet body together; and a lost motion spring(480) which is placed between the guide unit and the low lift tappet body. | ||||||
| 325 | 가변밸브리프트 장치의 오작동 방지구조 | KR1020050121263 | 2005-12-10 | KR1020070061633A | 2007-06-14 | 오정한 |
| A malfunction preventing structure of a variable valve lift apparatus for an engine is provided to smoothly perform valve lift transformation under any condition of the engine. A malfunction preventing structure of a variable valve lift apparatus for an engine includes an outer body(1) and an inner body(7). The outer body transmits kinetic force of a high lift cam. The inner body is coupled inside the outer body such that the inner body is relatively rotatable through a shaft(3). The inner body has a locking pin arranged at the side opposite to the side connected with the shaft, such that the locking pin is protruded and retracted so as to switch the state locked to the high lift cam. A protrusion(9) is formed on the outer body so as to suppress protrusion of the locking pin. | ||||||
| 326 | Detection apparatus | US09505535 | 2000-02-17 | US06386482B1 | 2002-05-14 | Richard S Capewell |
| A detection apparatus for use with a system having a plurality of moveable surfaces, the apparatus comprising a signal transmission apparatus extending across each surface, a signal generator and a signal receiver. The apparatus further comprises a signal interrupter associated with adjacent ones of the surfaces and arranged to interrupt the transmission of a signal along the signal transmission apparatus upon relative movement of the adjacent ones of the surfaces occurring. The invention also relates to a leading edge high lift system of an aircraft wing having a plurality of moveable leading edge high lift surfaces. | ||||||
| 327 | Gas turbine engine | US3761042D | 1971-05-04 | US3761042A | 1973-09-25 | DENNING R |
| A gas turbine engine has a variable pitch fan and a first compressor mounted on one shaft and driven from a common turbine, together with a high pressure compressor and turbine on a second shaft, ducting to supply bleed air to high lift devices on an aircraft in which the engine is mounted, and means for bleeding air from the first compressor to the high lift devices when the fan blades are turned to fine pitch. A control system is included to maintain the first compressor speed at maximum when the high lift devices are being used.
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| 328 | Device for supporting acceptance/rejection of use of high lift work vehicle | JP2009195332 | 2009-08-26 | JP2011046464A | 2011-03-10 | SUGIYAMA MASANORI |
| <P>PROBLEM TO BE SOLVED: To support the determination whether or not a high lift work vehicle can be used when executing a distribution line work. <P>SOLUTION: A device for supporting acceptance/rejection of the use of a high lift work vehicle includes a power pole database 4 for storing power pole information such as the installation position of power poles and its peripheral map information in relation to the power pole number for identifying the power poles, and a support program 5 for supporting the determination whether or not the power pole work is possible by a boom of the high lift work vehicle while the high lift work vehicle is parted in the vicinity of the power pole of the input power pole number based on vehicle information including the input power pole number, the size of the high lift work vehicle, and the kind of the boom or the like, and power pole information of the power pole database 4. <P>COPYRIGHT: (C)2011,JPO&INPIT | ||||||
| 329 | Working vehicle | JP2005223857 | 2005-08-02 | JP2007038777A | 2007-02-15 | KUBO ATSUSHI; MORIYAMA AKIRA |
| PROBLEM TO BE SOLVED: To provide a working vehicle for operating a work device provided on a vehicle body, and enabling adjustment for making the center of gravity of the combination of the vehicle body and the work device overlap with a ground position of a turntable in plan view. SOLUTION: A road railer 1 includes the vehicle body 2 traveling with front and rear wheels 3a and 3b, a high lift work unit 8 provided on the vehicle body 2 and operating so that an attitude thereof on the vehicle body 2 varies, and the turntable 12 provided on the vehicle body 2 and protruding downward to lift the vehicle body 2, and operates the high lift work unit 8 so that the center of gravity of the combination of the vehicle body 2 and the high lift work unit 8 overlaps with the ground position 12a of the turntable 12 in plan view and thereafter lifts the vehicle body 12 with the turntable 12. In the road railer 1, the high lift work unit 8 is operated while making it correspond to a visual marking 13 so that the center of gravity of the combination overlaps with the ground position 12a in plan view. COPYRIGHT: (C)2007,JPO&INPIT | ||||||
| 330 | High lift work device | JP2000297306 | 2000-09-28 | JP2002104792A | 2002-04-10 | OTA MINORU; NOHARA YOSHITO; YAKUWA MASAKAZU |
| PROBLEM TO BE SOLVED: To provide a light and compact leveling mechanism in a high lift work device wherein a work stand is attached at a tip end portion of a boom moving upward/downward. SOLUTION: At the tip end portion of the boom 5 capable of moving upward/ downward to a base stand, a link member 65 and a piston rod 62 of a leveling cylinder 60 are rockably journaled within a vertical surfaces, and the other end of the link member 65 and a cylinder body 61 of the leveling cylinder are rockably journaled within the vertical surface, thereby composing the leveling mechanism 6. By attaching the work stand 8 to the cylinder body 61 through an oscillating mechanism 7, and actuating the leveling cylinder 60 to expand and contract, the work stand 8 is rockably arranged within the vertical surface with reference to the boom 5, thereby composing the high lift work device. COPYRIGHT: (C)2002,JPO | ||||||
| 331 | Klappenanordnung für einen Flugzeugtragflügel | EP86109811.9 | 1986-07-17 | EP0218021A1 | 1987-04-15 | Renken, Jürgen, Dr.-Ing.; Martens, Wilhelm, Dipl.-Ing. |
Eine Klappenanordnung für einen Flugzeugtragflügel (1) besteht aus jeweils wenigstens einer an der Tragflügelhinterkante angeordneten, ausfahrbaren Hochauftriebsklappe (2) sowie wenigstens einem dieser Klappe zugeordneten Spoiler (3). Ferner weist sie je eine der Hochauftriebsklappe bzw. dem Spoiler zugeordnete Stelleinrichtung (4, 5) auf. Die den Stelleneinrichtungen vorgeschalteten Steuer-und Regeleinrichtungen (6, 7) sind dabei über ein Kopplungselement (11) miteinander verbunden, das bei einer Veränderung der Position der Hochauftriebsklappe eine Nachführung des Spoilers derart bewirkt, daß zwischen der Klappe und dem Spoiler kein Luftspalt entsteht. |
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| 332 | Extendible airfoil track assembly | EP87200084.9 | 1981-07-08 | EP0227643A2 | 1987-07-01 | Cole, James Byron |
An actuation and extension mechanism for aerodynamic high-lift devices such as a wing leading edge slat or a wing trailing edge flap; wherein an aerodynamic panel (20) is connected to one end of an extendible track member (23) that is supported and guided by its other end through rollers (26) fixedly mounted to wing rib structure (l5). The track member incorporates a separate rack gear segment (24) internally thereof as part of the extension or retraction mechanism and this combination of track and gear segment provides the primary support and drive means to the high-lift device, without compromising the structural strenth, safety, or operational reliability of said combination. |
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| 333 | Retractable infill panel for high-lift device | EP13193183.4 | 2013-11-15 | EP2733062A2 | 2014-05-21 | Hodkisson, Mark; Wilson, James; Evans, Samuel |
The present invention provides an aircraft assembly with a fixed structure and a high-lift device. The fixed structure has a spar, a forward part which provides a foremost edge of an aircraft wing, and a lower part which provides a lower surface of the aircraft wing. A high-lift device is downwardly movable relative to the fixed structure from a stowed configuration to a deployed configuration. The high-lift device has a forward part which provides a foremost edge of the aircraft wing and a lower part which provides a lower surface of the aircraft wing. Downward movement of the high-lift device causes progressive opening of a lateral gap between the lower part of the high-lift device and the lower part of the fixed structure. A retractable infill panel is arranged to progressively extend from a retracted configuration to an extended configuration to fill the lateral gap.
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| 334 | HIGH-LIFT-GENERATING DEVICE, WING, AND NOISE-REDUCTION DEVICE FOR HIGH-LIFT-GENERATING DEVICE | EP10799817.1 | 2010-07-12 | EP2455282A1 | 2012-05-23 | HIRAI, Makoto; TAKENAKA, Keizo; IMAMURA, Taro; YAMAMOTO, Kazuomi; YOKOKAWA, Yuzuru |
In a high-lift-device, a wing, and noise reduction device for a high-lift-device that are capable of reducing noise generated when a flap is extended, preventing deterioration of aerodynamics characteristic when retracting the flap, and preventing an increase in weight, a flap main body (5) disposed so as to be extendable/retractable relative to a main wing and a protruding portion (6A-1) that smoothly protrudes at least at the vicinity of one end portion of a positive-pressure surface (PS) of the flap main body (5) in a direction away from the flap main body (5) are provided. |
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| 335 | WIND GENERATOR BLADE WITH HYPER-SUPPORTING ELEMENTS | EP09754010.8 | 2009-05-28 | EP2292926A1 | 2011-03-09 | ROMERO SANZ, Ignacio; JIMENEZ DE LAGO, Mario |
Wind turbine blade with high-lift devices in the leading edge and/or trailing edge (the latter has a relative thickness) in the root area, so that aerodynamic performance is improved and therefore the amount of energy extracted from the wind compared to traditional blades with cylindrical or oval roots. |
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| 336 | HIGH LIFT SYSTEM FOR AN AIRCRAFT AND METHOD FOR INFLUENCING THE HIGH LIFT CHARACTERISTICS OF AN AIRCRAFT | EP12717709.5 | 2012-04-27 | EP2701975A1 | 2014-03-05 | HUE, Xavier; SCHLIPF, Bernhard |
| A high lift system for an aircraft includes a basic body, a flap which is movably mounted on the basic body and has a flap edge, and a retaining element. The high lift system is set up to form a gap between the flap edge and the basic body. The retaining element is mounted on a region of the flap close to the flap edge and extends towards the basic body to restrict the distance between the flap edge and the basic body. The retaining element is preferably configured as a linear attachment means. Consequently, a gap dimension between a flap and a basic body can be influenced to restrict flexing effects during loading of the flap and of the basic body. | ||||||
| 337 | Einrichtung zur Verstellung von Hochauftriebsklappen an Flugzeugtragflügel | EP87107332.6 | 1987-05-20 | EP0253986A1 | 1988-01-27 | Heynatz, Johann Theodor, Prof. Dr.-Ing. |
Einrichtung zur Verstellung von Klappen, insbesondere von Hochauftriebsklappen bzw. Klappensystemen an der Hinterkante von Flugzeugtragflügeln, mit Tragarmen bzw. Auslegerarmen zur schwenkbaren Aufnahme der Hochauftriebsklappen und Klappenverstelleinrichtungen. Zur Verminderung des Luftwiderstandes sind insbesondere für die Marschflugphase eines Flugzeuges die außerhalb der Flügelkontur liegenden Klappen-Schwenklagerungen (25, 26) um Achsen (24; 22, 23), die sich in Richtung der Flügeltiefe erstrecken, in eine widerstandsarme Stellung einklappbar vorgesehen. Die Klappen-Schwenklagerungen (25, 26) und deren Träger (10, 11) sind von einem Hauptträger (9) aufgenommen und sind mit diesem einklappbar. |
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| 338 | SCHIEBEDACHSYSTEM FÜR EIN KRAFTFAHRZEUG | PCT/EP2017/050335 | 2017-01-09 | WO2017133865A1 | 2017-08-10 | HEIDAN, Michael |
Ein derartiges Schiebedachsystem mit einem beweglichen Dachteil (2), das mit einem Trägerprofil (3) fest verbunden ist, das mittels einer Verstellmechanik relativ zu einer Führungsschienenanordnung (6) in Hochrichtung und in Längsrichtung verlagerbar ist, wobei die Verstellmechanik über ein Antriebssystem antreibbar ist, das einen Antriebsschlitten (5) aufweist, der über einen Gleitschuh mit einem quer abragenden Kulissensteg (4) des Trägerprofils zusammenwirkt, wobei der Gleitschuh den Kulissensteg über eine in Hochrichtung obere Gleitanlage und eine untere Gleitstütze (10) stützt, ist bekannt. Erfindungsgemäß ist die untere Gleitstütze (7) formstabil gestaltet, und die obere Gleitanlage ist als elastisch nachgiebige Ausgleichskonstruktion ausgeführt. Einsatz bei Personenkraftwagen. |
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| 339 | HIGH-LIFT SYSTEM FOR AN AIRCRAFT | EP10798973.3 | 2010-12-23 | EP2516260A2 | 2012-10-31 | GÖLLING, Burkhard |
| A high-lift system (100) with a main wing (112) and adjustable flaps (110) as well as guiding devices (130) for holding the adjustable flaps (110) and adjustment devices (120) for adjusting the adjustable flaps (110), wherein the respective guiding device (130) and/or adjustment device (120) at least in part comprise/comprises a fairing (118), comprising a flow influencing (10) device for influencing the flow around the high- lift system (100), with at least one inlet line (20) with at least one inlet that is situated on or below the bottom of the high- lift system (100), wherein, furthermore, at least one outlet line (30) for air is provided that comprises a fluid-communicating connection to the inlet line (10) and comprises at least one outlet situated at the top in the region of at least one adjustable flap (110) of the high-lift system (100). | ||||||
| 340 | RETRACTABLE INFILL PANEL FOR HIGH-LIFT DEVICE | US14084828 | 2013-11-20 | US20140138487A1 | 2014-05-22 | Mark HODKISSON; James WILSON; Samuel EVANS |
| The present invention provides an aircraft assembly with a fixed structure and a high-lift device. The fixed structure has a spar, a forward part which provides a foremost edge of an aircraft wing, and a lower part which provides a lower surface of the aircraft wing. A high-lift device is downwardly movable relative to the fixed structure from a stowed configuration to a deployed configuration. The high-lift device has a forward part which provides a foremost edge of the aircraft wing and a lower part which provides a lower surface of the aircraft wing. Downward movement of the high-lift device causes progressive opening of a lateral gap between the lower part of the high-lift device and the lower part of the fixed structure. A retractable infill panel is arranged to progressively extend from a retracted configuration to an extended configuration to fill the lateral gap. | ||||||
