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1. 发明公开

EP0102353A4 AIRCRAFT LANDING WHEEL ROTATING MEANS. 失效
标题翻译： LANDUNGSRADANTRIEBSANORDNUNGFÜRFLUGZEUG。
公开(公告)号：EP0102353A4
公开(公告)日：1984-09-06
申请号：EP82902345
申请日：1982-08-13
申请人： SINCLAIR GRAHAM ROGER
发明人： SINCLAIR GRAHAM ROGER
IPC分类号： B64C25/40
CPC分类号： B64C25/40
摘要： An aircrfat landing wheel rotating means has an airscoop (21) mounted on the undercarriage unit (10) between a pair of landing wheels (16) fitted with tyres (14). A wheel outlet (25) in each side of the airscoop (21) directs the airflow over turbine blades (20) formed integrally with the landing wheels (16) as spokes interconnecting the rims to the wheel hubs (15) (which incorporate disc breaking systems). The airscoop (21) has a rearward venting outlet (24) which is selectively closed by hinged doors (29) and/or flaps (34) to direct the airflow to the turbine blades (20) or opened to allow a portion of the airflow to bypass the turbine blades (20) and so reduce the drag produced by the airscoop as the undercarriage unit (10) is lowered prior to landing or on take-off.
摘要翻译：空气着陆轮旋转装置具有安装在一个装配有轮胎（14）的一对着陆轮（16）之间的底架单元（10）上的空气调节器（21）。在飞机（21）的每一侧中的轮出口（25）将气流引导到与着陆轮（16）一体形成的涡轮机叶片（20）上，作为将轮辋与轮毂相互连接的轮辐（15）系统）。该空气调节器（21）具有后部通风出口（24），该后部通风出口通过铰链门（29）和/或翼片（34）选择性地关闭，以将气流引导至涡轮叶片（20）或打开以允许一部分气流以绕过涡轮机叶片（20）并且因此在着陆或起飞之前降低当底架单元（10）降低时由空气滤清器产生的阻力。

2. 发明授权

EP0102353B1 AIRCRAFT LANDING WHEEL ROTATING MEANS 失效
标题翻译：飞机着陆轮转向
公开(公告)号：EP0102353B1
公开(公告)日：1987-08-05
申请号：EP82902345.6
申请日：1982-08-13
申请人： SINCLAIR, Graham Roger
发明人： SINCLAIR, Graham Roger
IPC分类号： B64C25/40
CPC分类号： B64C25/40
摘要： An aircrfat landing wheel rotating means has an airscoop (21) mounted on the undercarriage unit (10) between a pair of landing wheels (16) fitted with tyres (14). A wheel outlet (25) in each side of the airscoop (21) directs the airflow over turbine blades (20) formed integrally with the landing wheels (16) as spokes interconnecting the rims to the wheel hubs (15) (which incorporate disc breaking systems). The airscoop (21) has a rearward venting outlet (24) which is selectively closed by hinged doors (29) and/or flaps (34) to direct the airflow to the turbine blades (20) or opened to allow a portion of the airflow to bypass the turbine blades (20) and so reduce the drag produced by the airscoop as the undercarriage unit (10) is lowered prior to landing or on take-off.

3. 发明公开

EP0102353A1 AIRCRAFT LANDING WHEEL ROTATING MEANS 失效
标题翻译：飞机着陆轮旋转装置
公开(公告)号：EP0102353A1
公开(公告)日：1984-03-14
申请号：EP82902345.0
申请日：1982-08-13
申请人： SINCLAIR, Graham Roger
发明人： SINCLAIR, Graham Roger
IPC分类号： B64C25
CPC分类号： B64C25/40
摘要： Des moyens de rotation des roues d'atterrissage d'un aéronef possèdent une prise d'air (21) montée sur le train d'atterrissage (10) entre une paire de roues d'atterrissage (16) sur lesquelles sont montés des pneus (14). Une sortie de roue (25) de chaque côté de la prise d'air (21) dirige le flux d'air sur les aubes de turbine (20) formées de manière solidaire avec les roues d'aterrissage (16) sous la forme de rayons reliant les pourtours des roues au moyeu (15) des roues (dans lesquels sont incorporés des systèmes de freinage à disque). La prise d'air (21) possède une sortie d'évent vers l'arrière (24) qui est fermée sélectivement par des portes à charnière (29) et/ou des volets (34) pour diriger le flux d'air vers les aubes de turbine (20) ou est ouverte pour permettre une partie du flux d'air de bypasser les aubes de turbine (20) et donc de réduire la trainée produite par la prise d'air lorsque le train d'atterrissage (10) est abaissé avant d'atterrir ou au moment du décollage.
摘要翻译：用于旋转飞机的着陆轮的装置具有安装在起落架（10）上的一对进入轮（16）之间的进气口（21），轮胎安装在所述一对着轮（16）上 14）。在进气口（21）的每一侧上的车轮出口（25）将空气流引导到与着陆轮（16）一体形成的涡轮叶片（20）上，形式为将车轮的周边连接到车轮轮毂（其中包括盘式制动系统）的轮辐。进气口（21）具有后部通风口（24），后部通风口通过铰链门（29）和/或翼片（34）选择性地关闭，以将气流引导至涡轮叶片（20）或打开以允许部分气流绕过涡轮叶片（20）并因此减少当起落架（10）为空气时由进气口产生的阻力降落前或降落时降低。

4. 发明公开

EP0170658A1 AIRCRAFT UNDERCARRIAGE ASSEMBLIES 失效
标题翻译：飞机起落架组件。
公开(公告)号：EP0170658A1
公开(公告)日：1986-02-12
申请号：EP84901934.0
申请日：1984-05-14
申请人： SINCLAIR, Graham Roger
发明人： SINCLAIR, Graham Roger
IPC分类号： B64C25
CPC分类号： B64C25/40
摘要： Un montage de train d'atterrissage d'avion (10) possède un chariot de train d'atterrissage (15) dont la paire de roues arrière (25) est montée sur un élément de support arrière (1) déplaçable de manière pivotante par rapport à l'élément de support avant (16) lorsque l'avion roule au sol afin de produire un effet de direction, mais blocable d'une façon alignée avec la paire de roues avant (24) pendant le vol. Une roue (37) de chaque paire de roues (24, 25) est reliée à l'axe respectif (22, 23), la roue (37) possédant des rayons (39) similaires à une turbine qui reçoivent de l'air dirigé par un manche-à-air ouvert (45) pour faire tourner la roue (37) jusqu'à la vitesse. Un montage d'embrayage (55) relie ensuite de manière opérationnelle la seconde roue (49) à l'axe respectif (22, 23) afin de permettre de faire tourner ladite roue (49) à la vitesse. Les roues (37, 49) sont freinées de manière indépendante par des paires respectives de disque de friction et de disque de frein (61, 64; 68, 70) engagées par des pistons de frein (67, 71) sur le carter d'axe respectif (17, 21).

5. 发明专利

AU2002303093A1 Mycobacterial vaccines 未知
公开(公告)号：AU2002303093A1
公开(公告)日：2002-09-12
申请号：AU2002303093
申请日：2002-02-20
申请人： GAORA PEADAR CAOIMHIN EOIN O , STEWART GRAHAM ROGER , IMP COLLEGE INNOVATIONS LTD , YOUNG DOUGLAS BROWNLIE
发明人： O'GAORA PEADAR CAOIMHIN EOIN , STEWART GRAHAM ROGER , YOUNG DOUGLAS BROWNLIE
IPC分类号： A61K39/04 , C07K14/35
摘要： Methods and compositions for the treatment and prevention of infectious diseases are provided. In particular, efficient vaccines comprising genetically modified pathogens are provided. The vaccines generally comprise mycobacterial mutants having modified protein production capabilities. In one embodiment, the mutants overexpress heat shock protein. In a specific embodiment, the mycobacterial mutant overexpresses heat shock proteins 60 and/or 70. Also provided are modified BCG vaccines capable of overexpressing heat shock proteins 60 and/or 70.

6. 发明专利

CA1340066C GRAFT COPOLYMERS AND BLENDS THEREOF WITH POLYOLEFINS 未知
公开(公告)号：CA1340066C
公开(公告)日：1998-09-29
申请号：CA617058
申请日：1996-08-28
申请人： WORK WILLIAM JAMES , ILENDA CASMIR STANISLAUS , BORTNICK NEWMAN , GRAHAM ROGER KENNETH
发明人： WORK WILLIAM JAMES , ILENDA CASMIR STANISLAUS , BORTNICK NEWMAN , GRAHAM ROGER KENNETH
IPC分类号： C08L51/06
摘要： A novel graft copolymer capable of imparting to a polyolefin when blended therewith high tensile modulus and high sag resistance without increasing melt viscosity, and a method of making the same. The graft copolymer is a polyolefin having a relatively high weight-average molecular weight methacrylate polymer grafted thereto. The graft copolymer is formed by dissolving or swelling a non-polar polyolefin in an inert hydrocarbon solvent, heating to dissolve the polyolefin, and while stirring the mixture, adding a methacrylate monomer, together with an initiator to produce a constant, low concentration of radicals, to form a graft copolymer with a high molecular weight polymer chain covalently bonded or grafted to the polyolefin backbone. The graft copolymer can be separated from the solvent, isolated by volatilizing the solvent, for example in a devolatilizing extruder, and extruded into a desired shape such as a sheet, tube or the like. This graft copolymer can be blended with a polyolefin matrix. The blend exhibits improved physical properties in the melt, upon cooling, and in the solid state, and is useful in cast and oriented films, solid extruded rod and profile, foamed rod, profile and sheet, blown bottles and the like. The graft copolymer further improves compatibility in a wide range of polymer blends.

7. 发明专利

GB2451065B Traffic flow control device 未知
公开(公告)号：GB2451065B
公开(公告)日：2012-06-20
申请号：GB0713721
申请日：2007-07-14
申请人： LEE GRAHAM ROGER RICHARD , LEE RICHARD MICHAEL ROBERT
发明人： LEE GRAHAM ROGER RICHARD , LEE RICHARD MICHAEL ROBERT
IPC分类号： E01F13/10 , E01F13/12

8. 发明专利

GB2451065A Traffic flow control device 未知
公开(公告)号：GB2451065A
公开(公告)日：2009-01-21
申请号：GB0713721
申请日：2007-07-14
申请人： LEE GRAHAM ROGER RICHARD , LEE RICHARD MICHAEL ROBERT
发明人： LEE GRAHAM ROGER RICHARD , LEE RICHARD MICHAEL ROBERT
IPC分类号： E01F13/10 , E01F13/12
摘要： The traffic flow control device, primarily for use in car parks and the like, comprises a support body 41 and at least one barrier member 45 supported by and moveable relative to the support body between a first position in which it impedes the flow of traffic in a first direction and a second position to which it is moveable to permit a flow of traffic in a second, opposite direction, the device having magnetic biasing elements comprising two elements 47,49 associated respectively with the support body and barrier member and arranged to provide a biasing force to urge the barrier member to move from the second position to the first position and normally to be at rest in said first position. At least one of the elements may be a permanent magnet or an electro-magnet and/or one of the elements may be formed from a ferrous material. The device may comprise two magnets arranged to repel one another. The magnetic elements may be fully embedded in the support and barrier elements or located in dovetail-shaped recesses. The support body may be provided with a footprint sized to facilitate the use of adhesive to secure the device to the ground.

9. 发明专利

DE3276902D1 AIRCRAFT LANDING WHEEL ROTATING MEANS 未知
公开(公告)号：DE3276902D1
公开(公告)日：1987-09-10
申请号：DE3276902
申请日：1982-08-13
申请人： SINCLAIR GRAHAM ROGER
发明人： SINCLAIR GRAHAM ROGER
IPC分类号： B64C25/40
摘要： PCT No. PCT/AU82/00130 Sec. 371 Date Jun. 1, 1983 Sec. 102(e) Date Jun. 1, 1983 PCT Filed Aug. 13, 1982 PCT Pub. No. WO83/01239 PCT Pub. Date Apr. 14, 1983.An aircraft landing wheel rotating means has an airscoop (21) mounted on the undercarriage unit (10) between a pair of landing wheels (16) fitted with tires (14). A wheel outlet (25) in each side of the airscoop (21) directs the airflow over turbine blades (20) formed integrally with the landing wheels (16) as spokes interconnecting the rims to the wheel hubs (15) (which incorporate disc breaking systems). The airscoop (21) has a rearward venting outlet (24) which is selectively closed by hinged doors (29) and/or flaps (34) to direct the airflow to the turbine blades (20) or opened to allow a portion of the airflow to bypass the turbine blades (20) and so reduce the drag produced by the airscoop as the undercarriage unit (10) is lowered prior to landing or on take-off.

10. 发明专利

AU8764082A AIRCRAFT LANDING WHEEL ROTATING MEANS 未知
公开(公告)号：AU8764082A
公开(公告)日：1983-04-27
申请号：AU8764082
申请日：1982-08-13
申请人： SINCLAIR GRAHAM ROGER
发明人： SINCLAIR G R
IPC分类号： B64C25/40

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