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1. 发明授权

US5135357A Main helicopter rotor 失效
标题翻译：主要直升机转子
公开(公告)号：US5135357A
公开(公告)日：1992-08-04
申请号：US681149
申请日：1991-04-05
申请人： Santino Pancotti
发明人： Santino Pancotti
IPC分类号： B64C27/35
CPC分类号： B64C27/35 , Y10S416/50
摘要： A main helicopter rotor having a number of blades and wherein a drive shaft supports, at its top end, an annular hub integral with the drive shaft and in turn supporting, via a spherical elastomeric joint having its center on the axis of the drive shaft, and an elastic axial suspension, a toroidal body surrounding the drive shaft. Each blade is connected to the hub by a connecting element extending through both the hub and the toroidal body, and connected respectively to the same by a first and second spherical elastomeric bearing.
摘要翻译：具有多个叶片的主要直升机转子，并且其中驱动轴在其顶端支撑与驱动轴一体的环形轮毂，并通过其中心在驱动轴的轴线上的球形弹性体接头支撑，以及弹性轴向悬架，围绕驱动轴的环形体。每个叶片通过延伸穿过轮毂和环形体的连接元件连接到轮毂，并通过第一和第二球形弹性轴承分别连接到其上。

2. 发明授权

US08381630B2 Aircraft wing 有权
标题翻译：飞机机翼
公开(公告)号：US08381630B2
公开(公告)日：2013-02-26
申请号：US12479051
申请日：2009-06-05
申请人： Santino Pancotti , Dante Ballerio
发明人： Santino Pancotti , Dante Ballerio
IPC分类号： F41A9/29
CPC分类号： F41A9/34 , B64C27/04 , B64C2025/325 , B64D7/04 , F41A9/79
摘要： A wing for an aircraft having at least one weapon, and a feed duct for feeding the weapon with ammunition supplied in the form of a belt; the wing has a compartment for housing a portion of the belt and connectable to a loading opening of the feed duct.
摘要翻译：用于具有至少一种武器的飞机的翼，以及用于以带形式供应的弹药供给武器的进料管; 机翼具有用于容纳皮带的一部分并可连接到进料管的装载开口的隔室。

3. 发明申请

US20120061517A1 AIRCRAFT 有权
标题翻译：飞机
公开(公告)号：US20120061517A1
公开(公告)日：2012-03-15
申请号：US12580928
申请日：2009-10-16
申请人： Santino Pancotti , Dante Ballerio , Fabio Nannoni
发明人： Santino Pancotti , Dante Ballerio , Fabio Nannoni
IPC分类号： B64C1/22 , B64C27/22 , B64C1/14 , B64C27/04
CPC分类号： B64C1/1415
摘要： An aircraft capable of hovering, and having a fuselage in turn having a nose, a tail portion at the opposite end to the nose, and a cabin interposed between the nose and the tail portion; the cabin has a loading opening at the opposite end to the nose, and a first wall movable between a closed position engaging at least one portion of the loading opening, and an open position allowing free access to the portion of the loading opening; and, working from the tail portion towards the nose, the first wall in the open position extends on the opposite side of a first edge of the loading opening with respect to a second edge, opposite the first edge, of the loading opening.
摘要翻译：一种能够悬停的机身，机身又具有鼻子，在与鼻子相对的端部具有尾部，以及插入在鼻子和尾部之间的舱室; 所述舱室在与所述鼻部相对的端部处具有加载开口，并且可在接合所述装载开口的至少一部分的关闭位置和允许自由进入所述装载开口部分的打开位置之间移动的第一壁; 并且从尾部向鼻部工作时，处于打开位置的第一壁相对于装载开口的第一边缘的第二边缘在装载开口的第一边缘的相对侧延伸。

4. 发明申请

US20100096492A1 Helicopter 有权
标题翻译：直升机
公开(公告)号：US20100096492A1
公开(公告)日：2010-04-22
申请号：US12581560
申请日：2009-10-19
申请人： Santino Pancotti , Dante Ballerio , Attilio Colombo
发明人： Santino Pancotti , Dante Ballerio , Attilio Colombo
IPC分类号： B64C27/04
CPC分类号： B64C27/001 , Y10S416/50
摘要： A helicopter having a rotor, a fuselage, and a transmission connected functionally to the rotor; the helicopter has a supporting body supporting at least the transmission, and connecting means having a first connecting member and at least one second connecting member connected to the supporting body and the fuselage respectively; and the connecting means have elastic means interposed between the first and second connecting member.
摘要翻译：具有转子，机身和与转子功能相连的变速器的直升机; 所述直升机具有至少支撑所述变速器的支撑体，并且所述连接装置具有分别连接到所述支撑体和所述机身的第一连接构件和至少一个第二连接构件; 并且所述连接装置具有插入在所述第一和第二连接构件之间的弹性装置。

5. 发明申请

US20100044508A1 AIRCRAFT WING 有权
标题翻译：飞机票
公开(公告)号：US20100044508A1
公开(公告)日：2010-02-25
申请号：US12479051
申请日：2009-06-05
申请人： Santino Pancotti , Dante Ballerio
发明人： Santino Pancotti , Dante Ballerio
IPC分类号： B64C3/00 , F41A9/29 , F41A9/34 , F41A9/61 , B64C3/18
CPC分类号： F41A9/34 , B64C27/04 , B64C2025/325 , B64D7/04 , F41A9/79
摘要： A wing for an aircraft having at least one weapon, and a feed duct for feeding the weapon with ammunition supplied in the form of a belt; the wing has a compartment for housing a portion of the belt and connectable to a loading opening of the feed duct.
摘要翻译：用于具有至少一种武器的飞机的翼，以及用于以带形式供应的弹药供给武器的进料管; 机翼具有用于容纳皮带的一部分并可连接到进料管的装载开口的隔室。

6. 发明授权

US4375940A Rotor shaft with internal controls for helicopters 失效
标题翻译：转子轴带直升机内部控制
公开(公告)号：US4375940A
公开(公告)日：1983-03-08
申请号：US114963
申请日：1980-01-24
申请人： Bruno Lovera , Santino Pancotti
发明人： Bruno Lovera , Santino Pancotti
IPC分类号： B64C27/59 , B64C27/605 , B64C27/72 , B64C27/74
CPC分类号： B64C27/72 , B64C27/605 , Y02T50/34
摘要： A rotor shaft for helicopters in which a main rotatable shaft is tubular and supports in its interior a shaft (25) which is angularly fixed relative to the helicopter body and disposed coaxially to said main shaft; a swivel plate assembly being coupled to said fixed inner shaft and being disposed, together with at least part of a plurality of kinematic linkages connecting said swivel plate to the rotor blades and a plurality of actuator means controlling the position of said swivel plate, inside the space lying between said main shaft and said inner shaft.
摘要翻译：一种用于直升机的转子轴，其中主旋转轴是管状的并且在其内部支撑相对于直升机主体成角度地固定并与所述主轴同轴设置的轴（25）; 旋转板组件联接到所述固定内轴并且与将所述旋转板连接到转子叶片的多个运动连接件的至少一部分一起设置，并且多个致动器装置控制所述旋转板的位置，位于所述主轴和所述内轴之间的空间。

7. 发明授权

US4369019A Helicopter rotor comprising elastomer joints 失效
标题翻译：直升机转子包括弹性体接头
公开(公告)号：US4369019A
公开(公告)日：1983-01-18
申请号：US245721
申请日：1981-03-20
申请人： Bruno Lovera , Santino Pancotti
发明人： Bruno Lovera , Santino Pancotti
IPC分类号： B64C27/32 , B64C27/35 , B64C27/48 , B64C27/72 , B64C27/38
CPC分类号： B64C27/322 , B64C27/35
摘要： A helicopter rotor comprising elastomer joints, in which each blade is connected to a rotatable hub by means of a yoke constituted by a single U-shaped piece and mounted through a relative aperture provided in said hub;each yoke being connected to a transverse arm outwardly bordering said aperture, by means of a U stirrupembracing the relative said arm and provided with two overlying appendices extending outwards and having two surfaces inclined towards the other and acting as stop surfaces for two rocker arms constituting a devicefor controlling the flapping movements of said blade; said two rocker arms being mounted rotatable in a substantially vertical plane passing through the axis of the relative blade and being supported by a lever for controlling the pitch of this latter.
摘要翻译：一种包括弹性体接头的直升机转子，其中每个叶片通过由单个U形件构成的轭连接到可旋转毂，并通过设置在所述毂中的相对孔安装; 每个轭通过包围相对所述臂的U形镫形连接到与所述孔对接的横向臂，并且设置有向外延伸的两个上覆附件，并且具有朝向另一个倾斜的两个表面，并且用作构成的两个摇臂的止动表面用于控制所述叶片的扑动运动的装置; 所述两个摇臂被安装成可旋转地穿过相对叶片的轴线的基本上垂直的平面，并且由杠杆支撑，以控制后者的俯仰。

8. 发明授权

US4342540A Articulated rotor for helicopters 失效
标题翻译：用于直升机的铰接式转子
公开(公告)号：US4342540A
公开(公告)日：1982-08-03
申请号：US113726
申请日：1980-01-21
申请人： Bruno Lovera , Santino Pancotti , Emilio Pariani , Giuseppe Virtuani
发明人： Bruno Lovera , Santino Pancotti , Emilio Pariani , Giuseppe Virtuani
IPC分类号： B64C27/32 , B64C27/35 , B64C27/38
CPC分类号： B64C27/322 , B64C27/35
摘要： The multi-blade articulated rotor for helicopters, comprises a hub connected to a shaft rotatable substantially about a vertical axis, the hub being in the form of a plate comprising a plurality of perforations, each of which defines a bridge of material of said plate between a part of the edge of said perforation and a part of the edge of said plate; a plurality of yokes, each of which is substantially of U shape and comprises a pair of substantially parallel arms and a base element which connects together one end of said arms, the other end of the arms being connected to one of said blades, said base element being inserted into one of said perforations in the hub; a plurality of elastomer bearings, each of which is disposed between said base element of a yoke and the corresponding hub bridge; and means for limiting the amplitude of the swivel movement which each of said yokes can make substantially in a vertical plane.
摘要翻译：用于直升机的多叶片铰接转子包括连接到基本上绕垂直轴线旋转的轴的毂，所述轮毂为包括多个穿孔的板的形式，每个穿孔限定所述板的材料的桥接在所述穿孔的边缘的一部分和所述板的边缘的一部分; 多个轭，其大致为U形，并且包括一对基本平行的臂和将所述臂的一端连接在一起的基座元件，所述臂的另一端连接到所述刀片之一，所述基座元件被插入到所述毂中的所述穿孔之一中; 多个弹性体轴承，每个弹性体轴承设置在轭的所述基座元件和对应的毂桥之间; 以及用于限制旋转运动的幅度的装置，每个所述轭可以基本上在垂直平面上形成。

9. 发明申请

US20090321556A1 Helicopter with an improved vibration control device 有权
标题翻译：直升机具有改进的振动控制装置
公开(公告)号：US20090321556A1
公开(公告)日：2009-12-31
申请号：US11436928
申请日：2006-05-15
申请人： Santino Pancotti , Attilio Colombo
发明人： Santino Pancotti , Attilio Colombo
IPC分类号： B64C27/04 , B64C27/51
CPC分类号： B64C27/001 , B64C2027/002
摘要： A helicopter having a rotor, a fuselage connected to the rotor by connecting means, and a control device for controlling vibration of the fuselage; the control device including generating means for generating signals associated with vibration of the fuselage, and actuating means for producing a force on the fuselage associated with the signals to reduce vibration; and the actuating means being carried by the connecting means.
摘要翻译：具有转子，通过连接装置连接到转子的机身的直升机和用于控制机身振动的控制装置; 所述控制装置包括用于产生与所述机身的振动相关联的信号的发生装置，以及用于在与所述信号相关联的机身上产生力以减少振动的致动装置; 并且致动装置由连接装置承载。

10. 发明授权

US06666407B2 Helicopter undercarriage 有权
标题翻译：直升机起落架
公开(公告)号：US06666407B2
公开(公告)日：2003-12-23
申请号：US10304910
申请日：2002-11-26
申请人： Santino Pancotti
发明人： Santino Pancotti
IPC分类号： B64C2514
CPC分类号： B64C25/14 , B64C2025/325
摘要： An undercarriage for a helicopter, having a supporting structure connectable to the fuselage of the helicopter, a wheel suspended from the supporting structure, and a shock absorbing member which has a bottom end portion hinged to the wheel, and is interposed, in use, between the wheel and the fuselage. The supporting structure has an attachment fixable to the fuselage, and a first and a second beam having first connecting portions hinged about a first axis to each other and to a top end portion of the shock absorbing member. Second connecting portions are connected to separate portions of the attachment in articulated manner and lower down with respect to the first connecting portions.
摘要翻译：一种用于直升机的起落架，具有可连接到直升机的机身的支撑结构，从支撑结构悬挂的车轮，以及具有铰接到车轮的底端部分的减震构件，并且在使用中介于车轮和机身。支撑结构具有可固定到机身的附件，以及第一和第二梁，其具有围绕第一轴线彼此铰接并且与冲击吸收构件的顶端部分铰接的第一连接部分。第二连接部分以铰接的方式连接到附件的分离部分，并相对于第一连接部分向下连接。

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