CN1610267B - 微型设备和装备有微型设备的蜂窝式电话 - Google Patents

微型设备和装备有微型设备的蜂窝式电话 Download PDF

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CN1610267B
CN1610267B CN2004100857641A CN200410085764A CN1610267B CN 1610267 B CN1610267 B CN 1610267B CN 2004100857641 A CN2004100857641 A CN 2004100857641A CN 200410085764 A CN200410085764 A CN 200410085764A CN 1610267 B CN1610267 B CN 1610267B
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micromodule equipment
rotor
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CN1610267A (zh
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P·佩洛
B·派雷蒂
R·菲尼兹奥
C·卡维格内塞
P·雷佩特托
D·博尔利
D·卡佩洛
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/20—Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/02—Aircraft not otherwise provided for characterised by special use
    • B64C39/028—Micro-sized aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/80—UAVs characterised by their small size, e.g. micro air vehicles [MAV]
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B64U30/29—Constructional aspects of rotors or rotor supports; Arrangements thereof
    • B64U30/294—Rotors arranged in the UAV body
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/11—Propulsion using internal combustion piston engines
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/13—Propulsion using external fans or propellers
    • B64U50/14—Propulsion using external fans or propellers ducted or shrouded
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04M—TELEPHONIC COMMUNICATION
    • H04M1/00—Substation equipment, e.g. for use by subscribers
    • H04M1/02—Constructional features of telephone sets
    • H04M1/21—Combinations with auxiliary equipment, e.g. with clocks or memoranda pads
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/10—Rotorcrafts
    • B64U10/13—Flying platforms
    • B64U10/14—Flying platforms with four distinct rotor axes, e.g. quadcopters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2101/00—UAVs specially adapted for particular uses or applications
    • B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00—UAVs characterised by their flight controls
    • B64U2201/20—Remote controls
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04M—TELEPHONIC COMMUNICATION
    • H04M1/00—Substation equipment, e.g. for use by subscribers
    • H04M1/72—Mobile telephones; Cordless telephones, i.e. devices for establishing wireless links to base stations without route selection
    • H04M1/724—User interfaces specially adapted for cordless or mobile telephones
    • H04M1/72403—User interfaces specially adapted for cordless or mobile telephones with means for local support of applications that increase the functionality
    • H04M1/7243—User interfaces specially adapted for cordless or mobile telephones with means for local support of applications that increase the functionality with interactive means for internal management of messages

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Signal Processing (AREA)
  • Toys (AREA)
  • Mobile Radio Communication Systems (AREA)
  • Instructional Devices (AREA)
  • Fittings On The Vehicle Exterior For Carrying Loads, And Devices For Holding Or Mounting Articles (AREA)

Abstract

本发明描述了一种微型设备，其可以例如与蜂窝式电话相关联，该微型设备设置有至少四个利用压缩流体或者通过环形电马达来致动的微型转子。

Description

微型设备和装备有微型设备的蜂窝式电话
技术领域
本发明涉及一种微型设备(microaircraft)，其包括基本上平的本体，该本体具有至少四个基本上共面的并且布置在四边形的顶点上的环形微型转子，用于控制所述微型转子的马达装置，以及用于控制所述马达装置的电子微型控制器。
发明内容
在优选的实施例中，所述微型转子是压缩空气涡轮，并且所述马达装置包括用于毫微粒子的燃料的微型燃烧室和与每个微型涡轮相关联的一个或多个喷嘴，用于将微型燃烧室内部产生的一个或多个震动波前引导至微型涡轮上。
具体而言，本发明提供一种微型设备，其包括本体，该本体具有至少四个基本上共面的并且布置在四边形的顶点上的环形微型转子，用于控制所述微型转子的马达装置，以及用于控制所述马达装置的电子微型控制器，其特征在于，所述微型设备以可拆卸的方式连接到一蜂窝式电话的本体，所述电话设置有用于遥控所述微型设备的装置。
在另一种实施例中，马达装置包括用于每个微型马达的环形电马达，每个微型转子构成相应的电马达的转子。
本发明还涉及一种蜂窝式电话，上述微型设备以可拆卸的方式连接到该蜂窝式电话上。该蜂窝式电话装备有用于遥控微型设备的装置。优选地，微型设备设置有多媒体装置，例如小型相机和麦克风，因此可以将音频和视频消息传送到客户移动电话，或者也可以传送到其他的蜂窝式系统和因特网。
微型设备的四个微型转子的控制装置被设计成相互独立地或者成对地控制着所述微型转子。优选地，微型设备的控制方式是：在布置于四边形的两个相对顶点上的两个环形微型涡轮上产生顺时针的转动，并且在其他两个微型涡轮上产生逆时针的转动。设备具有四个自由度。通过同步地或异步地改变微型涡轮的速度，可以获得垂直运动、侧向运动、水平运动或者绕偏航轴线的转动。
通过同时增大或减小所有四个微型涡轮的动力来控制垂直运动。通过在四边形的同一侧上将两个涡轮的动力相对于其他两个涡轮增大来控制侧向运动。例如，通过在左侧增大涡轮的速度，设备朝向右侧移动。以相同的方式，两个后面或前面的涡轮的动力增大分别导致了向前和向后的运动。通过转子电阻产生的感应力矩来控制第四个自由度。这个力矩沿着与转子转动相反的方向作用。为了消除设备偏航，所有感应的力矩的和应该是零。然而，如果布置在四边形的顶点上的一组转子增大其转速，例如顺时针旋转的那些转子，那么所得到的感应力矩将产生设备的逆时针转动。
在利用电马达获得推进的特定情况下，在一个优选的实施例中，微型设备使用商业上可以得到的薄膜电池或者微型燃料电池。
附图说明
从下面参照附图仅作为非限制性实例提供的说明来看，本发明的其他特征和优点将很清楚，其中
图1是根据本发明的蜂窝式电话-微型设备的组件的透视前视图，其处于分解状态；
图2是图1的组件的透视后视图；
图3是属于图1、2的组件的微型设备的放大的局部剖视透视图；
图3A表示了一种变型；
图4是表示了用于微型设备的四个微型转子上的控制标准；
图5、6是每个微型转子的可能的实施例的透视图；以及
图7是根据本发明的微型设备的控制系统的方块图。
具体实施方式
参照图1、2，数字1总体表示设置有用于可拆卸地连接微型设备2的装置的微型蜂窝式电话。在模拟式的TACS一代和数字式的GSM一代之后，第三代蜂窝式电话可以达到高达每秒2兆位的传输速率，即，比GSM系统的限制大了200倍，因此可以进行高清晰度的音频和视频传输。作为全球移动通讯标准的所述标准的成功使得可以进行世界范围的虚拟连接。如图3中所示，微型设备2包括大致平的本体3，其具有布置在四边形的顶点处的四个微型转子4，基本上彼此共面。通过阀6进行供给的压缩气体(或空气)箱5A限定在本体3的内部。每个微型转子4与连接于微型燃烧室8的一个或多个喷嘴7相关联，在该微型燃烧室8中，毫微粒子的燃料产生了微燃烧，产生一个或多个震动波前来控制每个微型转子。喷嘴7可以布置在置于两个相邻的涡轮之间的同一微型燃烧室的两个相对端部上(图3A)，以便控制两个涡轮。用于获得脉冲喷射的系统可以是“无阀式的”或者“爆震式的”。每个微型涡轮的转子可以是“磁提升式的(magnetic lift)”。
在图4中，微型转子4简称为AS(左前方)、AD(右前方)、PS(左后方)和PD(右后方)。两个转子对AS、PD以及AD、PS沿着相反的方向转动，如图4中所示，以便确保偏航力矩的相互抵消。如以上所述，垂直、侧向、水平运动和偏航转动通过四个微型转子的转速的选择性控制来实现。
图5、6是每个微型转子4的两个可能的实施例的透视图。
根据另一个实施例，每个转子4是布置在环形电马达的环形定子内部的转子。
微型设备的本体3装纳着电子微型控制器5，该电子微型控制器5在相距某一距离处与蜂窝式电话1通讯。多媒体装置进一步设置在微型设备上，例如小型相机、麦克风或者各种传感器，这些多媒体装置将音频和视频消息传送到客户移动电话或其他蜂窝式系统或者因特网。
图7示出了控制系统的结构，其中可以识别出两个主要元件，即，微型设备2和基站。微型设备2包括四个微型转子4，它们的控制马达7A通过微控制器5利用电子速度控制器8A来控制。微控制器5通过传感器20和GPS天线21以射频与移动电话或者因特网站通讯，它发送控制数据，而设备传送音频-视频数据。通过视频传送器23和天线24与视频基础接收器26的天线25相连的一个或多个小型相机22实现了所述结果。小型相机(CCD或者CMOS)也被设计为用于自我运动的动态影像传感器。控制信号通过控制站27或者通过移动电话利用R/C传送器28和传送天线29来发送，以便利用天线30通过数据接收器31来接收，数据接收器31接收电力线32并且在四通道线路33上将数据传送至微控制器5。微型设备最后与电池组件34相关联。
微控制器5是微型设备的核心。它从机载传感器接收输入信号并且从相机接收视频信息，并且发送用于微型涡轮转子的电子(毫微粒子)速度控制器的输出信号。如已经所述的，在相对于压缩空气马达的另一种形式中，所述马达可以是环形电马达。无论如何，本发明的优选的特征是使用利用微燃烧增压的压缩空气涡轮转子。
涡轮转子和环形电马达的自增压(self-charge)功能可以通过风能提供。
如已经所述的，可以使用薄膜电池或者微型燃料电池。
明显地，尽管本发明的基本理念保持相同，但是结构细节和实施例可以相对于已经通过实例描述和表示的内容来广泛地变化，而不会背离本发明的框架。

Claims (11)

1.一种微型设备，其包括本体，该本体具有至少四个基本上共面的并且布置在四边形的顶点上的环形微型转子(4)，用于控制所述微型转子的马达装置，以及用于控制所述马达装置的电子微型控制器(5)，其特征在于，所述微型设备以可拆卸的方式连接到一蜂窝式电话的本体，所述电话设置有用于遥控所述微型设备的装置。
2.根据权利要求1所述的微型设备，其特征在于，所述微型转子(4)是气体涡轮，并且所述马达装置包括用于毫微粒子的燃料的微型燃烧室(8)和与每个微型涡轮相关联的一个或多个喷嘴(7)，用于将微型燃烧室(8)内部产生的一个或多个震动波前引导至微型涡轮上。
3.根据权利要求1所述的微型设备，其特征在于，马达装置包括用于每个微型转子(4)的环形电马达，每个微型转子是相应的电马达的转子。
4.根据权利要求1所述的微型设备，其特征在于，微型转子(4)是磁提升式的。
5.根据权利要求1所述的微型设备，其特征在于，微型设备设置有多媒体装置，因此可以将音频和视频消息传送到客户移动电话，或者也可以传送到其他的蜂窝式系统和因特网。
6.根据权利要求5所述的微型设备，其特征在于，微型设备的四个微型转子的控制装置被设计成相互独立地控制着所述微型转子。
7.根据权利要求6所述的微型设备，其特征在于，微型设备的控制方式是：在布置于四边形的两个相对顶点上的两个环形微型转子上产生顺时针的转动，并且在其他两个微型转子上产生逆时针的转动。
8.根据权利要求7所述的微型设备，其特征在于，其设置有用于同步地或异步地改变微型涡轮的速度以获得垂直运动、侧向运动、水平运动或者绕偏航轴线的转动的控制装置，通过同时增大或减小所有四个微型涡轮的动力来控制所述垂直运动，通过在四边形的同一侧上将两个涡轮的动力相对于其他两个涡轮增大来控制侧向和前/后运动，并且通过将沿一个方向旋转的转子相对于沿其他方向旋转的转子以不同的速度转动来控制偏航力矩。
9.根据权利要求5所述的微型设备，其特征在于，微型设备使用薄膜电池或者微型燃料电池。
10.根据权利要求5所述的微型设备，其特征在于，微型设备使用小型相机，该小型相机也被设计为自我运动的动态影像传感器。
11.根据权利要求5所述的微型设备，其特征在于，微型设备包括利用风能的马达自增压装置。
CN2004100857641A 2003-10-17 2004-10-18 微型设备和装备有微型设备的蜂窝式电话 Expired - Fee Related CN1610267B (zh)

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DE602004001649D1 (de) 2006-09-07
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