公开(公告)号：US07665688B2

公开(公告)日：2010-02-23

申请号：US11691971

申请日：2007-03-27

Applicant: David A Cylinder ,  James C Kellogg

Inventor： David A Cylinder ,  James C Kellogg

IPC: B64C27/24 ,  B64C27/28

CPC classification number: B64C27/24 ,  B64C27/28 ,  B64C39/024 ,  B64C39/12 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/108

Abstract: A micro aerial vehicle can be converted during flight between a fixed wing flight mode and a rotary wing flight mode. The canard design micro aerial vehicle includes a fuselage, two tiltable propellers and airfoils arranged at a forward portion of fuselage, a pair of coaxial drive shafts positioned aft of the tiltable propeller and airfoil arranged for contra-rotation, a stop rotor mechanism, and a pair of wing panels, each of the wing panels attached to one of the coaxial drive shafts. The wing panels act as contra-rotating rotor blades in the rotary wing flight mode, and act as fixed wing panels in the fixed wing mode.

Abstract translation: 微型飞行器可以在固定翼飞行模式和旋翼飞行模式之间的飞行过程中转换。 鸭子设计的微型飞行器包括机身，两个可倾斜的螺旋桨和机身，其布置在机身的前部，一对同轴驱动轴，位于可倾斜推进器和翼型的后方，布置成用于反向转动，止动转子机构和 一对翼板，每个翼片连接到同轴驱动轴之一。 翼板作为旋转翼飞行模式中的反转叶片，以固定翼模式作为固定翼板。

公开(公告)号：US20090014599A1

公开(公告)日：2009-01-15

申请号：US11691971

申请日：2007-03-27

Applicant: David A Cylinder ,  James C. Kellogg

Inventor： David A Cylinder ,  James C. Kellogg

IPC: B64C27/22

CPC classification number: B64C27/24 ,  B64C27/28 ,  B64C39/024 ,  B64C39/12 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/108

Abstract: A micro aerial vehicle can be converted during flight between a fixed wing flight mode and a rotary wing flight mode. The canard design micro aerial vehicle includes a fuselage, two tiltable propellers and airfoils arranged at a forward portion of fuselage, a pair of coaxial drive shafts positioned aft of the tiltable propeller and airfoil arranged for contra-rotation, a stop rotor mechanism, and a pair of wing panels, each of the wing panels attached to one of the coaxial drive shafts. The wing panels act as contra-rotating rotor blades in the rotary wing flight mode, and act as fixed wing panels in the fixed wing mode.

Abstract translation: 微型飞行器可以在固定翼飞行模式和旋翼飞行模式之间的飞行过程中转换。 鸭子设计的微型飞行器包括机身，两个可倾斜的螺旋桨和机身，其布置在机身的前部，一对同轴驱动轴，位于可倾斜推进器和翼型的后方，布置成用于反向转动，止动转子机构和 一对翼板，每个翼片连接到同轴驱动轴之一。 翼板作为旋转翼飞行模式中的反转叶片，以固定翼模式作为固定翼板。

公开(公告)号：US06959895B2

公开(公告)日：2005-11-01

申请号：US10774653

申请日：2004-02-04

Applicant: David A. Cylinder

Inventor： David A. Cylinder

IPC: B64C33/02 ,  B64C39/02 ,  B64C39/08

CPC classification number: B64C39/08 ,  B64C33/02 ,  B64C39/024 ,  B64C2201/025 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/126 ,  B64C2201/141 ,  B64C2201/146

Abstract: A vehicle for flying and having a forward portion and a rearward portion opposite the forward. The vehicle includes a first pair of wings arranged at the forward portion of the vehicle, a second pair of wings arranged at the rearward portion of the vehicle, and a support structure. The support structure is connected to the forward pair of wings and connected to the rearward pair of wings, the support structure being arranged to drive the forward pair of wings alternately toward each other and apart and drives the second pair of wings alternately toward each other and apart.

公开(公告)号：US08040443B2

公开(公告)日：2011-10-18

申请号：US13049503

申请日：2011-03-16

Applicant: Christopher M Spillmann ,  David A Cylinder ,  Banahalli R Ratna ,  Jawad Naciri ,  Brett D. Martin

Inventor： Christopher M Spillmann ,  David A Cylinder ,  Banahalli R Ratna ,  Jawad Naciri ,  Brett D. Martin

IPC: G02F1/133

CPC classification number: F03G7/06 ,  Y10T29/49826

Abstract: A method comprising arranging a first heating element on a first liquid crystal elastomer, arranging a first layer of thermal paste on the first heating element, and arranging a second liquid crystal elastomer on the first layer of thermal paste.

Abstract translation: 一种方法，包括在第一液晶弹性体上布置第一加热元件，在第一加热元件上布置第一层热膏，并在第一层热浆上设置第二液晶弹性体。