公开(公告)号：USD635083S1

公开(公告)日：2011-03-29

申请号：US29325966

申请日：2008-10-09

Applicant: James D. DeLaurier

Designer： James D. DeLaurier

公开(公告)号：US5288039A

公开(公告)日：1994-02-22

申请号：US921220

申请日：1992-07-29

Applicant: James D. DeLaurier ,  Jeremy M. Harris

Inventor： James D. DeLaurier ,  Jeremy M. Harris

IPC: B64C3/52 ,  B64C33/02 ,  B64C3/44

CPC classification number: B64C3/52 ,  B64C33/02 ,  Y02T50/145

Abstract: A closed shear flexible panel has upper and lower surfaces each having front ends which define a leading edge and rear edges which define a trailing edge. The rear edges are slideable longitudinally with respect to each other when a torsional force is applied to the panel or a linear force is applied to the rear edges to induce a spanwise gradient pitch in the panel.

Abstract translation: 封闭剪切柔性板具有上表面和下表面，每个前表面具有限定前缘的前端和限定后缘的后边缘。 当扭转力施加到面板上时，后边缘可相对于彼此纵向滑动，或者线性力施加到后边缘以在面板中引导翼展渐变间距。

公开(公告)号：US20100270424A1

公开(公告)日：2010-10-28

申请号：US12429542

申请日：2009-04-24

Applicant: James D. DeLaurier

Inventor： James D. DeLaurier

IPC: B64B1/20 ,  G09F21/08 ,  B64B1/12

CPC classification number: B64B1/06 ,  B64B1/14 ,  B64B1/20 ,  B64B1/30 ,  B64B2201/00 ,  B64C2201/00 ,  G09F21/08 ,  G09F21/10

Abstract: A hybrid airship comprises a non-rigid body having a delta-wing shape and an airfoil cross-section. The body is shaped for generating aerodynamic lift during forward flight, and contains a gas for generating buoyancy lift. At least one splitter plate is pivotally connected along a trailing edge of the body. The splitter plate is configured to be controllably pivoted for controlling the airship.

Abstract translation: 混合式飞艇包括具有三角翼形状和翼型横截面的非刚性体。 身体形状适合在向前飞行期间产生空气动力升力，并且包含产生浮力升力的气体。 至少一个分离板沿主体的后缘枢转地连接。 分离板构造成可控地枢转以控制飞艇。

公开(公告)号：US4955562A

公开(公告)日：1990-09-11

申请号：US272015

申请日：1988-11-16

Applicant: John E. Martin ,  James D. DeLaurier ,  George W. Jull ,  Arne Lillemark

Inventor： John E. Martin ,  James D. DeLaurier ,  George W. Jull ,  Arne Lillemark

IPC: A63H29/22 ,  B64C39/02 ,  B64C39/12 ,  B64D27/24

CPC classification number: B64C39/12 ,  B64C39/024 ,  B64D27/24 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/104 ,  Y02T50/62

Abstract: A microwave-powered aircraft has lifting surfaces for exerting lifting forces on the aircraft in response to the propulsion of the aircraft and a rectenna array for receiving and rectifying microwave energy transmitted to the aircraft from a location remote from the aircraft. An electric motor for driving a propeller is energized by microwave energy received by the rectenna array, which is provided in a body at the underside of the aircraft. The body has its major dimensions extending horizontally and is relatively shallow with a periphery which is vertically curved so as to reduce turbulence in the airstream over the body during flight. The body is separate from the lifting surfaces and shaped to at least substantially avoid the generation of lifting forces by the body.

Abstract translation: 一种微波动力飞机已升力面，用于响应于所述飞行器的推进和用于接收和整流从来自飞行器的位置远程传输到飞机微波能量整流天线阵列的飞机上施加升力。 用于驱动螺旋桨的电动机由通过设置在飞行器下侧的主体中的整流天线阵列接收的微波能量来激励。 该主体具有其主要尺寸水平延伸，并且与该被垂直弯曲的，以便在飞行期间，以减少气流在身体湍流周边相对较浅。 身体与提升表面分离并成形为至少基本上避免了身体产生提升力。