公开(公告)号：WO2010121384A1

公开(公告)日：2010-10-28

申请号：PCT/CA2010/000631

申请日：2010-04-23

Applicant: SOLARSHIP ,  DELAURIER, James D.

Inventor： DELAURIER, James D.

IPC: B64B1/02 ,  B64C13/50 ,  B64C31/00

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。 身体形状适合在前进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。