Title:
【発明の名称】ホーバクラフト操舵装置
Document Type and Number:
Japanese Patent JPH07507518
Kind Code:
A
Abstract:
PCT No. PCT/DE93/00529 Sec. 371 Date Dec. 16, 1994 Sec. 102(e) Date Dec. 16, 1994 PCT Filed Jun. 16, 1993 PCT Pub. No. WO93/25422 PCT Pub. Date Dec. 23, 1993.A steering device for a hovercraft having two driving engines (2, 3), a back skirt (5), a finger skirt (6) and a jet deflection device located downstream of the two driving engines (2, 3). The jet deflection device includes a negative Vee stream deflector (7) and rudder elements (11, 12) which can be operated in opposite directions. The Vee stream deflector (7) is arranged behind the driving engines (2, 3) in such a way that each driving engine (2, 3) is assigned a portion of the Vee stream deflector (7) having the rudder element (11; 12). The rudder elements (11; 12) run diagonally through an axis of symmetry of the respective driving engine (2, 3). The Vee stream deflector (7) further includes a middle section which acts as a stabilizing nose (8).
Inventors:
Bloom, albert
Schutteigler, Hartmut
Schutteigler, Hartmut
Application Number:
JP50103794A
Publication Date:
August 24, 1995
Filing Date:
June 16, 1993
Export Citation:
Assignee:
ABES Aircraft Actien Gezershaft
International Classes:
B60V1/11; B60V1/14; B60V1/16; (IPC1-7): B60V1/11; B60V1/14; B60V1/16
Attorney, Agent or Firm:
Kazuho Kawarada