Title:
INTEGRATED SPLINE/CONTROL SEAT SUB-ASSEMBLY FOR UNMANNED AIRCRAFT
Document Type and Number:
Japanese Patent JP2001026296
Kind Code:
A
Abstract:
To provide a rotor type unmanned aircraft which can be utilized for wide-range reconnaissance aviation, or communication mission and especially for tactical reconnaissance aviation.
An unmanned aircraft UAV has a composite annular fuselage structure 20 surrounding a rotary assembly 100 including a pair of co-axial multi-blade double reversing rotors. The annular fuselage structure 20 includes an annular C-type structure, and the annular C-type structure regulates a cavity and a freely removable panel structure fitted in combination with the annular C-type structure. The UAV has a drive train assembly including a sprag clutch, an engine connection sub-assembly, a transmission connection sub-assembly and a drive shaft.
Inventors:
CYCON JAMES P
HUNTER DAVID H
KOHLHEPP FRED W
KRAUSS TIMOTHY A
MILLEA VINCENT F
FAANZU KENNETH M
FARRELL MARVIN D
SANDY DAVID F
BEATTY ROBERT D
HANSEN BRUCE D
HUNTER DAVID H
KOHLHEPP FRED W
KRAUSS TIMOTHY A
MILLEA VINCENT F
FAANZU KENNETH M
FARRELL MARVIN D
SANDY DAVID F
BEATTY ROBERT D
HANSEN BRUCE D
Application Number:
JP2000182395A
Publication Date:
January 30, 2001
Filing Date:
June 18, 1993
Export Citation:
Assignee:
UNITED TECHNOLOGIES CORP
International Classes:
B64C27/10; B64C27/12; B64C27/14; B64C27/20; B64C27/33; B64C27/46; B64C27/473; B64C27/605; B64C29/00; B64C39/02; B64C39/06; F16C11/06; F16D1/02; F16D1/05; F16D1/06; F16D3/06; F16D3/18; F16D41/07; F16F15/10; F16H1/14; F16H1/22; F02B75/02; (IPC1-7): B64C27/10; B64C27/12; B64C27/20; B64C39/06; F16D1/06
Domestic Patent References:
| JPH04231290A | 1992-08-20 | |||
| JPH0367799A | 1991-03-22 | |||
| JPS63227497A | 1988-09-21 | |||
| JPH06509770A | 1994-11-02 |
Attorney, Agent or Firm:
Fujiya Shiga (2 outside)