JPS5440499A - Method of restoring unmanned aircraft - Google Patents
Method of restoring unmanned aircraftInfo
- Publication number
- JPS5440499A JPS5440499A JP10539177A JP10539177A JPS5440499A JP S5440499 A JPS5440499 A JP S5440499A JP 10539177 A JP10539177 A JP 10539177A JP 10539177 A JP10539177 A JP 10539177A JP S5440499 A JPS5440499 A JP S5440499A
- Authority
- JP
- Japan
- Prior art keywords
- aircraft
- axis
- opened
- parachute
- vertical flight
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Landscapes
- Toys (AREA)
Abstract
PURPOSE: To restore unmanned VTOL aircraft with ease, by switching the flight condition of acircraft from horizontal to vertical while the arifraft is descending slowly with its parachute being opened, and landing the aircraft at the fixed point on the ground or on the board of a ship.
CONSTITUTION: Exhaust nozzle 5 used for vertical flight of VTOL aircraft is equipped with control vanes 10, 11 and 12, 13 which are turned respectively about axis X' -X' parallel to the longitudinal axis X-X of the body of aircraft and axis Y'- Y' parallee to the lateral axis Y-Y of the aircraft, so as to compensate rolling, pitching and yawing of the aircraft body during vertical flight of the aircraft. A drag parachute 14 is stored in cylindrical rear end of aircraft body 1. The cylindrical portion 15 is separated from the aircraft body 1 a certain time after the dragparachute 14 is opened, and main parachute 17 is drawn out and opened, whereby the aircraft 1 is allowed to descend with its body being kept in landing position. In this while, guide vanes 6, 7 are turned to their vertical flight condition, and the aircraft 1 is enabled to land on the ground or on a ship smoothly while increasing the thrust (propulsive force) of engine 2.
COPYRIGHT: (C)1979,JPO&Japio
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP10539177A JPS5440499A (en) | 1977-09-03 | 1977-09-03 | Method of restoring unmanned aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP10539177A JPS5440499A (en) | 1977-09-03 | 1977-09-03 | Method of restoring unmanned aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS5440499A true JPS5440499A (en) | 1979-03-29 |
Family
ID=14406334
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP10539177A Pending JPS5440499A (en) | 1977-09-03 | 1977-09-03 | Method of restoring unmanned aircraft |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5440499A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6195774A (en) * | 1984-10-17 | 1986-05-14 | Kobe Steel Ltd | Output control method of welding power source |
JPS63298000A (en) * | 1987-05-28 | 1988-12-05 | 三菱電機株式会社 | Missile |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3980259A (en) * | 1974-04-03 | 1976-09-14 | British Aircraft Corporation Limited | Aircraft recovery methods |
-
1977
- 1977-09-03 JP JP10539177A patent/JPS5440499A/en active Pending
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3980259A (en) * | 1974-04-03 | 1976-09-14 | British Aircraft Corporation Limited | Aircraft recovery methods |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6195774A (en) * | 1984-10-17 | 1986-05-14 | Kobe Steel Ltd | Output control method of welding power source |
JPH0446672B2 (en) * | 1984-10-17 | 1992-07-30 | Kobe Steel Ltd | |
JPS63298000A (en) * | 1987-05-28 | 1988-12-05 | 三菱電機株式会社 | Missile |
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