JPS5539824A - Directional control device of hovercraft - Google Patents

Directional control device of hovercraft

Info

Publication number
JPS5539824A
JPS5539824A JP11151678A JP11151678A JPS5539824A JP S5539824 A JPS5539824 A JP S5539824A JP 11151678 A JP11151678 A JP 11151678A JP 11151678 A JP11151678 A JP 11151678A JP S5539824 A JPS5539824 A JP S5539824A
Authority
JP
Japan
Prior art keywords
hovercraft
chamber
compressed air
directional control
rudders
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
Application number
JP11151678A
Other languages
Japanese (ja)
Inventor
Yoshihiro Sakata
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to JP11151678A priority Critical patent/JPS5539824A/en
Publication of JPS5539824A publication Critical patent/JPS5539824A/en
Pending legal-status Critical Current

Links

Landscapes

  • Excavating Of Shafts Or Tunnels (AREA)

Abstract

PURPOSE: To reduce the turning radius of a hovercraft at the time of changing its direction and greatly improve its maneuverability, by exhausting compressed air from both broadsides of the fore body.
CONSTITUTION: The chamber of the hovercraft is divided into two parts 2A, 2B by hanging a skirt 5A from a partition board 8 at the beam center in the chamber. For changing the direction leftward, rudders 7, 7 are controlled and a control valve 12 is opened to exhaust part of compressed air in the chamber 2B from an opening 10b through an air injection pipe 10. This injection of compressed air provides the hull with a directional control force leftward in addition to the turning force by the rudders 7 for producing a quick turn.
COPYRIGHT: (C)1980,JPO&Japio
JP11151678A 1978-09-11 1978-09-11 Directional control device of hovercraft Pending JPS5539824A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP11151678A JPS5539824A (en) 1978-09-11 1978-09-11 Directional control device of hovercraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP11151678A JPS5539824A (en) 1978-09-11 1978-09-11 Directional control device of hovercraft

Publications (1)

Publication Number Publication Date
JPS5539824A true JPS5539824A (en) 1980-03-21

Family

ID=14563287

Family Applications (1)

Application Number Title Priority Date Filing Date
JP11151678A Pending JPS5539824A (en) 1978-09-11 1978-09-11 Directional control device of hovercraft

Country Status (1)

Country Link
JP (1) JPS5539824A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4971869A (en) * 1989-06-19 1990-11-20 Polaroid Corporation Color encoding photographic film
US5307893A (en) * 1993-01-15 1994-05-03 Textron, Inc. Air cushion vehicle having volute side thrusters
JPH0660594U (en) * 1986-07-31 1994-08-23 ソラリ，フランコ Propulsion system for a ship driven by drawing an air jet into a pair of longitudinal lateral channels in the lower hull

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0660594U (en) * 1986-07-31 1994-08-23 ソラリ，フランコ Propulsion system for a ship driven by drawing an air jet into a pair of longitudinal lateral channels in the lower hull
US4971869A (en) * 1989-06-19 1990-11-20 Polaroid Corporation Color encoding photographic film
US5307893A (en) * 1993-01-15 1994-05-03 Textron, Inc. Air cushion vehicle having volute side thrusters

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