JPS6483450A - Water surface plane - Google Patents

Water surface plane

Info

Publication number
JPS6483450A
JPS6483450A JP24188987A JP24188987A JPS6483450A JP S6483450 A JPS6483450 A JP S6483450A JP 24188987 A JP24188987 A JP 24188987A JP 24188987 A JP24188987 A JP 24188987A JP S6483450 A JPS6483450 A JP S6483450A
Authority
JP
Japan
Prior art keywords
trunk
stretched
blade
blades
movable frames
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.)
Granted
Application number
JP24188987A
Other languages
Japanese (ja)
Other versions
JPH0433660B2 (en
Inventor
Shigenori Ando
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.)
Meitec Group Holdings Inc
Original Assignee
Meitec Corp
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 Meitec Corp filed Critical Meitec Corp
Priority to JP24188987A priority Critical patent/JPS6483450A/en
Publication of JPS6483450A publication Critical patent/JPS6483450A/en
Publication of JPH0433660B2 publication Critical patent/JPH0433660B2/ja
Granted legal-status Critical Current

Links

Abstract

PURPOSE:To make it possible to increase the area of blades freely to improve lift at the time of a low speed for a plane of a type which can fly by use of a ground effect by providing a flap at least on one side of the front or back of a main blade to be possible to be stretched. CONSTITUTION:This water surface plane has a center trunk 1 with a turbo fan 2 for propulsion installed at a position at the top on the rear side, and has front blades 3 provided with a pair of right and left tilt type propellers 4 disposed in the front part of the center trunk 1. Main blades 5 are provided in the middle part of the center trunk 1, and each main blade 5 is separated to an inner blade part 5a and an outer blade part 5b at a boundary of a side trunk 6 acting as an auxiliary float. Movable frames 7, 7 are provided connected with each drive mechanism at the front and back edges of the inner blade part 5a, and canvas 9 stored in the side trunk 6 is stretched between the movable frames 7, 7 when the movable frames 7, 7 are stretched, so the area of the blade is increased.
JP24188987A 1987-09-25 1987-09-25 Water surface plane Granted JPS6483450A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP24188987A JPS6483450A (en) 1987-09-25 1987-09-25 Water surface plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP24188987A JPS6483450A (en) 1987-09-25 1987-09-25 Water surface plane

Publications (2)

Publication Number Publication Date
JPS6483450A true JPS6483450A (en) 1989-03-29
JPH0433660B2 JPH0433660B2 (en) 1992-06-03

Family

ID=17081055

Family Applications (1)

Application Number Title Priority Date Filing Date
JP24188987A Granted JPS6483450A (en) 1987-09-25 1987-09-25 Water surface plane

Country Status (1)

Country Link
JP (1) JPS6483450A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5520260A (en) * 1992-06-17 1996-05-28 Stiegler; Hartmut Steering gear for a hovercraft
US5860620A (en) * 1996-07-10 1999-01-19 Northrup Grumman Corporation Ram wing vehicle
JP2014506545A (en) * 2011-02-25 2014-03-17 エアバス オペラシオン ソシエテ パ アクシオンス シンプリフィエ Aircraft with reduced environmental impact

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5520260A (en) * 1992-06-17 1996-05-28 Stiegler; Hartmut Steering gear for a hovercraft
US5860620A (en) * 1996-07-10 1999-01-19 Northrup Grumman Corporation Ram wing vehicle
JP2014506545A (en) * 2011-02-25 2014-03-17 エアバス オペラシオン ソシエテ パ アクシオンス シンプリフィエ Aircraft with reduced environmental impact

Also Published As

Publication number Publication date
JPH0433660B2 (en) 1992-06-03

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