JPS61142667U - - Google Patents

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Publication number
JPS61142667U
JPS61142667U JP2701085U JP2701085U JPS61142667U JP S61142667 U JPS61142667 U JP S61142667U JP 2701085 U JP2701085 U JP 2701085U JP 2701085 U JP2701085 U JP 2701085U JP S61142667 U JPS61142667 U JP S61142667U
Authority
JP
Japan
Prior art keywords
hovercraft
hull
gravity
balance
points
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
JP2701085U
Other languages
Japanese (ja)
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 filed Critical
Priority to JP2701085U priority Critical patent/JPS61142667U/ja
Publication of JPS61142667U publication Critical patent/JPS61142667U/ja
Pending legal-status Critical Current

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Description

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は、本考案の一実施例を示す斜視図、第
2図は、同平面図である。何れも本体部分と翼部
分とでは縮尺が異なつている。 1はホーバークラフトの船体、2は支柱、3は
スクエアパラシユート、4は支持ロープ、5は座
席、6はスクコアパラシユートの打ち出し装置、
7はコントロールワイヤー、8はコントロールペ
ダル、9はハンドル、10は浮上用エンジン、1
1はスカート、12は推進用エンジン、13はダ
クト、14は推進用フアン、15はラダー。
FIG. 1 is a perspective view showing an embodiment of the present invention, and FIG. 2 is a plan view thereof. In both cases, the scale of the main body portion and the wing portion is different. 1 is the hull of the hovercraft, 2 is the support, 3 is the square parachute, 4 is the support rope, 5 is the seat, 6 is the launching device for the squoa parachute,
7 is a control wire, 8 is a control pedal, 9 is a handle, 10 is a levitation engine, 1
1 is a skirt, 12 is a propulsion engine, 13 is a duct, 14 is a propulsion fan, and 15 is a rudder.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] ホーバークラフトの船体の重心位置の少なくて
も3点に、スクエアパラシユートの多数の支持ロ
ープを、バランスするように、適宜分割して接続
した、空飛ぶホーバークラフト。
A flying hovercraft in which a large number of supporting ropes of a square parachute are divided and connected as appropriate to balance them at at least three points on the center of gravity of the hovercraft's hull.
JP2701085U 1985-02-26 1985-02-26 Pending JPS61142667U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2701085U JPS61142667U (en) 1985-02-26 1985-02-26

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2701085U JPS61142667U (en) 1985-02-26 1985-02-26

Publications (1)

Publication Number Publication Date
JPS61142667U true JPS61142667U (en) 1986-09-03

Family

ID=30523564

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2701085U Pending JPS61142667U (en) 1985-02-26 1985-02-26

Country Status (1)

Country Link
JP (1) JPS61142667U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109398695A (en) * 2018-12-13 2019-03-01 安徽科技学院 A kind of adjustable leading edge gas chamber automatic forming ram air parachute of established angle

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109398695A (en) * 2018-12-13 2019-03-01 安徽科技学院 A kind of adjustable leading edge gas chamber automatic forming ram air parachute of established angle

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