JPS62227896A - Departure and arrival performance improving auxiliary equipment for boat seaplane - Google Patents

Departure and arrival performance improving auxiliary equipment for boat seaplane

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Publication number
JPS62227896A
JPS62227896A JP7193486A JP7193486A JPS62227896A JP S62227896 A JPS62227896 A JP S62227896A JP 7193486 A JP7193486 A JP 7193486A JP 7193486 A JP7193486 A JP 7193486A JP S62227896 A JPS62227896 A JP S62227896A
Authority
JP
Japan
Prior art keywords
flying
water
flying boat
boat
mooring
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
JP7193486A
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Japanese (ja)
Inventor
小沢 甚一郎
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Individual
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Individual
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Application filed by Individual filed Critical Individual
Priority to JP7193486A priority Critical patent/JPS62227896A/en
Publication of JPS62227896A publication Critical patent/JPS62227896A/en
Pending legal-status Critical Current

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Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 イ2発明の目的 (産業上の利用分野) 本発明は飛行艇の離着水・水上航行・接岸操舵係留等に
必要な飛行艇の発着性能改善装置にかかわりλ特に離着
水性能改善用水中翼の構造と1離水を容易ならしめるた
めの気泡発生装置\水上航行時の航空燃料を節約すると
共に接岸時の操舵を容易なら1〜めるための飛行艇用水
中推進装置\飛行艇の係留を容易ならしめるための吸着
盤係留装置1人や荷物の積み降ろしを容易ならしめる飛
行艇用接岸岩壁及びジェット飛行艇の鳥害防止装置に関
する。
Detailed Description of the Invention A2 Objective of the Invention (Field of Industrial Application) The present invention relates to a device for improving the take-off and landing performance of an air boat, which is necessary for take-off and landing on water, navigation on water, berth steering, mooring, etc. Hydrofoil structure for improving take-off and landing performance and 1. Bubble generator to make take-off easier \ Submersible for flying boats to save aviation fuel when navigating on water and to make it easier to steer when docking Propulsion device / Suction cup mooring device for facilitating the mooring of an airship.Regarding a rock wall for docking an airship to facilitate the loading and unloading of one person and cargo, and a bird damage prevention device for a jet flying boat.

(従来の技術) 従来1飛行艇はペイロード(有効荷重効率)が悪いとの
基本観念のもとに)飛行艇による犬BE ?J’C空輸
送全輸送的に実施しようなどという計画は殆んどなされ
なかった。それでも海上自衛隊等で;佳対潜哨戒1海難
救助等の必要性から・荒天時のイ上離着水を可能ならし
めるような研究開発がなされてきた。しかしその研究開
発は専ら従来の飛行艇の基本形態を基として・飛行艇胴
体の接水底面の舟底形艇体を鋭角のV字状にして離水性
能を改善したり)主翼フラップを改良して垂直上昇力の
向上を図るなどの改良がなされてきた。飛行艇胴体接水
底面に1〜2段の「水切り」と称する段落を設けること
は昔からなされてきた技術である。
(Prior art) Conventional 1 Based on the basic idea that flying boats have poor payload (effective load efficiency)) dog BE using flying boats? There were almost no plans to implement all J'C air transportation. Nevertheless, the Japan Maritime Self-Defense Force and others have been conducting research and development to make it possible to take off and land on water in rough weather due to the necessity of maritime rescue. However, this research and development was based exclusively on the basic form of conventional flying boats (such as making the bottom of the water-contact boat-shaped hull of the flying boat body into an acute V-shape to improve water takeoff performance) and improving the main wing flaps. Improvements have been made to improve the vertical lift. It is a technology that has been used for a long time to provide one or two stages called "water drainers" on the bottom surface of an airship's fuselage that is in contact with the water.

従来り飛行艇の水上航行はA専ら飛行用エンジン推進力
を利用して航行しており為水上航行時の操舵は垂直尾翼
方向舵を主用し1水中舵を併用することもあったが入水
中舵の付いていない場合もあった。
Traditionally, flying boats have used the propulsion force of the flight engine exclusively for navigation on water, so the vertical tail rudder has been used primarily for steering during water navigation, and the submersible rudder has sometimes been used in conjunction with the submersible rudder. Sometimes there were no rudders.

従来λ飛行艇への人や荷物の積み降ろしは\飛行艇を滑
走台(エプロン)から陸上に引き揚げて行なうかA又は
水上で係留ブイに係留した飛行艇に小舟で近づいて接舷
して行なってきた。従って飛行艇用の接岸岩壁とか桟橋
等は存在しなかった。
Traditionally, loading and unloading of people and cargo onto a λ flying boat was done by pulling the flying boat onto land from the apron, or by approaching the flying boat moored to a mooring buoy on the water in a small boat and coming alongside. It's here. Therefore, there were no rock walls or piers for flying boats.

また1飛行梃の係留は専ら人手によって係留索のフック
を係留ブイに引っかけるか1又は飛行艇から錨を投錨し
て停船していた。
In addition, the mooring of the 1-aircraft was carried out manually either by hooking the mooring line to the mooring buoy, or by dropping an anchor from the flying boat.

ジェット飛行艇は存在しなかったのでλそのジェットエ
ンジンに対する鳥害防止装置も存在しなかった。ただし
ターボプロップエンジン飛行艇は存在した。
Since there were no jet flying boats, there were no bird protection systems for jet engines. However, turboprop engine flying boats did exist.

(発明が解決しようとする問題点) 「昭和60年特許願第60..−206601号」で特
許出願中の「水中翼による水上飛行機及び飛行艇の離着
水性能改善方式」を提唱しただけでば1ペイロードが悪
いといわれる飛行艇で大量航空輸送時代を招来させるこ
とはできず1このベイ−ロードを悪くしている諸要因を
解決除去しなければならない。本発明は1その主要な問
題を解決せんとするものである。また・特許出願中の「
昭和60年特許願第6O−2(16601号」は基本的
な方式の特許出願で1その水中翼は基本的な単一方式を
示しているだけなので、実際的な水中翼装置の構造を具
体的に明示する必要がある。また−飛行艇の水中翼は強
方な水の抵抗力を利用して飛行艇を短距離で離水させる
ものであるから、飛行艇胴体の接水底面は舟底形にする
必要はなく1普通の陸上航空機の胴体形状の)までよい
が\それでもやはり水の粘着力を解消させる方法を構す
る必要があり1飛行艇に水中翼を設置すれば水の抵抗力
が増大し1゛飛行艇の゛推−進力に対する抗力も増大す
るので1この抗力に打ち勝つ推進力を増加させる必要が
ある。
(Problem to be solved by the invention) The patent application is being applied for in "Patent Application No. 60..-206601 of 1985", which merely proposes "a method for improving the takeoff and landing performance of seaplanes and flying boats using hydrofoils". We cannot usher in the age of mass air transportation with flying boats, which are said to have a bad payload, and we must solve and eliminate the various factors that make this payload bad. The present invention seeks to solve one of these major problems. Also, patent pending “
Patent Application No. 6O-2 (No. 16601 of 1985) is a patent application for a basic system.1 Since the hydrofoil only shows a basic single system, it does not specifically describe the structure of a practical hydrofoil device. In addition, since the hydrofoil of an airship uses strong water resistance to take off the airship over a short distance, the bottom surface of the airship fuselage that is in contact with the water should be It is not necessary to make it into a shape like the fuselage of a normal land aircraft, but it is still necessary to devise a method to eliminate the adhesion of water.1 If you install hydrofoils on a flying boat, you can reduce the resistance of water. increases, and the drag against the propulsive force of the flying boat also increases, so it is necessary to increase the propulsive force to overcome this drag.

飛行艇の水上航行時)飛行用主エンジン推力だけで航行
していたのでは1水の抵抗力は空気の約800倍もある
のでh航空燃料が無駄に消費され極めて不経済である。
If a flying boat were to navigate on water using only the thrust of its main flight engine, the resistance of water would be approximately 800 times that of air, so aviation fuel would be wasted and it would be extremely uneconomical.

またh水上航行中の操舵を垂直尾翼方向舵で行なってい
たのでは大まかな操舵しかできず凡特に微細な操舵を必
要とする接岸時の操舵はh垂直尾翼方向舵だけでは到底
無理で1何らかの対策が必要である。
In addition, if the vertical tail rudder was used for steering while navigating on water, only rough steering would be possible, and steering when berthing, which requires particularly fine steering, would be impossible with the vertical tail rudder alone; is necessary.

飛行艇の係留に1人力によって係留索のフックを引っか
けるやり方は)非常な労力と時間の空費で1それだけ航
空燃料も無駄に消費され不経済でちる。
The method of manually hooking the mooring line to the mooring of an airship requires a great deal of effort and time, and also wastes aviation fuel, making it uneconomical.

飛行艇への人や荷物の積み降ろしに1飛行艇をいちいち
陸上に引き揚げて行なっていたのでは、時間と労力と航
空燃料!7)苅常な無駄使いであり、係留ブイに係留し
た飛行艇に小舟で接近して積み降ろしをすることも1時
間と労力の非常な無駄使いであるばかりでなく1非常に
不安定で危険なやり方で、一般的ではなかった。投錨停
泊中の飛行艇でも同様である。従って飛行艇も一般の船
舶と同じように岸壁に接岸させてしっかりと係留固定し
1人や荷物の積み降ろしを安全確実に1能率的に実施す
る必要があるが1飛行梃の主翼が5鷹になJ)X飛行艇
を岸壁に横付けさせることはできないので為飛行艇独特
な対策が必要でちった。
It would have taken time, effort, and aviation fuel to have to bring each flying boat back to land one by one to load and unload people and cargo onto the flying boat! 7) It is a common waste of money, and approaching the flying boat moored to the mooring buoy in a small boat to load and unload it is not only a huge waste of time and labor, but also extremely unstable and dangerous. It was not a common method. The same applies to flying boats at anchor. Therefore, just like other ships, flying boats need to be moored securely and moored to a quay in order to load and unload passengers and cargo safely, reliably, and efficiently. Since it was not possible to make the flying boat come alongside the quay, countermeasures unique to flying boats were required.

飛行艇の発着する港湾や貯水池等の多くは\鴎などの水
鳥が多数群がっておりX特にジェット飛行艇を発着させ
る場合には\ジェットエンジンに対する鳥害を防止する
ことが極めて重要な問題となる。
Many of the ports and reservoirs where flying boats take off and land are home to large numbers of water birds such as seagulls, and especially when taking off and landing jet flying boats, it is extremely important to prevent bird damage to jet engines. .

以上の諸問題を完全に解決しなければA飛行艇による本
格的な大量航空輸送時代を招来させることはできないの
で1これらの諸問題を本発明(でよって解決し)海に囲
まれた狭い島国日本で、陸上飛行場の全く不要な飛行艇
はよる本格的な大ffi a空輸送時代を招来させるこ
とを目的とする。
Unless the above-mentioned problems are completely solved, we will not be able to bring about the age of full-scale mass air transport using flying boats. In Japan, the purpose of the flying boat, which does not require any land airfield, is to usher in a full-fledged era of large-scale air transportation.

口1発明の構成 (問題点を解決するだめの手段) 本発明は以上の諸問題を解決するため1次の諸手段の組
み合わせ構成によって解決づせる。
1. Structure of the Invention (Means for Solving the Problems) The present invention solves the above-mentioned problems by combining the following means.

(1)  飛行艇用折りたたみ式扇形水中翼装置。(1) Foldable fan-shaped hydrofoil device for flying boats.

(2)気泡による飛行艇の離水性能改善装置。(2) A device for improving the take-off performance of flying boats using air bubbles.

(3)飛行艇の水中推進装置。(3) Underwater propulsion system for flying boats.

(4)  飛行艇の吸着係留装置。(4) Adsorption mooring device for flying boats.

(5)  飛行艇用浮桟橋。(5) Floating pier for flying boats.

(6)  ジェット飛行艇の鳥害防止装置。(6) Bird damage prevention device for jet flying boats.

(作用及び実施例) 以下図面によってへ以上の諸装置の作用及び実施例を1
特許請求の範囲第1項から第9項までの各項目毎に順次
詳細に説明する。
(Operations and Examples) The operations and examples of the above devices are explained below with reference to the drawings.
Each item of claims 1 to 9 will be explained in detail in turn.

(1)  飛行艇用折りたたみ式扇形水中翼装置(特許
請求の範囲第1項) 第1図の!A図は1飛行艇用折シたたみ式扇形水中翼装
置の扇形水中R1を水中に出した状態を氷水底面10の
胴体内部の収納箱9に収納した状態を示す側面図。0図
は1扇形水中R1を上から見た形状を示す平面図。D図
は)扇形水中翼1を収納箱9に収納して下から見た状態
を示す平面図。E図は1扇形水中真白体も折りたためる
構造の扇形水中翼11を上から見た状態を示す平面図。
(1) Foldable fan-shaped hydrofoil device for flying boats (Claim 1) Figure 1! Figure A is a side view showing a state in which the fan-shaped submersible R1 of the foldable fan-shaped hydrofoil device for an airship is put out into the water and stored in the storage box 9 inside the fuselage on the ice water bottom surface 10. Figure 0 is a plan view showing the shape of one fan-shaped underwater R1 viewed from above. Figure D) is a plan view showing the state in which the fan-shaped hydrofoil 1 is stored in the storage box 9 and viewed from below. Fig. E is a plan view showing a state in which a sector-shaped hydrofoil 11 having a structure in which even one sector-shaped underwater body can be folded is viewed from above.

2図は扇形水中翼11を折シたたんで収納箱9に収納し
て下から見た状態を示す平面図である。
FIG. 2 is a plan view showing the state in which the fan-shaped hydrofoil 11 is folded and stored in the storage box 9, viewed from below.

第2図はAジェット飛行艇胴体接水底面に扇形水中翼装
置15116を装備した一実施例を示し1ジ。
Figure 2 shows an embodiment in which a fan-shaped hydrofoil device 15116 is installed on the bottom surface of the A-jet flying boat's fuselage in contact with the water.

ニット飛行艇の下から見た状態を示す平面図。A plan view showing the state of the knitted flying boat seen from below.

第3図は)双胴無尾翼型ジェット飛行艇胴体接水底面に
扇形水中翼装置26% 27128X29を装備した実
施例を示し1双胴無尾翼型ジェット飛行艇の下から見た
状態を示す平面図である。
Figure 3) shows an example of a twin-hulled tailless jet flying boat equipped with a fan-shaped hydrofoil device 26% 27128x29 on the bottom surface of the fuselage in contact with the water, and shows a plane view from below of the twin-hulled tailless jet flying boat. It is a diagram.

第1図のA図において1扇形水中g1は支柱2の下端の
回転支持部8で所定の角度以上には下方に開かないよう
に連結されており1支柱2に通しである摺動環7は1操
縦席からの遠隔監視制御によって制御される連結棒5に
よって上下し1この摺動環7を上方に引き上げることに
より1扇形水中翼1は連結棒3によって上方に引き上げ
られ、扇形水中翼1は支柱2の下端の回転支持部8を支
点として上方に回転し1扇形水中翼工が支柱2に密着し
た状態で停止する。
In Fig. 1A, 1 fan-shaped submersible g1 is connected to the rotation support part 8 at the lower end of the support column 2 so as not to open downward beyond a predetermined angle, and the sliding ring 7 passing through the support column 2 is 1 The sector-shaped hydrofoil 1 is raised and lowered by the connecting rod 5 controlled by remote monitoring control from the pilot's seat, and by pulling the sliding ring 7 upward, the sector-shaped hydrofoil 1 is pulled upward by the connecting rod 3. The rotary support part 8 at the lower end of the strut 2 is used as a fulcrum to rotate upward, and the one sector-shaped hydrofoil is stopped in close contact with the strut 2.

次に支柱2に連結された連結棒4を飄操縦席からの遠隔
監視制御により後方に引き揚げればX支柱2は支柱2の
上部の回転支持部6を支点として後上方に回転して引き
揚げられ、8図の状態のように収納箱9に収納される。
Next, when the connecting rod 4 connected to the strut 2 is pulled up backwards by remote monitoring and control from the pilot's seat, the X strut 2 is rotated backwards and upwards using the rotational support section 6 at the top of the strut 2 as a fulcrum and pulled up. , are stored in the storage box 9 as shown in Figure 8.

収納している扇形水中翼1を水中に出す場合は1以上と
逆の操作をすればよい。
If you want to take out the stored fan-shaped hydrofoil 1 into the water, you can perform the operations in the reverse order.

扇形水中翼1自体は折シたたまない方式で構造が簡単で
あり1その材質は高速着水時の水の衝撃に耐え1耐塩水
性でなるべく軽い材質であれば何でもよいがλ折りたー
たみ式扇形水中翼11の場合にはへ以上の材質染件の外
に可撓性が必要であり1炭素繊維編組板のような強靭な
材質を使用しなければならない。
The fan-shaped hydrofoil 1 itself has a simple structure because it does not fold.1 The material can be made of any material as long as it can withstand the impact of water during high-speed landing and is resistant to salt water and is as light as possible. In the case of the fan-type hydrofoil 11, in addition to the material dyeing, flexibility is required, and a strong material such as a carbon fiber braided plate must be used.

水中翼を扇形にした利点は為以上の機構にょって1扇形
水中翼11の開閉を1丁度傘を開閉するように開閉でき
ることと1飛行艇の着水時Aこの扇形水中翼1又は11
が極めて合理的に接水することにある。即ち一飛行艇が
着水する場合に最初に接水するのはA第2図の実施例に
おいて\飛行艇後部の扇形水中翼16の「扇のかなめ部
分」から接水し1飛行艇の着水滑走速度が減少するに従
いへ扇形水中翼16の接水面積は次第に増大し1水に対
する抵抗力が速度に応じて極めて合理的に機能するから
である。
The advantage of having a fan-shaped hydrofoil is that the fan-shaped hydrofoil 11 can be opened and closed just like opening and closing an umbrella using the mechanism described above, and that when an airship lands on the water, the fan-shaped hydrofoil 1 or 11 can be opened and closed just like opening and closing an umbrella.
The reason is that it comes in contact with water in a very rational manner. In other words, when one flying boat lands on water, the first place it touches the water is in the embodiment shown in Figure 2. This is because as the hydroplane speed decreases, the water contact area of the fan-shaped hydrofoil 16 gradually increases, and the resistance force against water functions extremely rationally depending on the speed.

次に1水中翼によって離着水する飛行艇であるから)飛
行艇胴体の接水底面を舟形構造にする必要もなければ「
水切り」を設ける必要もなくA空中を飛行中は水中翼を
収納箱に収納して飛行するので有害な空気抵抗も生じな
い。′その上1飛行艇の離着水は水中翼に対する強力な
水の抵抗力による揚力によって離着水するわけであるか
ら)水中翼の面積は非常に僅少な面積で、も容易に飛行
艇を短距離で離水させることができ、第3図のような双
胴型飛行艇の実現も可能となる。この点1従来の主翼の
揚力だけで離水させようとしてきた飛行艇では1飛行艇
の双胴化などは全くの夢物語りに過ぎなかった。
Secondly, since it is a flying boat that takes off and lands on water using hydrofoils, there is no need to make the bottom surface of the flying boat body in contact with the water a boat-shaped structure.
There is no need to install a "drainer" and the hydrofoils are stored in the storage box while flying in the air, so there is no harmful air resistance. 'Furthermore, (1) the area of a hydrofoil is very small, making it easy for a flying boat to take off and land on water. It can take off from water over a short distance, making it possible to create a twin-hulled flying boat as shown in Figure 3. In this respect, 1. With conventional flying boats that attempted to take off from water using only the lift of the main wings, the idea of turning a flying boat into a twin-hulled aircraft was nothing more than a pipe dream.

飛行艇の双胴化には重大な必要理由がある。それはA単
胴の飛行艇が離着水する場合には1必らず風上方向に向
かって離着水する必要がある。もしも横風を受けての離
着水を強行すれば1単胴の飛行艇は簡単に横転転覆して
しまうからである。
There are important reasons why flying boats should be made into twin hulls. When an A single-hulled flying boat takes off and lands on water, it must always take off and land in the upwind direction. This is because if a single-hulled flying boat were forced to take off and land in a crosswind, it would easily capsize.

その点\2ヶの主車輪でシラカリと大地に支えられてい
る陸上航空機の場合は1相当強い横風を受けての離着陸
が可能である。しかるに飛行艇が内陸部の狭い貯水池等
で離着水する場合には1地形の関係上どうしても横風離
着水せねばならぬ場合がある。それを可能ならしめる方
法は為飛行艇を双胴化することだけである。かかる理由
から水中翼によって飛行艇を双胴化できることは1極め
て重要な意義を有するのである。従って単なる空想によ
って双胴型飛行艇を提唱するものではなく1以上の重大
なる必要性によってり飛行艇ρ双胴化を提唱するもので
あA− かくして双胴大型の水中翼式ジェット飛行艇を実現させ
れば1いかなる荒天時の洋上離着水も可能となり、いつ
いかなる海難救助にもスピーディに対処でき1海難救助
に一犬威力を発揮するでちろう。また)双胴型水中翼飛
行艇は漁業等にもfll用される。
On the other hand, in the case of a land aircraft, which is supported firmly by the ground with its two main wheels, it is possible to take off and land in considerably strong crosswinds. However, when an airship takes off and lands on water at a narrow inland reservoir, etc., there are cases where it is necessary to take off and land in a crosswind due to the topography. The only way to make this possible is to make the flying boat a twin hull. For this reason, the ability to make a flying boat a twin-hulled aircraft using hydrofoils has extremely important significance. Therefore, I am not advocating a twin-hulled flying boat based on mere fantasy, but rather due to one or more serious needs. If realized, it would be possible to take off and land on the ocean in any stormy weather, and it would be possible to respond quickly to any kind of marine rescue at any time, demonstrating the power of one dog for each marine rescue. Also, twin-hulled hydrofoils are used for fishing, etc.

なお1第2図のジェット飛行艇は水陸両用型を示し11
9λ、20は主車輪121は前車輪を示し1このジェッ
ト飛行艇が陸上の飛行場で離着陸する場合にば1従来の
陸上航空機゛と姿形も何ら変るところはない。また第3
図の双胴塑ジェット飛行艇も水陸両用型で、32,33
は主車輪)34s35は前車輪でである。なお40s4
1s42は無尾翼上面のジェットエンジンを示す。この
ように従来の陸上ジェット機と変りのない飛行艇なので
)外国航空路に使用しても何ら支障はなく1狭い島国日
本からは飛行艇として港湾から発進I−1アメリカ等の
大陸には普通の陸上航空機として着陸すればよい。実は
アメリカは広大な大陸国だからこそ1広大な飛行場を幾
つも作ることができ)従って陸上ジェット機だけを発展
させてきたとも云い得る。しかるに日本は狭い島国であ
るから国情は全く異なり為アメリカ流に飛行場を沢山作
り1飛行場を拡張して行ったのではタマッタものではな
い。ここに日本の航空行政の根本的に重大な問題がある
。日本は狭い島国らしく1飛行艇を主体にした航空体制
に切替えるべきである。そして南方島国諸国との交流も
飛行艇によって活発化すべきである。それには水中翼に
よる飛行艇が最適である。
Note that the jet flying boat shown in Figure 1 is an amphibious type.11
9λ, 20 indicates a main wheel 121 representing a front wheel. 1 When this jet flying boat takes off and lands at an airfield on land, its appearance is no different from that of a conventional land aircraft. Also the third
The twin-hulled plastic jet flying boat shown in the figure is also an amphibious type, 32,33
is the main wheel) 34s35 is the front wheel. In addition, 40s4
1s42 shows a jet engine with a tailless upper surface. In this way, since it is a flying boat that is no different from a conventional land jet aircraft, there is no problem in using it on foreign air routes.1 From the small island nation of Japan, it is launched from the port as a flying boat. Just land as a land aircraft. In fact, because the United States is a vast continental country, it was able to build multiple vast airfields; therefore, it can be said that the United States has only developed land-based jet aircraft. However, since Japan is a small island nation, the national situation is completely different, and building many airfields and expanding one airfield in the American style would not have been a complete success. Here lies a fundamentally serious problem with Japan's aviation administration. Japan, as a small island nation, should switch to an air system based on one flying boat. Exchanges with the southern island nations should also be activated through the use of flying boats. A flying boat using hydrofoils is ideal for this purpose.

また\従来の外国航路の陸上ジェット機でも\事故等に
よシ太平洋上に不時着水せねばならぬ場も当然想定して
おくべきで1水中翼装置は以上の説明で明らかなように
A極めて単純小型な装置であるから)これらの陸上ジェ
ット機に装備することも容易であi事故時の洋上着水も
安全に行なうことができ1人命救助にも大いに役立つ。
Also, even with conventional land-based jet aircraft on foreign routes, it is of course necessary to assume that there will be situations where an emergency landing in the Pacific Ocean may occur due to an accident.1 The hydrofoil system is extremely simple, as is clear from the above explanation. Since it is a small device, it is easy to install it on these land jet aircraft, and it can safely land on the ocean in the event of an accident, making it extremely useful in saving one person's life.

広い洋上に比較すれば、どんなに広い飛行場でも非常に
狭いので1操縦不能に陥った時に\狭い飛行場に着陸し
ようとすることは非常に危険でλこρような場合には広
い洋上に不時着水すべきである。
Compared to the vast ocean, even the widest airfield is very narrow, so if you lose control of the aircraft, it is very dangerous to try to land on a narrow airfield. Should.

(2)  気泡による飛行艇の離水性能改善装置(特許
請求の範囲第2項) 本発明の基本は)水中翼による飛行艇の離着水性能の改
善にあり1水中翼に対する水の強力な抵抗による揚力に
よって1短距離の離水滑走に上り強引に飛行艇胴体を離
水させることにあるから\飛行艇胴体の接水底面は一通
常の陸上航空機の胴体形状のままでよいことに大きな特
徴がある。
(2) Device for improving the take-off and landing performance of flying boats using air bubbles (Claim 2) The basis of the present invention is to improve the take-off and landing performance of flying boats using hydrofoils. 1. Strong resistance of water against hydrofoils. The purpose of this is to force the flying boat's fuselage to take off from the water by using the lift force generated by the aircraft to take off over a short distance.A major feature is that the bottom surface of the flying boat's fuselage that touches the water can remain in the shape of a normal land aircraft fuselage. .

しかしそうは云っても1飛行艇胴体の接水底面には何ら
の離水性能改善対策もなされていないのであれば)飛行
艇胴体接水底面と水との吸着力は絶大なものとなり1こ
の吸着力が1水中翼による離水力を妨害することになる
However, if no measures have been taken to improve take-off performance on the water-contact bottom surface of the flying boat's fuselage, the adsorption force between the water and the water-contact bottom surface of the flying boat's fuselage will be enormous, and this adsorption The force will interfere with the take-off force by the hydrofoil.

しかし1飛行艇胴体接水底面と水との間に空気層を介在
せしめれば1この吸着力は急激に減少する。、このこと
は昔かられかっていたことで1水上飛行機や飛行艇の接
水底面に気泡が流入し易かよ、5、な対策が構しられて
きた。・その方法は接:水底面の前部にヒレを付けるな
どによって\空気が流入し易いようにしたものだが−か
がる方法では飛行中の有害抵抗が増大し1あまり得策で
はなかった。
However, if an air layer is interposed between the water-contact bottom surface of the flying boat's fuselage and the water, this adsorption force will decrease rapidly. This has been known for a long time, and countermeasures have been taken to prevent air bubbles from entering the bottom of seaplanes and flying boats.・The method was to make it easier for air to flow in by attaching a fin to the front of the bottom surface of the water, but the method of bending increased the harmful resistance during flight and was not very good.

そこで本発明は1飛行艇内部に空気ポンプを置きXこの
空気ポンプから圧送される空気を)可撓バ、イブを通し
て飛行艇胴体の接水底面の前部及び中間部附近に導ひき
)その気泡放出口から気泡を放出せしめ)飛行艇胴体接
水底面と水との吸着力を解消せしめたものである。
Therefore, in the present invention, an air pump is installed inside the flying boat, and the air pumped from this air pump is guided to the vicinity of the front and middle parts of the water-contacted bottom of the flying boat body through a flexible bar and an eve. Air bubbles are released from the outlet to eliminate the adsorption force between the bottom surface of the flying boat's body and the water.

この方法であれば、小さな気泡放出口を開閉することは
簡単なので1離水時にのみこの気泡放出口を開いて気泡
を発生せしめ)飛行中は閉ぢて飛行すれば)−有害抵抗
が生ずる恐れもない。
With this method, it is easy to open and close the small bubble outlet, so if you open the bubble outlet to generate bubbles only during takeoff (and keep it closed during flight) - there is a risk of harmful resistance. do not have.

第2図の22,23及び1第3図の36 X37\38
\39は気泡放出口で1その配置状況の一実施例を示す
22, 23 in Figure 2 and 1 36 in Figure 3 X37\38
\39 is a bubble discharge port 1. An example of its arrangement is shown.

かかる程度の空気ポンプは小型軽量のポンプで十分と思
われるので一飛行艇の荷重を増やすことにはならない、
− (3)  ジェットエンジン排気の一部を利用した気泡
による飛行艇の離水性能改善装置(特許請求の範囲第3
項) 本発明は\前項の空気ポンプの代りに)ジェットエンジ
ン排気の一部を利用したもので1ジエツトエンジン排気
といっても為高熱排気ではなく・低熱部分を利用する。
It seems that a small and lightweight air pump of this kind is sufficient, so it will not increase the load of the flying boat.
- (3) A device for improving the take-off performance of an airship using air bubbles using a part of jet engine exhaust (Claim 3)
Section) The present invention uses a part of the jet engine exhaust (instead of the air pump in the previous section), and although it is called a single jet engine exhaust, it uses the low-heat part rather than the high-heat exhaust.

(4)  飛行艇の水中推進機(特許請求の範囲第4項
)飛行艇に水中推進機を取り付ける目的は次の三つであ
る。第一1水上航行は水中推進機(スクリュウ)で航行
させA航空燃料を節約する。第二\飛行艇接岸時の操舵
。第三1離水滑走時為水中翼の抵抗増加分をスクリュウ
で推力を増加させる。
(4) Underwater propulsion device for a flying boat (Claim 4) The purpose of installing a underwater propulsion device on a flying boat is as follows. The 11th water navigation will use an underwater propulsion device (screw) to save aviation fuel. Second \Steering when the flying boat comes to shore. 31. During takeoff and skiing, the thrust is increased by the screw to compensate for the increased resistance of the hydrofoil.

従来1飛行艇が水上航行をする場合は・専ら飛行用主エ
ンジン推力によって航行していたが1水の抵抗力は空気
の約800倍もあり翫大きな梃体を飛行用エンジンで引
っばることは航空燃料の多大な損失であった。従って飛
行艇が水上航行する場合は直接に水に作用するスクリュ
ウで航行するのが最も合理的で経済的である。
Conventionally, when a flying boat navigated on water, it did so solely by the thrust of its main flight engine, but the resistance of water is about 800 times that of air, so it was impossible to pull a large lever with a flight engine. This was a huge loss of aviation fuel. Therefore, when a flying boat navigates on water, it is most rational and economical to do so using a screw that acts directly on the water.

第二の接岸時の操舵であるが\従来1水上における飛行
艇の操舵は)専ら飛行用主エンジン推力と垂直尾翼方向
舵を主用してきたが1これでは旋回半径が大きくなり1
敏速な制動もできず、犬まかな操舵しかできなかった。
Second, regarding steering during docking, conventionally 1 the steering of an airship on water has mainly used the thrust of the flight main engine and the vertical tail rudder, but 1 this increases the turning radius and 1
It was not possible to brake quickly and could only be steered in a rough manner.

しかるに後述するように、飛行艇が接岸係留して人や荷
物の積み降ろしをするようになれば)その接岸時の操舵
は微細正確な操舵が必要となり八とても従来のような大
まかな操舵では間に合わない。タッグボートで接岸させ
るという方法もあるが1飛行艇胴体は薄いジュラルミン
で出来ているので1そんなことはできない。
However, as will be explained later, if flying boats come to be moored to the shore and loaded and unloaded with people and cargo, fine and precise steering will be required when they come to the shore. do not have. There is also a method of bringing the ship to shore with a tugboat, but the body of the flying boat is made of thin duralumin, so that is not possible.

そこで本発明は)第2図のように≧−1推進方向を36
0度変えられるスクリュウ装置を、飛行艇胴体接水底面
の前部と後部に各々1ケづつ取り付けて、操舵を容易な
らしめたものである。第2図において\前部のスクリュ
ウ17と後部のスクリュウ18は矢印で示すように1推
進方向が反対になっている状態を示しているが旭前部と
後部のスクリュウの推進方向を反対方向にすれば1飛行
艇は同一場所で方向変換が可能となる。また、スクリュ
ウの推進方向を飛行艇の横方向の同一方向にすれば1飛
行艇は横方向に進みA飛行艇用桟橋(後述)への接舷も
唾めて容易となる。また1飛行艇が出航する場合にば1
これらのスクリュウ推進方向を出航方向にすればよいわ
けである。この点1従来の飛行用主エンジン推進力だけ
では非常に回器で1飛行用エンジンでいきなり逆推進を
かければ1岸壁上にいる人々に潮ふぶきをかけ大騒ぎと
なる。
Therefore, the present invention has been developed so that, as shown in Fig. 2, ≧-1 propulsion direction is 36
Screw devices that can be rotated by 0 degrees are attached to the front and rear parts of the water-contacted bottom of the flying boat's fuselage, making it easier to steer. In Figure 2, the front screw 17 and the rear screw 18 are shown with opposite propulsion directions as indicated by the arrows, but the front and rear screws have opposite propulsion directions. This allows one flying boat to change direction at the same location. Furthermore, if the propelling direction of the screws is the same as the lateral direction of the flying boat, one flying boat can move laterally and come alongside the jetty for flying boat A (described later) with great ease. In addition, if 1 flying boat departs, 1
The direction of propulsion of these screws should be the direction of sailing. In this point 1, the propulsion force of the conventional flight main engine is too strong, and if the flight engine were to suddenly apply reverse propulsion, the people on the pier would be splashed with sea spray and it would cause a big fuss.

なお1飛行艇が接岸する場合には1一般の船舶と同様に
X 「前進1前進微速A後進」などと、スクリュウ推進
力を微細に調節しながら静かに接岸しなければならない
が1そのためには1飛行艇用のスクリュウも逆回転でき
るスクリュウを使用することが望ましい。しかし飛行艇
前部と後部のスクリュウ推進方向を反対にしなから−静
かに接岸することも可能である。
In addition, when an airship berths, it must berth quietly while finely adjusting the propelling force of the screw, such as 1. 1. It is desirable to use a screw that can be rotated in the opposite direction for a flying boat. However, it is also possible to berth quietly by reversing the propulsion directions of the front and rear screws.

第3図は双胴型飛行艇にスクリュウを配置した状態を示
し1スクリユウは30s31に示す。この場合にはスク
リュウは右胴体後部と左胴体後部と離れた位置について
いるので1この2ケのスクリュウだけで飛行艇の方向変
換は可能であシへ飛行艇前部のスクリュウは省略できる
。しかし大型双胴の飛行艇の場合には前部にも必要であ
る。
Figure 3 shows the state in which the screws are arranged on a twin-hulled flying boat, and one screw is shown at 30s31. In this case, the screws are located apart from the rear right fuselage and the rear left fuselage, so it is possible to change the direction of the flying boat with just these two screws, and the screw at the front of the flying boat can be omitted. However, in the case of large twin-hulled flying boats, it is also necessary for the front part.

第三の問題点)本発明の基本は水中翼により飛行艇の離
水を早める点にあるが1水中翼を水中に出せば当然水中
抵抗力が増大し翫飛行艇の推進力に対して大きな抗力と
なる。従ってこの抗力増大分をスクリュウ推進力で相殺
し為飛行艇の離水をさらに早める。
Third problem) The basic idea of the present invention is to use hydrofoils to speed up the take-off of the flying boat, but if the hydrofoils are brought out into the water, the underwater resistance naturally increases, creating a large drag against the propulsion force of the flying boat. becomes. Therefore, this increase in drag is offset by the propelling force of the screw, thereby further speeding up the take-off of the flying boat.

かくして前述の気泡による離水性能改善装置や従来から
の主翼フラップによる高揚力装置等を併用すればh飛行
艇の離水滑走距離は大幅に短縮できる。
Thus, by using the above-mentioned water-separation performance improvement device using air bubbles, the conventional high-lift device using main wing flaps, etc., the water-takeoff run distance of the H flying boat can be significantly shortened.

第4図は1本発明の飛行艇用水中推進装置の構造概要を
原理的に示し\A図は平面図1 B図はスクリュウ46
を水中に出した状態の側面図10図はスクリュウ46を
飛行艇胴体接水底面60部の収納箱54に収納した状態
の側面図である。
Figure 4 shows the principle of the structure of the underwater propulsion system for flying boats according to the present invention. Figure A is a plan view. Figure B is a screw 46.
FIG. 10 is a side view of the screw 46 stored in the storage box 54 at the water-contact bottom surface 60 of the flying boat fuselage.

されらの図面においてλ47はスクリュウ46を駆動す
るガソリンエンジン又は電動モーターで1この駆動部4
7は操縦席からの遠隔監視制御によって制御される。
In these drawings, λ47 is a gasoline engine or an electric motor that drives the screw 46.
7 is controlled by remote supervisory control from the cockpit.

スクリュウ46の推進方向は360度の方向変換が可能
であるが1その方向変換はサーボモーター48によって
駆動され\このサーボモーター48に直結した駆動ギヤ
ー50により為連動ギヤー49が連動してスクリュウ駆
動部47が回転し\スクリュウ46の推進方向を目的と
する方向に向ける。以上の制御も操縦席からの遠隔監視
制御によって制御する。
The direction of propulsion of the screw 46 can be changed by 360 degrees.1 The direction change is driven by a servo motor 48, and an interlocking gear 49 is interlocked with a drive gear 50 directly connected to this servo motor 48 to drive the screw. 47 rotates to direct the propelling direction of the screw 46 to the desired direction. The above controls are also controlled by remote monitoring and control from the cockpit.

飛行中はスクリュウ46をスクリュウ収納用連結棒56
によって収納箱54に収納する。その場合1スクリュウ
装置本体は、連動ギヤー49との支持部51を支点とし
て後方に回転して引き揚げられ1収納箱54に収納され
る。
During flight, the screw 46 is connected to the connecting rod 56 for storing the screw.
It is then stored in the storage box 54. In this case, the main body of the 1-screw device is rotated backward using the support portion 51 with the interlocking gear 49 as a fulcrum, and is lifted up and stored in the 1-storage box 54.

その他へ52は連動ギヤー49を支持する支持環で、こ
の支持環52は収納箱54及びフレーム53に固定され
ている。また1スクリユウ装置収納用連結棒56とスク
リュウ装置との連結部は連結環59によって連結されて
いる。これはスクリュウ46の推進方向を自由に変えら
れるようにするためである。
52 is a support ring that supports the interlocking gear 49, and this support ring 52 is fixed to the storage box 54 and the frame 53. Further, the connecting rod 56 for housing one screw device and the connecting portion of the screw device are connected by a connecting ring 59. This is to enable the direction of propulsion of the screw 46 to be changed freely.

以上の説明は1スクリユウ装置の全体を原理的に説明す
る便宜上1スクリユウ46と駆動部47を一体にした構
造で説明したが為実際には、駆動部47が水没したので
は具合いが悪いので1駆動部47は飛行艇内部の浸水し
ない場所に固定し1スクリユウ46のリンク機構以下の
部分を水中に出すようKする。
In the above explanation, for the sake of explaining the entire 1-screw device in principle, the structure in which the 1-screw 46 and the drive section 47 are integrated has been explained. The drive unit 47 is fixed in a place inside the flying boat where it will not be flooded with water, and the part below the link mechanism of the first screw 46 is exposed to the water.

(5)  飛行艇の吸着係留装置(特許請求の範囲第5
項)飛行艇による大量航空輸送時代となれば1人や荷物
の積み降ろしは安全迅速に行なう必要があり1飛行艇の
接岸係留も安全迅速に行なわなければならず、従来の「
もやい綱」で係留するようなやり方では間に合わない。
(5) Adsorption mooring device for flying boat (Claim No. 5)
Section) In the age of mass air transport using flying boats, it is necessary to load and unload one person and cargo safely and quickly, and mooring one flying boat to the shore must also be done safely and quickly.
Mooring with a "mooring rope"won't make it in time.

本発明の吸着係留装置は1かかる飛行艇を安全迅速に係
留する装置で\第6図はその機構を原理的匝示した説明
図で\第6図はその一実施例を示す平面図・〜第7図は
側面図島相8図は双胴型飛行艇に応用した場合の平面図
である。
The suction mooring device of the present invention is a device for mooring such an airship safely and quickly. Figure 6 is an explanatory diagram showing the principle of the mechanism. Figure 6 is a plan view showing one embodiment of the device. Figure 7 is a side view, and Figure 8 is a plan view when applied to a twin-hulled flying boat.

第5図において)飛行艇67が岸壁66に接岸する場合
には1排気ポンプ63に可撓バイブロ2で連結された吸
着盤61が1繰り出し装置65によって飛行艇67の艇
首部分から必要な長さだけ繰り出され覆板着盤61を岸
壁66に圧着するだけで吸着盤61は岸壁661C吸着
し)飛行艇67は簡単に係留される。この係留を解除す
る場合には1可撓バイブロ2の途中の開閉弁64を開く
ことにより)吸着盤61の吸着力はなくなり為吸着盤6
1は簡単に岸壁6Gから離れ為飛行艇67の係留は解除
される。係留を解除して飛行艇が出航する場合には・為
繰り出し装置65によって吸着盤61を収納し)艇首を
艇首カバー68で覆って水上航行に移る。以上の操作−
はすべて操縦席からの遠隔監視制御によ゛つて行う。
5) When the flying boat 67 is docked on the quay 66, the suction cup 61 connected to the exhaust pump 63 by the flexible vibro 2 is moved to the required length from the bow of the flying boat 67 by the feeding device 65. The flying boat 67 is easily moored by simply pressing the cover plate mounting plate 61 onto the quay wall 66, and the suction cup 61 attracts the quay wall 661C. When this mooring is released, by opening the on-off valve 64 in the middle of the flexible vibro 2), the suction force of the suction cup 61 is lost, so the suction cup 6
1 easily leaves the quay 6G, and the mooring of the flying boat 67 is released. When the flying boat departs from the mooring, the suction cup 61 is retracted by the feeding device 65), the bow is covered with the bow cover 68, and the boat starts sailing on water. Above operations −
All operations are controlled remotely from the cockpit.

飛行艇の接岸岩壁が満員の場合には為係留ブイに係留し
て待機する必要も生ずるが1この場合の係留ブイへの係
留も上記と同様に吸着係留させる。
If the rock wall where the flying boat is docked is full, it may be necessary to moor to a mooring buoy and wait.1 In this case, the mooring to the mooring buoy is also done by suction mooring in the same way as above.

次に)第6図と第7図の実施例において〜飛行艇78の
吸着盤による吸着係留は71.72.73の3ケ所で係
留されており、吸着盤71は岸壁741c吸着し)吸着
盤72.73は飛行艇用浮桟橋75の側壁吸着面に吸着
係留されている。ただし飛行艇用浮桟[75は後述の本
発明の特許請求の範囲第8項の浮桟橋である。
Next) In the embodiments shown in Figs. 6 and 7, the suction mooring of the flying boat 78 by the suction cups is moored at three locations 71, 72, and 73, and the suction cup 71 suctions the quay wall 741c) 72 and 73 are suction moored to the side wall suction surface of the floating jetty 75 for flying boats. However, the floating pier for an airship [75 is a floating pier according to claim 8 of the present invention, which will be described later.

このように3ケ所以上で確実に係留すれば1人や荷物の
積み降ろしを安全迅速に行なうことができる。
If the vessel is securely moored at three or more locations in this way, one person or cargo can be loaded and unloaded safely and quickly.

第8図の双胴型飛行艇の実施例においては1吸着盤91
%92は岸壁111に吸着係留し)吸着盤93N94、
明−96は飛行艇用浮桟橋97%98に吸着係留してい
る。この場合12本の浮桟橋97 z、 98は双胴型
飛行艇の2本の胴体102.103の内側の間隔と余裕
のあるように浮かせて置き1飛行艇は岸壁111に接岸
して吸着係留したる後1双胴型飛行艇の右側胴体102
は吸着盤93194を繰り出して浮桟橋97を吸着して
引き寄せ1左側用体103も同・様・恍゛シて浮桟橋9
8を吸着固定させる。
In the embodiment of the twin-hulled flying boat shown in FIG.
%92 is suction moored to the quay 111) suction cup 93N94,
Mei-96 is adsorbed and moored to floating jetty 97%98. In this case, the 12 floating piers 97z and 98 are placed afloat with enough space between the two bodies 102 and 103 of the twin-hulled flying boat, and one flying boat is docked at the quay 111 and moored by suction. Right fuselage 102 of Shirugo 1 twin-hulled flying boat
The suction cup 93194 is pulled out and the floating pier 97 is sucked and pulled.
8 is fixed by suction.

しかし1以上のような飛行艇の接岸は1従来の飛行用主
エンジン推進力だけによる大まかな操舵では全く接岸不
可能で1前述の飛行艇に装備した水中スクリユウによる
外はない。
However, the berthing of the above-mentioned flying boats is completely impossible with conventional rough steering using only the propulsion force of the main flight engine, and the only way to do so is by using the underwater screws installed on the above-mentioned flying boats.

(6)  電磁石式吸着盤(特許請求の範囲第6項)前
述の空気式吸着方式を電磁石式方式で実施することも当
然可能であって1この場合には1岸壁や浮桟橋の吸着面
には)鉄板等の磁性体を取り付けて薗けげよい。もちろ
ん電磁石式吸着盤の電源はへ蓄電池等の直流電源を使用
する。
(6) Electromagnetic suction cup (Claim 6) It is of course possible to implement the above-mentioned pneumatic suction method using an electromagnetic method. A) Attach a magnetic material such as an iron plate to the ground. Of course, the electromagnetic suction cup uses a DC power source such as a storage battery.

(7)  岸壁側からの吸着係留装置(特許請求の範囲
第7項) 前述の空気式または電磁石式による吸着係留′装置を陸
上岸壁側に装備して一飛行艇を吸着係留させることも可
能である。特に定期的に所定の港湾や貯水池等に就航し
ている飛行艇の場合には〜わざわざ飛行艇に吸着係留装
置を装備してffi量を増やす必要はなく)岸壁側から
吸着係留させた方がよい。
(7) Adsorption mooring device from the quay side (Claim 7) It is also possible to install the above-mentioned pneumatic or electromagnetic suction mooring device on the land quay side to suction and moor a flying boat. be. Especially in the case of an airship that is regularly in service at a designated port or reservoir, it is better to attach an adsorption mooring from the quayside (there is no need to go to the trouble of equipping the airship with an adsorption mooring device to increase the amount of ffi). good.

(8)  飛行艇用浮桟橋(特許請求の範囲第8項)一
般の船舶であれば岸壁に?直接接舷できるが1飛行艇は
主翼が邪魔になシ1飛行艇の胴体を岸壁に横付けさせる
ことはできない。
(8) Floating pier for flying boats (Claim 8) Is it a quay for ordinary ships? Although it is possible to come alongside directly, the main wing of the 1st flying boat gets in the way, so the body of the 1st flying boat cannot be brought alongside the quay.

そこで本発明は〜第6図箋第、7図のように1.岸壁7
4から海洋方向又は湖面方向の直角方向に1飛行艇用浮
桟橋75を水面87に浮かべ)この浮桟橋75の一端は
橋絡桟橋部分を径由して岸壁74の金具に連結し1浮桟
橋75の水上側他端は係留索88で水底90の係留ブリ
ック89に係留保持して置き)飛行艇78が接岸する場
合には)tず艇首の吸着係留a171を岸−壁74に吸
着係留せしめ1次に吸着係留盤7z:と73で本発明の
飛行艇用浮桟橋75を吸着係留して固定し1人や荷物の
禎み降ろしを安全迅速に行ない得るようにした。
Therefore, the present invention is as follows: 1. As shown in Figure 6 and Figure 7. Quay 7
Floating a floating jetty 75 for one flying boat on the water surface 87 in a direction perpendicular to the sea direction or the lake surface direction from the floating jetty 75) One end of this floating jetty 75 is connected to the metal fittings of the quay wall 74 via the bridging pier part, and the first floating jetty The other end of 75 on the water side is moored to a mooring brick 89 on the water bottom 90 with a mooring cable 88.) When the flying boat 78 comes ashore, the suction mooring a171 on the bow of the boat is suction moored to the shore wall 74. First, the floating jetty 75 for an airship according to the present invention is suction moored and fixed by suction mooring plates 7z and 73, so that one person and cargo can be safely and quickly unloaded.

従りてこの浮桟橋75の側面には飛行艇78の吸着盤7
2と73を吸着させるだめの吸着面を備え1空気式吸着
の場合には平滑な吸着面とし1電磁石式吸着盤の場合に
は鉄板等の磁性体の吸着面とする。
Therefore, the suction cup 7 of the flying boat 78 is attached to the side of this floating pier 75.
In the case of pneumatic suction, it is a smooth suction surface, and in the case of electromagnetic suction cup, it is a suction surface for a magnetic material such as an iron plate.

この浮桟橋75はフロート部83によって水上に浮かん
でいるので為水位の変動で上下し−そのため岸壁74と
の橋絡部分の勾配ば85と86の点線で示すように変動
する。即ち港湾でちれば満潮と干潮によって変動し、干
満の差が多い所では5米以上も変化するので、この勾配
部はその変動程度に応−じて設計しなければならない。
Since this floating pier 75 is floating on the water by a float part 83, it moves up and down as the water level fluctuates; therefore, the slope of the bridge section with the quay wall 74 changes as shown by dotted lines 85 and 86. In other words, in a harbor, the slope changes depending on the high and low tides, and in places where there is a large difference between high and low tides, the slope can change by more than 5 meters, so this slope section must be designed according to the degree of fluctuation.

また貯水池等においても1河川流量の変化やダム放流等
により入水位は大幅に変る。
In addition, the water level in reservoirs, etc. can change significantly due to changes in river flow, dam discharge, etc.

しかし飛行艇78も水位の変動に応じて上下しているの
で1浮桟橋75との相対関係は変らずA常に一定の接舷
状態が保てるので支障はない。
However, since the flying boat 78 also moves up and down in response to changes in the water level, its relative relationship with the floating jetty 75 does not change, so there is no problem as a constant berthing state can always be maintained.

その他、この浮桟橋75には安全確保の手スリやへ雨天
時用の屋根84等も設けているが1その高さは飛行艇7
8の主翼に引っかからない高さとする。
In addition, this floating pier 75 is equipped with handrails to ensure safety and a roof 84 for use in rainy weather.
The height should be so that it does not get caught on the main wing of No. 8.

双胴型飛行艇を接岸させる場合には、第8図のように浮
桟橋を2本り双胴型飛行艇胴体内側間隔に余裕のあるよ
うに浮かべて置く。双胴型飛行艇はこの2本の浮桟橋9
7,98を真ん中にはさむように静かに接岸し1缶胴体
の艇首に付いている吸着盤91.92で岸壁]1】に吸
着係留し1次に右側胴体102は吸着盤93浮桟橋との
間にかけた梯子109又は110で昇降する。
When a twin-hulled flying boat is docked, two floating jetties are placed afloat with enough space between the insides of the twin-hulled flying boat as shown in Figure 8. The twin-hulled flying boat has these two floating piers 9
7 and 98 in the middle, and suction moored to the quay with suction cups 91 and 92 attached to the bow of the 1 can body. Go up and down using a ladder 109 or 110 placed between the two.

なお、104% 1051106はジェットエンジンを
示し1107 % 108は方向舵を示す。
Note that 104% 1051106 indicates a jet engine, and 1107% 108 indicates a rudder.

(9)  ジェット飛行艇の鳥害防止装置(特許請求の
範囲第9頂) 港湾や貯水池等には多数の水鳥が群がり住んでいるので
Aこれらの水鳥がジェット飛行艇のジェットエンジンに
吸い込まれないように\特別に対策を講する必要がある
(9) Bird damage prevention device for jet flying boats (claim 9) Since many waterbirds live in clusters in harbors, reservoirs, etc.A, these waterbirds are not sucked into the jet engines of jet flying boats. As such, special measures need to be taken.

そこで本発明は)第9図のように一ジェットエンジン1
13の空気吸入口の前に1ジエツトエンジン113の内
部のタービン・シャフトに直結したホーン状タービン1
12を取り付け1水烏115に突き当っても、この水鳥
115は矢印116の方向にはね飛げされ1ジエツトエ
ンジン113には吸い込まれないようにした。
Therefore, the present invention) has one jet engine 1 as shown in FIG.
A horn-shaped turbine 1 is directly connected to the turbine shaft inside the jet engine 113 in front of the air intake port 13.
12 is attached so that even if the water bird 115 collides with the water bird 115, the water bird 115 will be thrown away in the direction of the arrow 116 and will not be sucked into the jet engine 113.

このホーン状タービン112の羽根の角度方向は1第9
図のB図の断面部117に示す角度方向で一回転方向は
矢印120p方向であるから)空気−は尤の・タービン
117によって吸い込まれるので支障はない。
The angular direction of the blades of this horn-shaped turbine 112 is
Since the direction of one rotation in the angular direction shown in the cross section 117 in Figure B is the direction of the arrow 120p, there is no problem since the air is sucked in by the turbine 117.

ナオ)119バタービンシヤフト、118はホーン状タ
ービンの正面の半分を示しA114は主翼を示す。
119 is the front half of the horn-shaped turbine, and A114 is the main blade.

(発明の効果) 飛行艇に水中翼を装備し1気泡発生装置や水中スフリー
ラ装置により\飛行艇の離水滑走距離は大幅に短縮され
、飛行艇の着水時はh水中翼が水鳥の両足を広げて着水
するように作用してA飛行艇の着水衝撃を大幅に緩和し
\飛行艇の離着水性能を飛躍的に改善できても1これだ
けでは飛行艇を普及発展させる力とはなり得ず1飛行艇
の水上航行時の航空燃料節減対策や\接岸時の微細操舵
や、係留債の簡略化1人や荷物の積み降ろしの安全迅速
化等の諸1問題を解決しなければならなかったが1以上
の各発明により1これらの諸問題は基本的にはすべて解
決した。従って本発明により飛行艇の普及発展は大いに
期待できると思う。特に日本は海に囲まれた狭い島国で
あるから1今後の陸上飛行場の増設や拡張は困難となり
\都市のほとんどは海岸に集結しているので\飛行艇を
普及発展させれば1高速交通時代に最適の交通機関とな
る。また1南方の島国諸国との往来にも飛行艇は最適の
交通機関である。
(Effects of the invention) By equipping the flying boat with hydrofoils and using a bubble generator and an underwater squirrel device, the takeoff and run distance of the flying boat is greatly shortened, and when the flying boat lands on the water, the hydrofoils protect both legs of the waterfowl. Even if it spreads out and lands on the water, greatly mitigating the landing impact of the flying boat A, and dramatically improving the flying boat's takeoff and landing performance, this alone is not enough to popularize and develop flying boats. This cannot happen unless we solve various problems such as measures to save aviation fuel when an airship sails on water, fine-grained steering when docking, simplifying mooring for one person, and making loading and unloading safer and faster. However, one or more inventions have basically solved all of these problems. Therefore, I believe that the present invention can be highly expected to popularize and develop flying boats. In particular, since Japan is a narrow island nation surrounded by the sea, it will be difficult to build or expand land airfields in the future.Most of the cities are concentrated on the coast, so if flying boats are popularized and developed, it will become the era of high-speed transportation. It is the best means of transportation for Flying boats are also the best mode of transportation for traveling to and from the southern island nations.

水中に出し入れ可能で推進方向を自由に変えられる水中
スクリュウは、大型船舶にも利用すれば操舵が極めて容
易となり一接岸時のタッグボートも不要となる。
Underwater screws, which can be taken in and taken out of the water and can freely change the direction of propulsion, can be used on large ships, making steering extremely easy and eliminating the need for tug boats when berthed.

また1本発明の吸着係留装置は一飛行艇のみならず1普
通の船舶にも応用され1接岸係留に要する時間と労力は
大幅に削減されるでおろう。
Furthermore, the suction mooring device of the present invention can be applied not only to flying boats but also to ordinary ships, and the time and labor required for one berthing and mooring will be greatly reduced.

その他、いざ実施するとなれば種々の問題も生ずると思
われるが1それらの諸問題の解決はそれぞれの専門家の
解決に期待する。
In addition, various other problems are likely to arise if the project is to be implemented, and we hope that these problems will be resolved by experts in each area.

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

第1図は飛行艇用折りたたみ式扇形水中翼装置の構造を
示す原理図で、A図は水中翼を水中に出しだ状態の側面
図。B図は水中翼を収納箱に収納した状態を示す側面図
。0図は扇形水中翼を上から見た平面図。D図は水中翼
を収納箱に収納して下から見た状態の平面図。E図は水
中翼自体も折りたためる構造の平面図。2図はE図の水
中翼を折りたたんで収納箱に収納した状態を下から見た
平面図である。 1・・・扇形水中翼 2・・・支柱 7・・・摺動環 
5・・・摺動環駆動用連結棒 4・・・支柱折りたたみ
用連結棒 9・・・収納箱 10・・・飛行艇の接水底
面 11・・・折シたたみ水中翼第2図は本発明の諸装
置をジェット飛行艇の接水底面に装備した状態を示す一
実施例である。 15116・・・扇形水中g17X18・・・水中スク
リュウで矢印は推進方向を示す 19.20・・、主車
輪 21・・・前車輪 22X23・・・気泡放出口2
4)25・・・ジェットエンジン 第3図は双胴無尾翼型ジェット飛行艇の接水底面に1本
発明の諸装置を装備した状態を示す実施例図である。 26.27.28.29・・・水中翼 30\31・・
・水中スクリュウ 32,33・・・主車輪 34X3
5・・・前車輪 36.37.38.39・・・気泡放
出口 ・↓0X41s42・・・ジェットエンジン 4
3・・・操縦席胴体 44・・・左側胴体 45・・・
右側胴体第4図は水中スクリュウ装置の構造を原理的に
示しXA図は平面図)B図は水中スクリュウを水中に出
した状態を示す側面図。0図は水中スクリュウを収納箱
に収納した状態を示す側面図。 46・・・水中スクリュウ 47・・・水中スクリュウ
駆動部 48・・・サーボモーター 49・・・推進方
向変換用ギヤー 50・・・サーボモーター直結ギヤー
 52・・・水中スクリュウ装置支持金具54・・・収
納箱 56・・・スクリュウ収納連結棒第5図は空気式
吸着係留装置の構造を示す原理図である。 61・・・吸着盤 62・・・空気ノ々イブ 63・・
・排気ポンプ 64・・・開閉弁 65・・・繰り出し
装置 68・・・艇首カバー 第6図は本発明の吸着係留装置と飛行艇用浮桟橋を使用
した実施例を示す平面面で)第7図はその側面図である
。 71.72.73・・・吸着盤 75・・・飛行艇用浮
桟橋 77・・・浮桟橋出入口 79\80・・・翼端
フロート83・ ・・浮桟橋フロート 85・ ・・上
水位時の浮桟橋橋絡部の傾斜角度 86・・・低水位時
の浮桟橋橋絡部の傾斜角度 88・・・係留索89・・
・水底の係留ブロック 90・・・水底第8図は吸着係
留装置と浮桟橋を双胴型飛行艇の係留に応用した場合の
実施例を示す平面図で飄91.92.93へ94.95
.96・・・吸着盤 97.98・・・浮、桟橋 99
.100・・・浮桟橋出入口 101・・・操縦席胴体
 102.103・・・客席胴体 104110510
6・・・ジェットエンジン 107X108・・・方向
舵 109.110・・・操縦土用昇降はしご第9図は
ジェットエンジンの鳥害防止装置の原理ロー、ΔF71
I斤佃1而M1B図は正面図でちる。 112・ ・ ・鳥害防止用ホーン型タービン 113
・パジエノトエンジン 114・・・主翼115・・・
水鳥 116・・・水鳥の飛散方向 117・・・ホー
ン凰タービンの断面図 118・・・ホーン型タービン
の正面図119・・・タービンシャフト 120・・・
タービンの回転方向 (以上) 第1図(記号番号1〜14) 第5図(記号番号61〜70)
Fig. 1 is a principle diagram showing the structure of a foldable fan-shaped hydrofoil device for an airship, and Fig. A is a side view of the hydrofoil in a state in which it is extended into the water. Figure B is a side view showing the hydrofoil stored in the storage box. Figure 0 is a plan view of the fan-shaped hydrofoil seen from above. Figure D is a plan view of the hydrofoil stored in the storage box and viewed from below. Figure E is a plan view of the structure in which the hydrofoil itself can be folded. Figure 2 is a plan view of the hydrofoil shown in Figure E folded and stored in a storage box, viewed from below. 1... Fan-shaped hydrofoil 2... Strut 7... Sliding ring
5... Connecting rod for sliding ring drive 4... Connecting rod for folding struts 9... Storage box 10... Bottom surface in contact with the water of the flying boat 11... Figure 2 of the folding hydrofoil is in this book This is an embodiment showing the state in which various devices of the invention are installed on the water-contact bottom surface of a jet flying boat. 15116...Fan-shaped underwater g17X18...Underwater screw, arrow indicates propulsion direction 19.20..., Main wheel 21...Front wheel 22X23...Bubble release port 2
4) 25...Jet Engine FIG. 3 is an embodiment diagram showing a state in which various devices of the present invention are installed on the water-contact bottom surface of a twin-hulled tailless jet flying boat. 26.27.28.29...Hydrofoil 30\31...
・Underwater screw 32, 33...Main wheel 34X3
5...Front wheel 36.37.38.39...Bubble release port ・↓0X41s42...Jet engine 4
3...Cockpit fuselage 44...Left side fuselage 45...
Figure 4 of the right fuselage shows the principle of the structure of the underwater screw device, Figure XA is a plan view, Figure B is a side view showing the underwater screw taken out into the water. Figure 0 is a side view showing the underwater screw stored in the storage box. 46... Underwater screw 47... Underwater screw drive unit 48... Servo motor 49... Propulsion direction conversion gear 50... Servo motor direct connection gear 52... Underwater screw device support fitting 54... Storage box 56...Screw storage connecting rod FIG. 5 is a principle diagram showing the structure of the pneumatic adsorption mooring device. 61... Suction cup 62... Air nob 63...
・Exhaust pump 64... Opening/closing valve 65... Feeding device 68... Bow cover FIG. Figure 7 is a side view thereof. 71.72.73... Suction cup 75... Floating pier for flying boat 77... Floating pier entrance/exit 79\80... Wing tip float 83... Floating pier float 85... At water level Inclination angle of floating pier bridge section 86...Inclination angle of floating pier bridge section at low water level 88...Mooring cable 89...
・Bottom mooring block 90...Bottom bottom Figure 8 is a plan view showing an example of applying the suction mooring device and floating pier to the mooring of a twin-hulled flying boat.
.. 96... Suction cup 97.98... Floating, pier 99
.. 100... Floating pier entrance/exit 101... Cockpit fuselage 102.103... Passenger seat fuselage 104110510
6...Jet engine 107X108...Rudder 109.110...Control ladder
The M1B figure is a front view. 112・・・Horn type turbine for bird damage prevention 113
・Pazienoto engine 114...Main wing 115...
Waterfowl 116...Dispersal direction of waterfowl 117...Cross-sectional view of horn-shaped turbine 118...Front view of horn-type turbine 119...Turbine shaft 120...
Turbine rotation direction (and above) Figure 1 (symbol numbers 1 to 14) Figure 5 (symbol numbers 61 to 70)

Claims (9)

【特許請求の範囲】[Claims] (1)「昭和60年特許願第60−206601号」(
水中翼による水上飛行機及び飛行艇の離着水性能改善方
式)で特許出願中の水中翼の形状を扇形にしして、傘を
折りたたむように折りたためる構造とし、扇形水中翼の
支柱の飛行艇底部支持点を支点として後方に引き上げ、
折りたたんだ扇形水中翼を収納箱に収納する構造にした
ことを特徴とする、飛行艇用折りたたみ式扇形水中翼装
置。
(1) “Patent Application No. 60-206601 of 1985” (
A method for improving take-off and landing performance of seaplanes and flying boats using hydrofoils) The hydrofoils, which are patent pending, are shaped into a fan shape and have a structure that can be folded like folding an umbrella. Using the support point as a fulcrum, pull it up backwards,
A foldable fan-shaped hydrofoil device for an airship, characterized by having a structure in which the folded fan-shaped hydrofoil is stored in a storage box.
(2)空気圧縮ポンプで圧縮した空気を可撓パイプを通
じて飛行艇胴体前部及び中間部の接水底面の気泡放出口
に導びき、飛行艇の離水滑走時に、この気泡を飛行艇接
水底面に放出し、飛行艇の離水を容易にしたことを特徴
とする、気泡による飛行行艇の離水性能改善装置。
(2) Air compressed by an air compression pump is guided through a flexible pipe to the air bubble outlet on the bottom of the water-contacted surface of the front and middle parts of the fuselage of the flying boat, and when the flying boat takes off from water, the air bubbles are released from the bottom of the water-filled surface of the flying boat. A device for improving the take-off performance of a flying boat using air bubbles, characterized in that the air bubbles are emitted to facilitate the take-off of the flying boat.
(3)ジェットエンジン排気の一部を飛行艇の接水底面
に導びいた特許請求の範囲第2項の気泡による飛行艇の
離水性能改善装置。
(3) A device for improving the water take-off performance of a flying boat using air bubbles according to claim 2, wherein a part of the jet engine exhaust is guided to the water-contact bottom surface of the flying boat.
(4)操縦席からの遠隔監視制御によって推進方向を3
60度方向変換可能で、飛行中及び揚陸時は収納箱に収
納される水中推進機(水中スクリュウ)を飛行艇胴体の
前部と後部に各1ケづつ取り付け、水上航行時はこの水
中推進機で、航行して航空燃料を節約し、接岸時は操舵
を容易ならしめ、離水滑走時には飛行艇の主エンジンと
水中推進機を併用して離水性能を改善したことを特徴と
する、飛行艇の水中推進装置。
(4) Three propulsion directions are controlled by remote monitoring and control from the cockpit.
Underwater propellers (underwater screws), which can change direction by 60 degrees and are stored in a storage box during flight and landing, are attached to the front and rear of the airship's fuselage. This is a flying boat that saves aviation fuel by navigating on shore, makes it easier to steer when docking, and improves takeoff performance by using both the main engine of the flying boat and an underwater propulsion machine when taking off from water. Underwater propulsion device.
(5)排気ポンプで吸着力を保持する吸着盤を排気ポン
プに連結した可撓パイプの先端に接続した吸着係留装置
を飛行艇の艇首及び胴体側壁の数ケ所に取り付け、この
吸着盤を飛行艇用の接岸岩壁又は飛行艇用桟橋に圧着す
るだけで飛行艇が係留され、係留を解除する場合には可
撓パイプ中間の開閉弁を開くことにより容易に係留が解
除されることを特徴とする、飛行艇の吸着係留装置。
(5) A suction mooring device connected to the tip of a flexible pipe connected to the exhaust pump with a suction cup that maintains the suction force of the exhaust pump is attached to several locations on the bow and fuselage side wall of the flying boat, and this suction cup is attached to the airship during flight. A flying boat can be moored by simply crimping it on a rock wall for boats or a pier for flying boats, and when the mooring is to be released, the mooring can be easily released by opening the on-off valve in the middle of the flexible pipe. A suction mooring device for an airship.
(6)電磁石によって吸着する特許請求の範囲第5項の
飛行艇の吸着係留装置。
(6) The adsorption mooring device for an airship according to claim 5, which is adsorbed by an electromagnet.
(7)吸着係留装置を陸上岸壁側に設置し、飛行艇の吸
着係留を陸上岸壁側から操作する特許請求の範囲第5項
及び第6項の飛行艇の吸着係留装置。
(7) The suction mooring device for an flying boat according to claims 5 and 6, wherein the suction mooring device is installed on the land quay side and the suction mooring of the flying boat is operated from the land quay side.
(8)飛行艇用接岸岩壁から海面又は湖面方向に直角方
向に、フロートで水上に浮かぶ構造の細長い桟橋を水面
上に浮かべ、その桟橋の岸壁側には蝶番金具で橋絡桟橋
が連結され、さらにこの橋絡桟橋の他端は蝶番金具で岸
壁に連結され、水面上に浮かべた桟橋の他端は係留索で
水底の係留ブロックに係留し、この浮桟橋の側壁には特
許請求の範囲第5項又は第6項の吸着盤を吸着させる吸
着板を装備するか、又は特許請求の範囲第7項の吸着係
留装置の吸着盤を装備して、海面水位又は湖面水位の変
動に応じて飛行艇の接岸係留を迅速確実ならしめたこと
を特徴とする、飛行艇用浮桟橋。
(8) A long and narrow pier with a floating structure is floated on the water surface from the rock wall for flying boats at right angles to the sea surface or lake surface direction, and a bridge pier is connected to the quay side of the pier with hinges. Furthermore, the other end of this bridging pier is connected to the quay wall with a hinge, and the other end of the pier floating on the water surface is moored to a mooring block on the bottom of the water with a mooring cable, and the side wall of this floating pier is attached to the claim. Equipped with a suction plate that adsorbs the suction cup according to paragraph 5 or 6, or equipped with the suction cup of the suction mooring device according to claim 7, according to changes in sea level or lake water level. A floating pier for flying boats that is characterized by its ability to quickly and reliably moor the flying boat.
(9)ジェット飛行艇のジェットエンジンの空気吸入口
の前部に、ジェットエンジン・タービン・シャフトに直
結したホーン状タービンを取り付け、空気は十分に吸入
し海鳥などはジェットエンジンに吸い込まれないように
したことを特徴とする、ジェット飛行艇の鳥害防止装置
(9) Attach a horn-shaped turbine directly connected to the jet engine turbine shaft to the front of the air intake port of the jet engine of the jet flying boat to ensure that sufficient air is sucked in and seabirds are not sucked into the jet engine. Bird damage prevention device for jet flying boats.
JP7193486A 1986-03-28 1986-03-28 Departure and arrival performance improving auxiliary equipment for boat seaplane Pending JPS62227896A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7193486A JPS62227896A (en) 1986-03-28 1986-03-28 Departure and arrival performance improving auxiliary equipment for boat seaplane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7193486A JPS62227896A (en) 1986-03-28 1986-03-28 Departure and arrival performance improving auxiliary equipment for boat seaplane

Publications (1)

Publication Number Publication Date
JPS62227896A true JPS62227896A (en) 1987-10-06

Family

ID=13474838

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7193486A Pending JPS62227896A (en) 1986-03-28 1986-03-28 Departure and arrival performance improving auxiliary equipment for boat seaplane

Country Status (1)

Country Link
JP (1) JPS62227896A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008137506A (en) * 2006-12-01 2008-06-19 Fjc:Kk Vessel

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5643099A (en) * 1979-09-13 1981-04-21 Shin Meiwa Ind Co Ltd Preventive device for jump of aeroboat
JPS576571U (en) * 1980-06-12 1982-01-13
JPS59217819A (en) * 1983-05-23 1984-12-08 Mitsubishi Heavy Ind Ltd Electromagnetic type mooring arrangement
JPS62120292A (en) * 1985-11-20 1987-06-01 Hajime Kubo Device of introducing air to ship bottom

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5643099A (en) * 1979-09-13 1981-04-21 Shin Meiwa Ind Co Ltd Preventive device for jump of aeroboat
JPS576571U (en) * 1980-06-12 1982-01-13
JPS59217819A (en) * 1983-05-23 1984-12-08 Mitsubishi Heavy Ind Ltd Electromagnetic type mooring arrangement
JPS62120292A (en) * 1985-11-20 1987-06-01 Hajime Kubo Device of introducing air to ship bottom

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008137506A (en) * 2006-12-01 2008-06-19 Fjc:Kk Vessel

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