| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 41 | Free skydiving simulated experiencing device | JP28334796 | 1996-10-04 | JPH10109696A | 1998-04-28 | KOARAI GENICHI; FUJISHIRO TAIICHIRO; MATSUMOTO NAOYUKI; OZAKI HIROYUKI |
| PROBLEM TO BE SOLVED: To provide a free skydiving simulated experiencing device which corrects a drop in flow speed at the outer circumferential peripheral part of ascending current, and thereby actualize stable diving therein. SOLUTION: Auxiliary air jet nozzles 27 are provided toward an exhaust port 26 for the wall surface part at the circumferential side of a floating space 23, concurrently the auxiliary air jet nozzles 27 are connected to the downstream position of an air blower 52 in an air blasting passage 50 because of a bypass passage 29, and it is so constituted that the speed distribution at the circumferential peripheral part of ascending current within the floating space 23 can be changed so as to be adjusted by means of an air flow spouted out of the auxiliary air jet nozzles 27 while air is being fed by way of the bypass passage 29. COPYRIGHT: (C)1998,JPO | ||||||
| 42 | Recreation facilities | JP26817689 | 1989-10-17 | JPH03131289A | 1991-06-04 | NAKAYORI MASAMI |
| PURPOSE: To contrive to lighten the rotation load of fans by connecting a facility for using the energy of a heavy wind to exhaust nozzles for taking out a part of the heavy wind to the outside in the middle part of the flow of the heavy wind provided in a skydiving facility through causing the wind energy-using facility to communicate with the exhaust nozzles. CONSTITUTION: A skydiving facility 2 is doughnut-shaped, and its internal passage is formed in a circulating manner and equipped with skydiving fans 4, 4,.... Further, the facility 2 is provided with exhaust nozzles 7, 7... in the middle part of the passage. These exhaust nozzles 7 take out a part of the current of air flowing through the facility 2 to jet the air current into a marine facility 3 and is provided with guide plates 8, 8... for the air current. In the marine facility 3, this wind is used, e.g. to sail yachts 13 and to play windsurfing. Thus, it is possible to lighten the load of fans for making a heavy wind. COPYRIGHT: (C)1991,JPO&Japio | ||||||
| 43 | JPS60501353A - | JP50322182 | 1982-10-20 | JPS60501353A | 1985-08-22 | |
| 44 | WIND TUNNEL TURNING VANE HEAT EXCHANGER | EP11702317.6 | 2011-01-15 | EP2524199B1 | 2018-05-02 | METNI, N, Alan; ARLITT, Mark |
| A cooling system for a wind tunnel (100) is disclosed. The heat exchanger (200) of the present disclosure is formed as a turning vane assembly in an airflow duct of a re-circulating wind tunnels. The individual vanes (201) are formed from extruded aluminum with coolant fluid channels (206, 207, 208) running continually down the length of the vane. One or more channels can be used, depending on the application of vane and the cooling capacity needed. The exterior of the vanes are formed in an airfoil shape to efficiently turn the air flow the de-sired amount in a manner well known in the art. The turning vanes are connected to a fluid supply (204) with single piece connectors (202) that removably attach to the turning vanes. In the depicted embodiment the connectors are attached with screws. In the depicted embodiment the connectors are formed as a single piece in a two-piece injection mold. | ||||||
| 45 | WIND TUNNEL TURNING VANE HEAT EXCHANGER | EP11702317.6 | 2011-01-15 | EP2524199A1 | 2012-11-21 | METNI, N, Alan; ARLITT, Mark |
| A cooling system for a wind tunnel (100) is disclosed. The heat exchanger (200) of the present disclosure is formed as a turning vane assembly in an airflow duct of a re-circulating wind tunnels. The individual vanes (201) are formed from extruded aluminum with coolant fluid channels (206, 207, 208) running continually down the length of the vane. One or more channels can be used, depending on the application of vane and the cooling capacity needed. The exterior of the vanes are formed in an airfoil shape to efficiently turn the air flow the de-sired amount in a manner well known in the art. The turning vanes are connected to a fluid supply (204) with single piece connectors (202) that removably attach to the turning vanes. In the depicted embodiment the connectors are attached with screws. In the depicted embodiment the connectors are formed as a single piece in a two-piece injection mold. | ||||||
| 46 | Wind tunnel skydiving simulator | EP09165707.2 | 2005-08-01 | EP2113458B1 | 2012-11-14 | Metni, N. Alan; Kitchen, William J.; Mort, Kenneth W.; Eastlake, Charles N.; Palmer, Michael J. |
| 47 | RECIRCULATING VERTICAL WIND TUNNEL SKYDIVING SIMULATOR AND REDUCED DRAG CABLE FOR USE IN WIND TUNNELS AND OTHER LOCATIONS | EP05803928.0 | 2005-08-01 | EP1819592B1 | 2012-04-04 | METNI, N. Alan; KITCHEN, William, J.; MORT, Kenneth, W.; EASTLAKE, Charles, N.; PALMER, Michael, J. |
| A vertical wind tunnel flight simulator comprises a flight chamber wherein a flier may experience a freefall simulation. Airflow to support the flier is induced by fans connected above the flight chamber through a duct. A staging area having openings to the flight chamber is adjacent to the flight chamber. One or two return air ducts are used to return air from the fans outlet to the fans inlet. Opposed louvers are included on at least one duct segment thereby regulating the temperature via forcing ambient air into the simulator. The use of many duct segments having diverging walls adds commercial value to the system by lowering the height. Mounting components on the roof and behind walls creates a spectacular pedestrian viewing scene of people in flight. | ||||||
| 48 | IMPROVED PANORAMIC, VERTICAL WIND TUNNEL | EP06841740.1 | 2006-12-15 | EP1964776A1 | 2008-09-03 | SERRANO, Miguel Angel |
The invention refers to a wind tunnel designed to operate in its vertical section that is to say, air currents generated by appropriate means meeting in a vertical area at the end of which the air current is capable of lifting objects in this vertical area. At the same time this lifting effect may be seen on the outside as it has been built from translucent materials. The viewing and lifting of bodies in this device allows both their display and measurements to be taken. |
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| 49 | SKYDIVING TRAINER WINDTUNNEL | EP96910369 | 1996-03-01 | EP0813728A1 | 1997-12-29 | KITCHEN WILLIAM J; BIRD KENNETH G |
| A skydiving simulator (1) combines a vertical air chamber (4) with a video projection system (6) on the interior wall (22). A virtual reality environment is created as the skydiver, while suspended, sees actual film footage of scenarios descending toward earth. A skydiver backpack (50) houses a transmitter (54) which interactively steps the skydiver through emergency procedures. | ||||||
| 50 | 垂直風洞スカイダイビングシミュレータ | JP2017555229 | 2016-04-22 | JP2018522599A | 2018-08-16 | ロマネンコ ルスラン; パーマニン アレクサンドル; イボニンスキー アレクサンドル; スブヤトスラフ リシン; サブチェンコ イバン; シャロフ イエブゲーニ |
| 垂直風洞スカイダイビングシミュレータは、待機空間内に延びる湾曲した気流偏向器を有する飛行空間入口を含み、飛行空間入口では、湾曲した気流偏向器の凸面が飛行空間入口を挟んで向き合うもしくは飛行空間入口を向くか、または飛行空間の内側を向き、待機空間に入る乱流の流れを大幅に低減するのに十分な距離ほど待機空間内に延びる。湾曲面は入口の最上部にあり、両側にあってもよい。湾曲面の範囲及び厳密な形状は様々な要素によるが、主な原則として、待機空間に入る乱流の流れを最小化するのに十分でなければならず、待機エリアにいる人にとってより快適であり騒音が少ない効果を有する。さらに湾曲面は、たとえ乱流ではない空気の層流が飛行空間入口を越えたとしても、飛行空間に保つよう促す。これにより、飛行はより快適で予測可能になる。 【選択図】図5 |
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| 51 | 循環式垂直風洞スカイダイビングシミュレータ | JP2013024136 | 2013-02-12 | JP5864450B2 | 2016-02-17 | メトニ,エヌ・アラン; キッチン,ウィリアム; モルト,ケネス・ダブリュー; イーストレイク・チャールズ・エヌ; パーマー,マイケル・ジェイ |
| 52 | 船、特にクルーズ船 | JP2015530292 | 2013-09-04 | JP2015527250A | 2015-09-17 | クルヒ、ティム |
| 少なくとも1つの露天甲板(2)と、該露天甲板(2)に隣接する構造体(4,5)とを有する船、特にクルーズ船において、露天甲板(2)上には、垂直方向に向いた風洞(3)が設けられており、該風洞には、上向きの気流によって、パラシュート降下および/または飛行体験がシミュレート可能である。風洞の上方の端部領域から流れ出る空気は、露天甲板(2)に隣接する構造体に構造的に統合された循環流路(6,16)を通って、戻される。【選択図】図1 | ||||||
| 53 | Improved panoramic vertical wind tunnel | JP2008546493 | 2006-12-15 | JP2009520967A | 2009-05-28 | ぺリセール，ミゲル アンゲル セラーノ |
| 【解決手段】本発明は風洞に関する。 本発明によれば、設計された風洞の効果はその垂直部でみられ、すなわち適切な手段により発生させた気流は垂直端部の領域に合流する。 気流は垂直領域で物体を持ち上げることができ、持ち上げられた物体は、前記垂直部が半透明の材料から構成されているので外部から見ることができる。 このようにして、組立体を通して物体の上昇を見ることができ、測定することができる。 | ||||||
| 54 | Sky diving simulator and sky diving training method using it | JP2002576104 | 2002-03-21 | JP2004519730A | 2004-07-02 | ビョンホ パク; ソンテ リ |
| 本発明の目的は、スカイダイバーが飛行機に搭乗する最初の段階から地上へ着地する最後の段階までの実際のスカイダイビングの過程をあたかも行ったかのようなスカイダイビングの訓練を目的とする環境及びその他の状況をシミュレーションスカイダイビングシミュレーター及びシミュレーターを使用したスカイダイビング訓練方法を提供することである。 このシミュレーターは、飛行機胴体（１０）と、飛行機胴体から飛び降りたスカイダイバーを支える回転吊り下げ部（３０）と、スカイダイバーが飛行機胴体から飛び降りる開放されたシミュレーション空間に水平方向および上方向の空気の流れを送風する二つの送風機部（４０、５０）と、により構成される。 風速感知器（４６、５６）は二つの送風機部からの空気の流れの速度を感知し、ＣＣＤカメラ（４７、５７）は訓練過程中のスカイダイバーの映像を生成し、中央制御手段（ＣＣＵ、６０）はシミュレーター及び過程を実時間で制御する。 | ||||||
| 55 | Wind tunnel device | JP14889096 | 1996-06-11 | JPH09327540A | 1997-12-22 | KIMURA YOSHIKAZU; NAKANO SUSUMU |
| PROBLEM TO BE SOLVED: To provide a wind tunnel device capable of performing practice for a cross wind in skydiving or the like as well by installing a mechanism capable of generating an air flow provided with the component of the cross wind in a test part in the wind tunnel device used for leisure such as the skydiving or the like for which a jetting port is installed to jet the air flow from down to up. SOLUTION: This wind tunnel device for the skydiving is composed of a blower 1, a conductor 4 for guiding the air flow to a nozzle 2, the nozzle 2 installed so as to accelerate the air flow accompanying the reduction of an area in a reduction flow passage and to jet the air flow upwards, the test part 3 for shielding gas jetted through the nozzle 2 from the outside air and performing the practice of the skydiving and an exhaust system. The centers of plural louvers 10 for changing the angle of the flowing direction of the air flow are installed to the nozzle 2 in a rotatable state and the lower ends or upper ends of the plural louvers 10 are connected by a louver connection material 11. The louver connection material 11 moves the louvers 10 by a hydraulic driving mechanism. COPYRIGHT: (C)1997,JPO | ||||||
| 56 | JPS633630B2 - | JP3500882 | 1982-03-05 | JPS633630B2 | 1988-01-25 | JAN SANNJIRUMAN |
| 57 | Space float field | JP3500882 | 1982-03-05 | JPS5832789A | 1983-02-25 | JIYAN SANNJIRUMAN |
| 58 | WIND TUNNEL SKYDIVING SIMULATOR | US16318810 | 2017-07-21 | US20190219476A1 | 2019-07-18 | Ruslan ROMANENKO; Alexandr PARMANIN; Aleksandr IVONINSKII; Svjatoslav LISIN; Ivan SAVCHENKO |
| A wind tunnel skydiving simulator including a flight chamber that includes a section that is inclined to the vertical. For example, it can be curved in the vertical plane, and the shape of the curve is then a smooth transition from approximately horizontal to approximately vertical. This enables the skilled sportsperson to practice wingsuit gliding and other sports where there is substantial forward motion through fast moving air—something impossible with a conventional vertical wind tunnel skydiving simulator. With this invention, the air flowing past the flyer can hence include a substantial, sustained (for many minutes) horizontal, relative component—making wingsuit flying possible. | ||||||
| 59 | VERTICAL WIND TUNNEL SKYDIVING SIMULATOR | US15951568 | 2018-04-12 | US20180229130A1 | 2018-08-16 | Ruslan ROMANENKO; Alexandr PARMANIN; Aleksandr IVONINSKII; Svjatoslav LISIN; Ivan SAVCHENKO; Eugeny SHAROV |
| A vertical wind tunnel skydiving simulator including a flight chamber entrance that has a curved air deflector that extends into a waiting chamber, in which a convex surface of the curved air deflector faces across or towards the flight chamber entrance or into the flight chamber, and extends into the waiting chamber a sufficient distance to substantially reduce the flow of turbulent air into the waiting chamber. The curved surface is at the top of the entrance and can also be at the sides. The shape the curved surface takes is sufficient to minimize the flow of turbulent air into the waiting chamber; the effect is to make it more comfortable and less noisy for people in the waiting area. This also helps to preserves the laminar, non-turbulent flow of air in the flying chamber, even across the flight chamber entrance. This makes flying more comfortable and predictable. | ||||||
| 60 | VERTICAL WIND TUNNEL SKYDIVING SIMULATOR | US15789234 | 2017-10-20 | US20180050276A1 | 2018-02-22 | Ruslan ROMANENKO; Alexandr PARMANIN; Aledsandr IVONINSKII; Svjatoslav LISIN; Ivan SAVCHENKO; Eugeny SHAROV |
| A vertical wind tunnel skydiving simulator including a flight chamber entrance that has a curved air deflector that extends into a waiting chamber, in which a convex surface of the curved air deflector faces across or towards the flight chamber entrance or into the flight chamber, and extends into the waiting chamber a sufficient distance to substantially reduce the flow of turbulent air into the waiting chamber. The curved surface is at the top of the entrance and can also be at the sides. The shape the curved surface takes is sufficient to minimize the flow of turbulent air into the waiting chamber; the effect is to make it more comfortable and less noisy for people in the waiting area. This also helps to preserves the laminar, non-turbulent flow of air in the flying chamber, even across the flight chamber entrance. This makes flying more comfortable and predictable. | ||||||
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