| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 1 | 飞艇 | CN201080057896.7 | 2010-10-12 | CN102753434A | 2012-10-24 | 巴普蒂斯特·雷加斯; 奥利维厄·乔扎恩 |
| 本发明涉及一种飞艇(1)，其包括没有刚性内结构且充填有比空气轻的气体的柔性罩(2)以及吊舱(3)。所述飞艇还包括将其安置于固体或液体表面的至少三个足部以及一个降落结构(5)。所述降落结构(5)位于柔性罩外，并将足部(6a，6b，6c)、吊舱(3)和罩(2)相连接。 | ||||||
| 2 | Airship Including Aerodynamic, Floatation, and Deployable Structures | US14058410 | 2013-10-21 | US20140231580A1 | 2014-08-21 | John Goelet |
| An airship is provided. The airship includes a hull configured to contain a gas, at least one propulsion assembly coupled to the hull and including a propulsion device, and at least one aerodynamic component including a plurality of fairing structures including one or more slats, wherein the at least one aerodynamic component is associated with the hull and is configured to direct airflow around the airship. | ||||||
| 3 | airship | JP2012533677 | 2010-10-12 | JP2013507293A | 2013-03-04 | レガス，バプティステ; ジョザン，オリビエ |
| 本発明は、剛性の内部構造を有さず、空気よりも軽い気体を格納する外皮（２）と、ゴンドラ（３）と、を備えた飛行船（１）に関するものである。 飛行船は、また、表面に到着できるようにするための３つの足と着陸構造体（５）とを備える。 着陸構造体（５）は、外皮の外側に位置し、足（６ａ，６ｂ，６ｃ）、ゴンドラ（３）、および外皮（２）の間に接続し、外皮（２）を取り囲む。 | ||||||
| 4 | AIRSHIP INCLUDING AERODYNAMIC STRUCTURES | EP12712835.3 | 2012-03-26 | EP2691295B1 | 2015-02-18 | GOELET, John |
| An airship is provided. The airship includes a hull configured to contain a gas, at least one propulsion assembly coupled to the hull and including a propulsion device, and at least one aerodynamic component including a plurality of fairing structures including one or more slats, wherein the at least one aerodynamic component is associated with the hull and is configured to direct airflow around the airship. | ||||||
| 5 | BALLON DIRIGEABLE. | EP10785104.0 | 2010-10-12 | EP2488409A1 | 2012-08-22 | REGAS, Baptiste; JOZAN, Olivier |
| The invention relates to an airship (1) including a flexible envelope (2) having no rigid inner structure containing a gas that is lighter than air, and a gondola (3). The balloon also includes three legs for setting the balloon on the surface and a landing structure (5). Said landing structure (5) is located on the outside of the envelope, and provides a connection between the legs (6a, 6b, 6c), the gondola (3) and the envelope (2) while surrounding the envelope (2). | ||||||
| 6 | Airship including aerodynamic, floatation, and deployable structures | US15242223 | 2016-08-19 | US09745042B2 | 2017-08-29 | John Goelet |
| An airship is provided. The airship includes a hull configured to contain a gas, at least one propulsion assembly coupled to the hull and including a propulsion device, and at least one aerodynamic component including a plurality of fairing structures including one or more slats, wherein the at least one aerodynamic component is associated with the hull and is configured to direct airflow around the airship. | ||||||
| 7 | AIRSHIP INCLUDING AERODYNAMIC, FLOATATION, AND DEPLOYABLE STRUCTURES | US15242223 | 2016-08-19 | US20160355248A1 | 2016-12-08 | John GOELET |
| An airship is provided. The airship includes a hull configured to contain a gas, at least one propulsion assembly coupled to the hull and including a propulsion device, and at least one aerodynamic component including a plurality of fairing structures including one or more slats, wherein the at least one aerodynamic component is associated with the hull and is configured to direct airflow around the airship. | ||||||
| 8 | Airship including aerodynamic, floatation, and deployable structures | US13430010 | 2012-03-26 | US08596571B2 | 2013-12-03 | John Goelet |
| An airship is provided. The airship includes a hull configured to contain a gas, at least one propulsion assembly coupled to the hull and including a propulsion device, and at least one aerodynamic component including a plurality of fairing structures including one or more slats, wherein the at least one aerodynamic component is associated with the hull and is configured to direct airflow around the airship. | ||||||
| 9 | Airship Including Aerodynamic, Floatation, and Deployable Structures | US13430010 | 2012-03-26 | US20120248241A1 | 2012-10-04 | John Goelet |
| An airship is provided. The airship includes a hull configured to contain a gas, at least one propulsion assembly coupled to the hull and including a propulsion device, and at least one aerodynamic component including a plurality of fairing structures including one or more slats, wherein the at least one aerodynamic component is associated with the hull and is configured to direct airflow around the airship. | ||||||
| 10 | Subsea deployment of aerial payloads utilizing long-term storage of lighter than air gases | US12835435 | 2010-07-13 | US08240602B1 | 2012-08-14 | Jeffrey M. Lloyd; Carol A. Becker; Brandon J. Wiedemeier; Jack Y. Dea; Rosteslaw M. Husar |
| A lighter than air (LTA) balloon and payload for the LTA balloon are stored on or in an underwater launcher. The launcher provides a source for a supply of a lighter than air gas, which is operatively connected to the LTA balloon until release. On deployment, the lighter than air gas is generated. The LTA balloon is deployed by activating the launcher to fill the LTA balloon and then releases the LTA balloon. | ||||||
| 11 | AIRSHIP INCLUDING AERODYNAMIC, FLOATATION, AND DEPLOYABLE STRUCTURES | US15675046 | 2017-08-11 | US20180050785A1 | 2018-02-22 | John GOELET |
| An airship is provided. The airship includes a hull configured to contain a gas, at least one propulsion assembly coupled to the hull and including a propulsion device, and at least one aerodynamic component including a plurality of fairing structures including one or more slats, wherein the at least one aerodynamic component is associated with the hull and is configured to direct airflow around the airship. | ||||||
| 12 | SAIL-EQUIPPED AMPHIBIOUS AEROSTAT OR DIRIGIBLE | US14157798 | 2014-01-17 | US20150203184A1 | 2015-07-23 | JOSEPH NILO SARMIENTO |
| A highly maneuverable craft or airship with aerostatic lift which may be manned or operated autonomously and remotely consists, in particular, a sail or similar device for main propulsion; the aerostat or dirigible sustains lift from gasbags containing helium or hydrogen or other similar lighter-than-air gas. Further, said aerostat may be mounted with a wind turbine for electrical power generation and mechanical operation; and, ballast tanks and landing gear to enable amphibious capability. | ||||||
| 13 | Airship | US13500744 | 2010-10-12 | US08783603B2 | 2014-07-22 | Baptiste Regas; Olivier Jozan |
| The invention relates to an airship including a flexible envelope having no rigid inner structure containing a gas that is lighter than air, and a gondola. The balloon also includes three legs for setting the balloon on the surface and a landing structure. The landing structure is located on the outside of the envelope, and provides a connection between the legs, the gondola and the envelope while surrounding the envelope. | ||||||
| 14 | Airship | US13500744 | 2010-10-12 | US20120199693A1 | 2012-08-09 | Baptiste Regas; Olivier Jozan |
| The invention relates to an airship including a flexible envelope having no rigid inner structure containing a gas that is lighter than air, and a gondola. The balloon also includes three legs for setting the balloon on the surface and a landing structure. Said landing structure is located on the outside of the envelope, and provides a connection between the legs, the gondola and the envelope while surrounding the envelope. | ||||||
| 15 | BALLON DIRIGEABLE. | EP10785104.0 | 2010-10-12 | EP2488409B1 | 2016-01-06 | REGAS, Baptiste; JOZAN, Olivier |
| 16 | AIRSHIP INCLUDING AERODYNAMIC, FLOATATION, AND DEPLOYABLE STRUCTURES | EP12712835.3 | 2012-03-26 | EP2691295A2 | 2014-02-05 | GOELET, John |
| An airship is provided. The airship includes a hull configured to contain a gas, at least one propulsion assembly coupled to the hull and including a propulsion device, and at least one aerodynamic component including a plurality of fairing structures including one or more slats, wherein the at least one aerodynamic component is associated with the hull and is configured to direct airflow around the airship. | ||||||
| 17 | NEW KIND OF AIRSHIPS OF THE FUTURE | PCT/AT2012000075 | 2012-03-22 | WO2012135876A3 | 2013-03-28 | KITA FIROOZ |
| An airship with a wide and flat, aircraft-like, not cigar-like, form, comprising a centrally arranged long fuselage and two wings, arranged on both sides of said fuselage, wherein a number of chambers or gas tanks that are delimited or separated from one another are provided, at least one, preferably more than one, in each of the two wings, and at least one means of propulsion, preferably a propeller, is provided in the front region and a means of propulsion is provided in the rear region of the airship, specifically on the upper side of the airship, wherein apertures or clearances, into or through which the means of propulsion can be pivoted or swung are formed in the airship or in the wings of the airship. | ||||||
| 18 | AIRSHIP INCLUDING AERODYNAMIC, FLOATATION, AND DEPLOYABLE STRUCTURES | PCT/US2012030562 | 2012-03-26 | WO2012135117A2 | 2012-10-04 | GOELET JOHN |
| An airship is provided. The airship includes a hull configured to contain a gas, at least one propulsion assembly coupled to the hull and including a propulsion device, and at least one aerodynamic component including a plurality of fairing structures including one or more slats, wherein the at least one aerodynamic component is associated with the hull and is configured to direct airflow around the airship. | ||||||
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