| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 81 | 一种遥控系留热气飞艇排气装置 | CN201220460259.0 | 2012-09-11 | CN202783766U | 2013-03-13 | 盛光喜; 贺应平; 薛富利; 王冰; 祝远程; 龚松洁 |
| 一种遥控系留热气飞艇排气装置，包括设置于艇囊上的排气口、设置于艇囊内壁的排气口盖布；排气口盖布经棉丝搭扣与排气口活动连接；排气口盖布固定连接有用于掀开排气口盖布排气的拉开绳；拉开绳从艇囊尾部伸出。当遥控系留热气飞艇快降落到地面时（距离地面5-10m），系留绳已不能工作，系留热气飞艇悬停在空中，通过拉开绳拉开排气口盖布，迅速将艇囊内热空气排出，使热气飞艇迅速降落，减少系留热气飞艇在降落时的留空时间，增强系统的安全性和可靠性。同时，排气口处于整个艇囊的后部，系留热气飞艇降落到地面时在外界风力作用下，能使飞艇内的空气通过排气口迅速排出，减少了人员手动排气的时间和劳动强度。 | ||||||
| 82 | 自带风扇散热的外转子电机和平流层飞艇 | CN201922102597.1 | 2019-11-28 | CN211046686U | 2020-07-17 | 段洣毅; 江京; 高鸿启; 邓迎春; 白贺冰 |
| 本实用新型提供一种自带风扇散热的外转子电机，包括内定子组件、外转子组件、内定子固定装置和外转子支撑装置；所述外转子组件包括永磁铁块、外转子、进风口风扇和出风口风扇，进风口风扇和出风口风扇分别固定在外转子沿轴向方向的两端，外转子、进风口风扇和出风口风扇形成腔室，并将内定子组件包围；进风口风扇与外转子支撑装置连接；永磁铁块设置在内定子组件相对应的外转子上；外转子绕着内定子组件旋转使电机工作，气流从进风口风扇进入腔室，从出风口风扇离开腔室，由此形成强迫空气对流，降低平流层上电机内部的温度，提升电机在平流层环境下持续工作的适应性。(ESM)同样的发明创造已同日申请发明专利 | ||||||
| 83 | 飞艇用超轻碳纤维复合隔热结构太阳能电池板 | CN202122573896.0 | 2021-10-25 | CN216054736U | 2022-03-15 | 武哲; 杨永强; 韩佳星; 彭钜锴; 卢小飞 |
| 本实用新型公开一种飞艇用超轻碳纤维复合隔热结构太阳能电池板包括太阳能电池板、碳纤维纸蜂窝复合镂空背板、碳管、隔热膜和芳纶纸蜂窝，所述太阳能电池板具有柔性，所述太阳能电池板安装于所述碳纤维纸蜂窝复合镂空背板的上侧，所述碳管安装于所述碳纤维纸蜂窝复合镂空背板的下侧，所述隔热膜和芳纶纸蜂窝均具有柔性，所述隔热膜的上侧与所述碳管连接，所述隔热膜的下侧与所述芳纶纸蜂窝连接。本实用新型的轻质飞艇具有质量轻、转换效率高和隔热性能高等优点。 | ||||||
| 84 | 一种平流层飞艇载荷舱电子设备热特性模拟与仿真预测系统与方法 | CN201610573005.2 | 2016-07-19 | CN106227060A | 2016-12-14 | 尹永利; 臧华兵; 高彦鹏; 田柳; 刘仁豪 |
| 一种平流层飞艇载荷舱电子设备热特性模拟与仿真预测系统与方法，其把低温低气压舱与飞行包线环境模拟参数控制算控制器结合，能极方便地依据飞行包线的输入，实现平流层飞艇全飞行阶段外部大气环境的动态变化模拟；将平流层飞艇载荷舱热网络模型的未知参数分为相对固定和随飞行高度H变化的参数，进行两段式模型参数辨识，提高了辨识收敛性和辨识结果的辨识精度；将相对固定的参数辨识结果作为下一个辨识过程的先验已知，显著提高了后一段参数辨识的精度。将第二段参数含有对流项参数的辨识结果拟合为飞行高度H的函数关系，有效提高了不同飞行剖面下设备温度预测的精度；针对单方程循环的参数辨识，大幅提高了参数辨识收敛性和辨识参数准确性。 | ||||||
| 85 | 一种应急热气飞艇浮空平台用涡轮基燃气发生器 | CN201120520587.0 | 2011-12-13 | CN202417714U | 2012-09-05 | 王毅; 张亚平; 郭颀; 缪海波; 杨尔卫 |
| 本实用新型为一种涡轮基燃气发生器，包括压气机、涡轮、燃烧室、点火器、液体氧化剂贮箱、液体燃料贮箱、电磁阀、富燃燃气发生器、波瓣掺混器、尾部整流器、控制器，是为应急热气飞艇浮空平台设计的新型吸气式涡轮基热力动力系统，具有寿命长、可靠性高、流量大、能量密度高、体积小和重量轻等特点，可满足应急热气飞艇浮空平台的快速升空和大负载能力的要求。 | ||||||
| 86 | Fuel cell for airship power generation and heating | PCT/US2004013895 | 2004-05-05 | WO2004100289A3 | 2005-11-10 | MCELROY JAMES FREDERICK; SRIDHAR K R |
| A neutrally buoyant airship, such as a blimp, contains a lifting body which allows the airship to remain neutrally buoyant in air and a fuel cell located in the airship. A method of generating power in the neutrally buoyant airship, comprising providing a fuel and a oxidizer to a solid oxide fuel cell to generate power, and providing heat from the fuel cell to a remotely located lifting body, wherein the lifting body allows the airship to remain neutrally buoyant in air. | ||||||
| 87 | 열 발생장치를 내장한 비행선장치 | KR2020010030521 | 2001-10-06 | KR200262005Y1 | 2002-02-06 | 김진경 |
| 본 고안은 부양가스 주머니(1)에 태양전지 모듈(2)이나, 엔진(30)의 추진력에 의한 발전기(31)로 발생한 전기에너지가, 비행선의 중앙에 위치한 보조주머니(40) 내부에 설치한 저항선장치(10)나 조명등장치(15)에서 열에너지로 변환되어, 보조주머니(40) 및 비행선 전체의 부양가스 주머니(1)를 팽창시켜서 비행선이 쉽게 뜨도록 한다. 또 저항선장치(10)나 조명등장치(15)로 가는 전력을 차단하면 보조주머니(40) 및 비행선 전체의 부양가스 주머니(1)를 수축시켜서 비행선이 쉽게 가라앉도록 한다. 본 고안의 비행선장치는 일반 비행선의, 공기와 부력이 비슷한 상태에서 날개의 양력이나 공기주머니라는 덤을 사용하지 않으며, 주변 기온이 차가운 환경에 쉽게 적용할 수 있기 때문에, 상층해야할 거리가 높고 기온이 차가운 성층권에 비행선을 뜨게 하거나 가라앉게 하는데 유리하고, 또한 장기간 비행선을 운용해야할 때 유리하다. | ||||||
| 88 | Radiator system for airships | US39261329 | 1929-09-14 | US1779898A | 1930-10-28 | LOUIS BREGUET |
| 89 | Moteur d'aéronef équipé de moyens d'échange thermiques | EP08151972.0 | 2008-02-27 | EP1967716B1 | 2016-05-18 | BRAULT, Michel; ROUSSELIN, Stéphane; TANTOT, Nicolas; TOURET, Roxane |
| 90 | Fuel cell for airship power generation and heating | US10428804 | 2003-05-05 | US20030207164A1 | 2003-11-06 | James Frederick McElroy; K.R. Sridhar |
| A neutrally buoyant airship, such as a blimp, contains a lifting body which allows the airship to remain neutrally buoyant in air and a fuel cell located in the airship. A method of generating power in the neutrally buoyant airship, comprising providing a fuel and a oxidizer to a solid oxide fuel cell to generate power, and providing heat from the fuel cell to a remotely located lifting body, wherein the lifting body allows the airship to remain neutrally buoyant in air. | ||||||
| 91 | Fuel cell for airship power generation and heating | US10428804 | 2003-05-05 | US06908702B2 | 2005-06-21 | James Frederick McElroy; K. R. Sridhar |
| A neutrally buoyant airship, such as a blimp, contains a lifting body which allows the airship to remain neutrally buoyant in air and a fuel cell located in the airship. A method of generating power in the neutrally buoyant airship, comprising providing a fuel and a oxidizer to a solid oxide fuel cell to generate power, and providing heat from the fuel cell to a remotely located lifting body, wherein the lifting body allows the airship to remain neutrally buoyant in air. | ||||||
| 92 | Fuel cell for airship power generation and heating | US10853194 | 2004-05-26 | US20040245385A1 | 2004-12-09 | James Frederick McElroy; K.R. Sridhar |
| A neutrally buoyant airship, such as a blimp, contains a lifting body which allows the airship to remain neutrally buoyant in air and a fuel cell located in the airship. A method of generating power in the neutrally buoyant airship, comprising providing a fuel and a oxidizer to a solid oxide fuel cell to generate power, and providing heat from the fuel cell to a remotely located lifting body, wherein the lifting body allows the airship to remain neutrally buoyant in air. | ||||||
| 93 | Deflation cap for pressurized hot air airship | US654858 | 1976-02-03 | US4033527A | 1977-07-05 | Roger R. Parsons |
| A hot air airship including an elongate aerodynamic shaped gas envelope carrying a pressure hot air generator system for pressurizing the envelope with heated air during flight with tail members at the aft end of the airship for guiding and directing the direction and attitude of flight, a gondola supported from the envelope for carrying the load including a push fan for propelling it in flight, a pressurizing blower and hot air generator for carrying with the ship, a deflation opening in the airship envelope having a cap over the elongate envelope with a netting sewn over the opening outwardly of the cap and the cap attached by Velcro along its edges and permanently attached at side edges so that the fore and aft edges can be pulled away from the opening. | ||||||
| 94 | Redundant blower drive for pressurized hot air airship | US676246 | 1976-04-12 | US4018406A | 1977-04-19 | Roger R. Parsons |
| A thermal airship including an elongate gas envelope of a soft flexible material with tail members on the aft end of the airship, a gondola carried below the airship hull, a first motor driving a propeller for propelling the airship horizontally, a pressurizing inflation leading into the hull, an air pressure generating mechanism for pressurizing the envelope with heated air during flight including a blower driven by a second motor positioned for moving a flow of air through the opening with a controlled burner positioned in the path of the flowing air, a drive train connected between the first motor and blower and a drive train clutch in the drive train for connecting the blower to be driven by the first motor in the event of failure of the second motor. | ||||||
| 95 | Apparatus providing heat, light, and radio service for airships | US28002928 | 1928-05-23 | US1709684A | 1929-04-16 | PAUL POSSIN |
| 96 | Piezoelectric and pyroelectric power-generating laminate for an airship envelope | US12011509 | 2008-01-28 | US07878453B2 | 2011-02-01 | Paul E. Liggett |
| A power-generating laminate for an airship comprises a base fabric layer, a barrier layer disposed upon the fabric layer, an inner metal film layer disposed upon the barrier layer, a piezoelectric/pyroelectric layer disposed upon the inner metal layer, an outer metal layer disposed upon the piezoelectric/pyroelectric layer, and a cover layer disposed upon the outer metal layer. The power-generating laminate forms a gas-impervious envelope to maintain lifting gas and air therein, and is configured such that when the envelope is subjected to structural strain or experiences changes in temperature, power is generated, which is used to supply power to the various electrical systems aboard the airship. | ||||||
| 97 | Piezoelectric and pyroelectric power-generating laminate for an airship envelope | US12011509 | 2008-01-28 | US20090189012A1 | 2009-07-30 | Paul E. Liggett |
| A power-generating laminate for an airship comprises a base fabric layer, a barrier layer disposed upon the fabric layer, an inner metal film layer disposed upon the barrier layer, a piezoelectric/pyroelectric layer disposed upon the inner metal layer, an outer metal layer disposed upon the piezoelectric/pyroelectric layer, and a cover layer disposed upon the outer metal layer. The power-generating laminate forms a gas-impervious envelope to maintain lifting gas and air therein, and is configured such that when the envelope is subjected to structural strain or experiences changes in temperature, power is generated, which is used to supply power to the various electrical systems aboard the airship. | ||||||
| 98 | Blower and burner to produce superpressure in a thermal airship | US687913 | 1976-05-19 | US4076188A | 1978-02-28 | Douglas B. Obermoller |
| A thermal airship including an elongate gas envelope of a soft material providing a hull for the airship with tail members, a gondola carried below the hull, a power propelling system supported by the hull and a system for pressurizing the soft envelope through an inflation opening with the gondola adjoining the hull surrounding the inflation opening in a sealed manner. The system for pressurizing includes a blower mounted on the hull extending through the opening and directing a flow of air past a burner within the interior of the envelope and a lateral baffle between the burner and blower deflecting an amount of the air from the blower laterally directly into the envelope interior. | ||||||
| 99 | Pressure and hot air relief vents for a pressurized hot air airship | US670183 | 1976-03-25 | US4090682A | 1978-05-23 | Roger R. Parsons |
| In a hot air airship including an elongate gas envelope aerodynamically shaped for horizontal flight with a pressure hot air generator for pressurizing the envelope and tail members on the envelope, a gondola below the envelope and power driven member for propelling the envelope horizontally, a method and structure for releasing over pressure from the airship envelope and for regulating its ascent and descent by a variably controllable first vent in the front end of the airship and a second variably controllable vent at the aft end of the airship, each of which functions to release air at a controlled rate to cause heated air to move toward either end and cause either end to ascend. | ||||||
| 100 | 参数自适应的单囊体平流层飞艇浮重平衡评估方法 | CN202011411705.4 | 2020-12-03 | CN112487559A | 2021-03-12 | 耿宝刚; 张永栋; 叶虎; 李敏; 姚璇; 宁辉; 张莉; 阴鹏 |
| 本发明涉及平流层飞艇技术领域，提供一种参数自适应的单囊体平流层飞艇浮重平衡评估方法，首先根据遥测数据，实时获取飞艇的压力和温度参数，计算飞艇内部氦气质量、拟合飞艇的氦气泄漏率；然后基于平流层飞艇的热力学环境构建单囊体平流层飞艇热力学模型，利用关键参数的在线修正值，计算和预估不同时刻平流层飞艇内部氦气的温度；再次进行单囊体平流层飞艇压差的计算；最后利用飞艇压差，完成对飞艇浮重的在线评估。本发明基于氦气的泄漏状态，可预估飞艇的后续可驻空时长，为飞艇的飞行决策提供了有力的支持。 | ||||||
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