公开(公告)号：JP4603222B2

公开(公告)日：2010-12-22

申请号：JP2001533020

申请日：2000-10-23

Applicant: フランツ・ブーヒャー

Inventor： フランツ・ブーヒャー

IPC: B64D27/24 ,  B64C29/00 ,  B64C39/00 ,  B64C39/06 ,  B64D31/12

CPC classification number: B64C29/0033 ,  B64D27/24 ,  Y02T50/62

公开(公告)号：JP4359239B2

公开(公告)日：2009-11-04

申请号：JP2004540701

申请日：2003-09-25

Applicant: ヴァゲルズ、ディーター

Inventor： ヴァゲルズ、ディーター

IPC: B64C29/00 ,  A63G31/00 ,  B64C15/00 ,  B64C39/00

CPC classification number: B64C39/001 ,  A63G31/00

公开(公告)号：JP2008106619A

公开(公告)日：2008-05-08

申请号：JP2006287514

申请日：2006-10-23

Applicant: Kansai Electric Power Co Inc:The ,  関西電力株式会社

Inventor： OGAWA MASARU

IPC: F03D11/00 ,  B64C23/08 ,  B64C39/00 ,  F03D1/06 ,  F03D7/02

CPC classification number: Y02E10/721 ,  Y02E10/723

Abstract: PROBLEM TO BE SOLVED: To attain improvement of dynamic lift of a wind power generator and an aircraft by developing a wing shape capable of generating the dynamic lift over low to high wind speed areas since in a conventional fixed wing, the dynamic lift is large at the high wind speed area but the dynamic force at the low/middle wind speed area is small and the dynamic lift by magnus effect is large at the low/middle wind speed area but a magnus cylinder becomes air resistance at the high wind speed area.
SOLUTION: The composite magnus type wing generates the dynamic lift of the fixed wing and the magnus force by mounting the rotation magnus cylinder to a middle of the fixed wing. The composite wing can generate the dynamic lift in a wide range from the low wind speed area to the high wind speed area by the dynamic lift by the magnus force at the low wind speed area and the dynamic lift by the fixed wing at the high wind speed area. Power generation at the wider wind speed area than conventional becomes possible by adopting it to a rotation wing of the wind power generator and performing control of the rotation number of the magnus wing. If it is adopted for the wing of the aircraft, it becomes a short fixed wing and taking off/landing in a short distance becomes possible.
COPYRIGHT: (C)2008,JPO&INPIT

Abstract translation: 要解决的问题：为了通过开发能够在低到高风速区域上产生动态升力的机翼形状来改善风力发电机和飞行器的动态升力，因为在常规的固定翼中，动态升力 在高风速区域较大，但低/中风速区域的动力较小，低风/中风速区域的大功率动力提升较大，而大气压气缸在高风区时变为空气阻力 速度区。

解决方案：复合马力型翼片通过将旋转马力缸安装到固定翼的中间，产生固定翼的动力提升和马力。 复合翼可以通过在低风速区域的大力矩的动力升高和高风时的固定翼的动力提升，从低风速区域到高风速区域产生宽范围的动力升力 速度区。 通过将其应用于风力发电机的旋转翼并执行马蹄翼的旋转数量的控制，可以在比常规更宽的风速区域发电。 如果采用飞机的机翼，它就变成一个很短的固定翼，而且在短距离内起飞/着陆是可能的。 版权所有（C）2008，JPO＆INPIT

公开(公告)号：JP2006315647A

公开(公告)日：2006-11-24

申请号：JP2005170071

申请日：2005-05-16

Applicant: Keigoro Shigiyama ,  桂五郎 鴫山

Inventor： SHIGIYAMA KEIGORO ,  NAGAI KOICHIRO ,  TORITANI KATSUYUKI

IPC: B64C39/00 ,  B64B1/40 ,  B64D27/02

CPC classification number: Y02T50/44

Abstract: PROBLEM TO BE SOLVED: To reduce noise and eliminate an exhaust gas and to realize energy-saving as a conventional light aircraft or a helicopter or further as an aircraft for air transportation not competing in speed, monitoring and service from the air above in an agriculture and forestry fishing industry and sight-seeing by attaching a wave motion propelling unit to it.
SOLUTION: The conventional engine, motor, transmission mechanism or the like are not required. (1) A wing surface itself is made to a bendable [wave motion piezoelectric membrane/wave motion piezoelectric surface] by application of a piezoelectric body. (2) The same membrane surface is made complementary to increase thrust and is attached to a gliding object to realize self-actuated flight. (3) It is made to a multiple wave motion piezoelectric surface to create a blown wing upper surface laminar flow and vertical taking off/landing is realized. Other required articles are a solar battery, a secondary battery and an electronic circuit for piezoelectric surface driving. It is light weight, flight at high height is realized and manufacturing of a large size aircraft can be realized. Mass transportation becomes possible utilizing the prevailing westerlies.
COPYRIGHT: (C)2007,JPO&INPIT

Abstract translation: 要解决的问题：为了减少噪音和排除废气，并将传统的轻型飞机或直升机或进一步作为航空运输的飞机实现节能，而不是以上述方式从空中竞争的速度，监视和服务 在农业和林业渔业中，通过附加一个波浪运动推动装置观察。 解决方案：不需要传统的发动机，电动机，变速机构等。 （1）通过施加压电体，将翼面本身制成为可弯曲的[波动压电膜/波动压电面]。 （2）相同的膜表面互补，增加推力，并附着在滑翔物体上，实现自行程飞行。 （3）制成多波动压电表面，形成吹风翼面上层流层，实现垂直起降。 其他需要的物品是太阳能电池，二次电池和用于压电表面驱动的电子电路。 重量轻，实现高高度飞行，实现了大型飞机的制造。 大众运输成为可能利用盛行的西风。 版权所有（C）2007，JPO＆INPIT

公开(公告)号：JP2006103652A

公开(公告)日：2006-04-20

申请号：JP2004322911

申请日：2004-10-07

Applicant: Tomoyasu Yoko ,  Tomoyasu Yutaka ,  友安 裕 ,  友安 陽子

Inventor： TOMOYASU YOSHIOKI

IPC: B64C39/00 ,  B64C29/00

Abstract: PROBLEM TO BE SOLVED: To solve the problem wherein a means using lifting power by a pressure difference to be generated by a difference between an upper and a lower angles formed in a blade of a wing by propelling force is used to float an article such as a robot in the air and large propelling force is necessary.
SOLUTION: A hydraulic device is used to directly generate buoyancy, and at the same time, wind force is taken to push the article upward, and the article is raised with slide of a cylinder.
COPYRIGHT: (C)2006,JPO&NCIPI

Abstract translation: 解决的问题为了解决这样一个问题，其中使用通过由推动力形成在翼片的叶片中的上下角之间的差产生的由压差产生的提升力的装置用于浮动 空气中的机器人和大推进力的物品是必要的。 解决方案：液压装置用于直接产生浮力，同时采取风力将物品向上推，物品用气缸滑动升起。 版权所有（C）2006，JPO＆NCIPI

公开(公告)号：JP2005324769A

公开(公告)日：2005-11-24

申请号：JP2004177638

申请日：2004-05-18

Applicant: Tomoyasu Yoko ,  Tomoyasu Yutaka ,  友安 裕 ,  友安 陽子

Inventor： TOMOYASU YOSHIOKI

IPC: B62D37/02 ,  B60F5/02 ,  B64C39/00

Abstract: PROBLEM TO BE SOLVED: To provide a transporter capable of efficiently performing an air operation by floating itself in the air by directly generating buoyancy by hydraulic equipment in a conventional airplane or automobile and simultaneously using propulsive force by conventional power, to remarkably attain energy saving and reduction of exhaust emissions.
SOLUTION: This transporter is provided with a function for directly floating a vehicle body in the air by operating a hydraulic device by utilizing power of an engine, a motor and a turbine of a transporting vehicle.
COPYRIGHT: (C)2006,JPO&NCIPI

Abstract translation: 要解决的问题：提供一种能够通过在常规飞机或汽车中通过液压设备直接产生浮力并同时使用常规动力的推进力而将其自身浮动在空气中以有效执行空气操作的运输机，以显着获得 节能减排废气排放。 解决方案：该输送器具有通过利用发动机，电动机和运输车辆的涡轮机的动力操作液压装置来直接将车体浮在空气中的功能。 版权所有（C）2006，JPO＆NCIPI

公开(公告)号：JP2003523870A

公开(公告)日：2003-08-12

申请号：JP2001558322

申请日：2001-02-07

IPC: B64C39/00 ,  B64C3/42 ,  B64C3/52 ,  B64C15/02 ,  B64C39/02 ,  B64C39/10 ,  B64D27/24 ,  B64D31/06 ,  G05D1/00 ,  H04B7/185

公开(公告)号：JP2003176729A

公开(公告)日：2003-06-27

申请号：JP2002323192

申请日：2002-09-30

Applicant: NOZAKI YOSHIO

Inventor： NOZAKI YOSHIO

IPC: B64C39/00 ,  C01B3/34 ,  F02C3/22 ,  F02C7/22 ,  F02K3/04

Abstract: PROBLEM TO BE SOLVED: To provide an airplane using hydrogen as fuel by a fuel reforming method. SOLUTION: In the airplane, a gas turbine is mainly driven by jet fuel (light oil) to cause intense air pollution. Depletion of oil resources approaches after a lapse of ten and several years. Accordingly, development and manufacture of the experimental airplane are started by two (German and Russian) companies in cooperation. In the experimental airplane, liquefied hydrogen is stored in each a refrigerated tank 15 of a temperature of -253°C and a withstanding pressure of 1.5 atm. The liquefied hydrogen fuel has a volume 4.2 times the jet fuel. The tank 15 of the withstanding pressure of 1.5 atm cannot be stored in main wings and a center wing. Accordingly, an upper part 14 of a body 9 is expanded, and the cylindrical fuel tanks 15 for liquefied hydrogen and a heat insulation material 16 therefor are stored in the upper part 14. Because a transport/refrigeration apparatus is newly provided, liquefied hydrogen causes a high cost. The experimental airplane is provided with fuel reformers 2 developed for the purpose of supply of hydrogen to a fuel cell of a fuel cell automobile, separates hydrogen of liquefied fuel (mainly light oil, artificial petroleum in the future), and uses the hydrogen as the fuel to drive propfan engines 7, 19. COPYRIGHT: (C)2003,JPO

公开(公告)号：JP2003002297A

公开(公告)日：2003-01-08

申请号：JP2001234235

申请日：2001-06-26

Applicant: Hirobumi Seki ,  関 博文

Inventor： SEKI HIROBUMI

IPC: B64C39/00

Abstract: PROBLEM TO BE SOLVED: To provide an aerial moving craft capable of flying easily.
SOLUTION: This aerial moving craft is provided with a lateral pair of flapping main wings 11, 12 with base parts 11a, 11b, 12a, 12b supported to swivel bearings 3, 4, 5, 6; a main wing drive mechanism 20 for extending the main wings long and speeding up the swing-down speed when the main wings swing down while shortening the main wings and slowing down the swing-up speed when the main wings swing up; and an airframe propulsion mechanism 30 for adjusting the swing-down operation timing of the front edge side and rear edge side of the main wings when the main wings swing down.
COPYRIGHT: (C)2003,JPO

Abstract translation: 要解决的问题：提供能够轻松飞行的空中移动工艺。 解决方案：这种空中移动工具设有一对侧翼的主翼11,12，底座部分​​11a，11b，12a，12b支撑在旋转轴承3,4,5,6上。 主翼驱动机构20，用于在主翼向上摆动的同时缩短主翼，并且当主翼向上摆动时减慢摆动速度，使主翼长期延伸并加快摆动速度; 以及用于当主翼向下摆动时调节主翼的前缘侧和后边缘侧的向下操作时间的机身推进机构30。

公开(公告)号：JP2001294200A

公开(公告)日：2001-10-23

申请号：JP2000111574

申请日：2000-04-13

Applicant: HOMARE SHOJI KK

Inventor： OGAWA YOSHIYUKI

IPC: B64C39/00 ,  B64C29/00 ,  F02K5/00 ,  F03H1/00

Abstract: PROBLEM TO BE SOLVED: To provide an aircraft capable of flying by propellers and by jets, taking off and landing like a helicopter without requiring a long runway or a large site, reducing noise, flying without using natural resource fuel, changing a flying system into a jet device at a proper altitude after tanking off. SOLUTION: This aircraft is provided with a propeller device 3 comprising plural rotary propellers 2, an aerial injection jet device 16 comprising a spiral screw, a compressed air receiving and storing regulation chamber 18, an ion supply device, and a combustion chamber to feed compressed air into the compressed air receiving and storing regulation chamber 18 to mix the compressed air with ions supplied by the ion supply device in the combustion chamber to form a jet current which is injected into open air, a jet injection device D, and a compressed air storage chamber 33.