| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 161 | 개폐장치를 통해 부피조절이 가능한 비행체 | KR1020120089893 | 2012-08-17 | KR1020140023671A | 2014-02-27 | 권철휘; 강훈; 이남도 |
| The present invention relates to an air balloon capable of controlling a volume and more specifically, to an air balloon which has a switchgear on the outer surface of the air balloon, makes a part of the outer surface of the air balloon inserted into the main body of the air balloon through the switchgear, and increases and decreases the total volume of the air balloon as much as an extra size which is inserted into the inside when opening the switchgear. The present invention includes: an air balloon main body which obtains static buoyancy by being filled with floating gas; the switchgear which is mounted to be able to open and close by being formed on the outer surface of the air balloon main body; an observation equipment box which is able to mount observation equipment including an infrared camera; a ground tow string which controls the lift height of the balloon; and a gas injection hole which is an inlet for filling the air balloon main body with the floating gas. The provided air balloon for mounting equipment is able to increase and decrease the total volume of the air balloon main body as much as the size of the outer surface of the air balloon main body which is inserted into the inside when opening the switchgear by inserting a part of the outer surface of the air balloon main body into the inside of the air balloon main body through the switchgear. | ||||||
| 162 | 성층권 비행선과 반사판을 이용한 지표면의 온도 조절 방법 | KR1020110121491 | 2011-11-21 | KR101141734B1 | 2012-05-03 | 최준민 |
| PURPOSE: A method for controlling local territorial temperature is provided to intercept the inflow of sunlight on the surface of the earth. CONSTITUTION: When a reflector(120) makes right angle against the incident angle of the sunlight(S), the sunlight is absorbed and the sunlight inflow to the surface of the earth is blocked. The reflecting surface is made of a cheap material and prevents the sunlight from permeating the reflector. The reflector is combined with the support line(110) of an airship(100) and moves to stratosphere by the floating of the airship. | ||||||
| 163 | 약품살포용 무인 비행선 | KR1020080103685 | 2008-10-22 | KR1020100044519A | 2010-04-30 | 송용규 |
| PURPOSE: A manless airship for sprinkling chemicals is provided to reduce reaction by remarkably reducing the size of the airship, and to maintain the low altitude of the airship by immediately controlling ascending and descending of the airship. CONSTITUTION: A manless airship(100) for sprinkling chemicals comprises an air sac part(1), a manipulation part(2), a rising part(3), a spraying part(4), and a control part. The air sac part is filled with air. The manipulation part is formed in the rear of the air sac part, and controls the direction of the airship. The rising part is coupled to a frame body(10). The spraying part is installed in the frame body, and sprays liquid chemicals. The control part controls operating of the manipulation part, the rising part, and the spraying part. | ||||||
| 164 | 비행기에 광선을 디스플레이하기 위한 장치 및 방법 | KR1020047010842 | 2003-01-10 | KR1020040101205A | 2004-12-02 | 쉐들바우어,베로니카; 리크,주에르겐 |
| 본 발명은 광선을 발생시키기 위한 하나 이상의 광원, 및 상기 광선을 투사 가능한 광선로 변환시키기 위한 하나 이상의 프로젝터를 포함하는, 비행기의 셸에 광선을 디스플레이하기 위한 장치 및 방법에 관한 것이다. 상기 하나 이상의 프로젝터는 광선을 내부(15)를 통해 셸(60)로 투사하기 위해 셸의 내부에 장착된다. 상기 셸은 적어도 부분적으로 투명하게 형성됨으로써, 투사된 광선이 외부로 가시화된다. 본 발명은 또한 비행기의 셸에 광선을 디스플레이하기 위한 방법에 관한 것이다. | ||||||
| 165 | 가스와 열을 이용한 상승 부력을 얻는 비행선. | KR1020100083069 | 2010-08-26 | KR1020120019702A | 2012-03-07 | 이청주 |
| PURPOSE: An airship, which obtains buoyancy using gas and heat, is provided to implement advertisement at low cost by using a small amount of rising gas and a low-price heater. CONSTITUTION: An airship raises an existing device with a small amount of rising gas and increases the shell of a sphere to obtain buoyancy and maximize an advertisement area. The airship obtains buoyancy by using a low-price heater and reusing heated air through a heat exchanger. A rising gas bag is installed on the top of the airship and a burner(2) is installed on the bottom of the airship. | ||||||
| 166 | 비행선의 조립 구조 | KR1020090096886 | 2009-10-12 | KR1020110039856A | 2011-04-20 | 제정형; 이성근 |
| PURPOSE: An assembling structure of an airship is provided to make a patch connection structure for connecting a patch to a gondola without shaking. CONSTITUTION: An assembling structure of an airship comprises a gondola(100), a wind direction adjusting member a first rail, a second rail, and a patch connection part(130). The gondola has an engine rotation server member. The engine rotation server member is installed in a specified region of a gas bag using a patch in order to locate the gas bag on a right position. The wind direction adjusting member corrects the location of gas bag according to the direction of wind. The first rail and second rail are arranged in both upper side part of the gondola in a row along the longitudinal direction of the gas bag using a plurality of brackets. The patch connection part comprises a connection hole. A plurality of connection holes is located on the first and second rails at a fixed interval. | ||||||
| 167 | 가스 배출이 용이한 기낭 구조 | KR1020080123888 | 2008-12-08 | KR1020100065522A | 2010-06-17 | 김성욱; 김동민 |
| PURPOSE: An envelope structure is provided to prevent the movement of gas due to the attachment of the inner wall of an envelope by forming a gas guide unit inside the envelope such as a balloon, an airship, or a tube. CONSTITUTION: An envelope structure(200) comprises a gas storage unit(110) and a gas guide unit(120). The gas storage unit is formed inside the envelope structure. The gas guide unit is integrated with the inner surface of the envelope and has fixed thickness to prevent inner surfaces of the envelope from contacting each other. The gas flows in the gas guide unit. The gas guide unit comprises multiple discharge holes. A discharge path is formed inside the gas guide unit and guides the gas inside the gas storage unit along to the gas guide unit. | ||||||
| 168 | 한정된 내부 공간 내에서 사용자를 이송하는 추진 시스템및 추진 장치 | KR1020087004554 | 2006-07-26 | KR1020080063744A | 2008-07-07 | 미도우즈제이스티븐 |
| The present invention comprises an inflatable balloon of sufficient volume and buoyancy to allow a human pilot to float above the ground and to glide over the ground within an enclosed area. The balloon incorporates several safety features that permit it to be used for recreation, including a prop-bike to enable the user to propel the balloon. Various structures, including a portable structure and a retaining structure in a stadium are described for use with the inflatable balloon. | ||||||
| 169 | 비행선 | KR1020027014028 | 2002-03-13 | KR100487594B1 | 2005-05-04 | 오가와,다이하치; 오가키,마사노부; 사사키,요시타카; 수가와라,마사히코; 마에하타,타카요시; 푸쿠모토,카츠지 |
| A plurality of bulkheads (23a to 23d) are installed in a hull (21) so as to divide the interior space of the hull (21) into a plurality of compartments ( DELTA S1 to DELTA S5) successively arranged along the axis (22) of the hull (21). Thecompartments ( DELTA S1 to DELTA S5) are divided into upper flotation gas containing spaces (25a to 25e) and lower air containing spaces (26a to 26e) by flexible diaphragms (24a to 24e) impermeable to air and a flotation gas, respectively. The bulkheads (23a to 23d) have upper parts A1a, Alb, A1c and A1d formed of a meshed sheet, extending upward from joints (27a to 27d) of the diaphragms (24a to 24e) and the bulkheads (23a to 23d) , exposed to the flotation gas containing spaces (25a to 25e). The upper parts are provided with a plurality of vents through which the flotation gas is allowed to flow. <IMAGE> | ||||||
| 170 | 비행선 | KR1020027014028 | 2002-03-13 | KR1020030015229A | 2003-02-20 | 오가와,다이하치; 오가키,마사노부; 사사키,요시타카; 수가와라,마사히코; 마에하타,타카요시; 푸쿠모토,카츠지 |
| 기체(21)에, 이 기체(21) 내를 기축(22)방향으로 복수의 공간부분(△S1 ~ △S5)으로 분할하는 복수의 격벽(23a ~ 23d)이 설치되어 있다. 상기 각 공간부분(△S1 ~ △S5)은 부양가스 및 공기의 통과를 차단하는 가요성을 가진 격막(24a ~ 24e)에 의해 부양가스를 수용하는 상층의 부양가스수용영역(25a ~ 25e)과 공기를 수용하는 하층의 공기수용영역(26a ~ 26e)으로 칸막이되어 있다. 상기 각 격벽(23a ~ 23d)의 각 격막(24a ~ 24e) 중 결합점(27a ~ 27d) 보다 위쪽의 각 부양가스수용영역(25a ~ 25e)에 해당하는 상층부분(A1a ~ A1d)에 부양가스의 통과를 허용하는 통기구멍이 갖춰지도록 되어 있다. | ||||||
| 171 | NEAR-SPACE OPERATION SYSTEMS | US15616758 | 2017-06-07 | US20170349291A1 | 2017-12-07 | Taber K. MacCallum; Jacob H. Dang; Robert Alan Eustace; John Zaniel Maccagnano; Julian R. Nott; Sebastian A. Padilla; Sreenivasan Shankarnarayan; John Straus; Jared Leidich; Daniel Pieter Jacobus Blignaut |
| A system enabling safe manned and unmanned operations at extremely high altitudes (above 70,000 feet). The system utilizes a balloon launch system and parachute and/or parafoil recovery. | ||||||
| 172 | WIND POWER GENERATION SYSTEM USING AIRSHIP | US15180575 | 2016-06-13 | US20170321658A1 | 2017-11-09 | Kwangwoo AN |
| The present invention relates a wind power generation system using an airship, which can generate wind power using strong wind of a jet stream by using the airship, convert the wind power into a laser beam and transmit the laser beam to the ground so that power can be produced on the ground by converting the laser beam into electricity. The present invention provides efficiency and convenience in collecting power of the airship on the ground by implementing a wind power generation system using an airship to include: an airship for producing power through wind power generation while floating in the air and transmitting the produced power as a laser beam; and a ground receiving unit for receiving the laser beam transmitted. from the airship and converting the laser beam into electricity. | ||||||
| 173 | INDUSTRIAL MACHINE ACOUSTIC INSPECTION USING UNMANNED AERIAL VEHICLE | US15051078 | 2016-02-23 | US20170240278A1 | 2017-08-24 | Richard Lynn Loud; Michael Alan Davi |
| A method for collecting acoustic data from an industrial machine is disclosed. The method may include: providing an unmanned aerial vehicle (UAV) having an acoustic receiver attached thereto; and positioning the unmanned aerial vehicle at a specific location so that the acoustic receiver collects acoustic data from the industrial machine at the specific location. An acoustic receiver is attached to the UAV for collecting acoustic data from the industrial machine. An acoustic filter is attached to the acoustic receiver and the UAV for filtering unwanted sound from the acoustic data. Acoustic data can be used by a flight control system to identify a specific location relative to the industrial machine that is a source a specific acoustic signature emanating from the industrial machine. | ||||||
| 174 | Industrial machine acoustic inspection using unmanned aerial vehicle | US15051078 | 2016-02-23 | US09738381B1 | 2017-08-22 | Richard Lynn Loud; Michael Alan Davi |
| A method for collecting acoustic data from an industrial machine is disclosed. The method may include: providing an unmanned aerial vehicle (UAV) having an acoustic receiver attached thereto; and positioning the unmanned aerial vehicle at a specific location so that the acoustic receiver collects acoustic data from the industrial machine at the specific location. An acoustic receiver is attached to the UAV for collecting acoustic data from the industrial machine. An acoustic filter is attached to the acoustic receiver and the UAV for filtering unwanted sound from the acoustic data. Acoustic data can be used by a flight control system to identify a specific location relative to the industrial machine that is a source a specific acoustic signature emanating from the industrial machine. | ||||||
| 175 | GAS-FILLED CARRIER AIRCRAFTS AND METHODS OF DISPERSING UNMANNED AIRCRAFT SYSTEMS IN DELIVERING PRODUCTS | US15427277 | 2017-02-08 | US20170233053A1 | 2017-08-17 | Donald R. High; David C. Cox |
| In some embodiments, apparatuses and methods are provided herein useful to transport unmanned aircraft systems to delivery products. In some embodiments, gas-filled aerial transport and launch system, comprises: a transport aircraft comprising: a gas chamber; and a carrier compartment where the gas chamber induces a lifting force on the carrier compartment; at least one propulsion system; and a navigation control system that controls the direction of travel of the transport aircraft; wherein the carrier compartment comprises: an unmanned aircraft system (UAS) storage area configured to receive multiple UASs; and an UAS launching bay that enables the UAS to be launched while the transport aircraft is in flight and while the UAS is carrying a package to be delivered. | ||||||
| 176 | EXTENDED ENDURANCE AIR VEHICLE | US15222704 | 2016-07-28 | US20160332714A1 | 2016-11-17 | William Edmund Nelson |
| An air vehicle comprises a vehicle body and a propulsion assembly. The vehicle body has the shape of a wing airfoil so that the vehicle body generates lift when air flows over the vehicle body. The vehicle body has a body longitudinal axis, and includes a first hull and a second hull that are secured together side-by-side, the hulls having longitudinal axes that are substantially parallel to the body longitudinal axis. Each hull defines a separate fluid chamber that is filled with a fluid that is at least partially buoyant. The propulsion assembly is secured to the vehicle body. The propulsion assembly generates thrust and includes a port front engine, a port rear engine, a starboard front engine, and a starboard rear engine, wherein at least two of the engines have independently controlled thrust vectors. | ||||||
| 177 | Lighter-Than-Air Systems, Methods, and Kits for Obtaining Aerial Images | US14845701 | 2015-09-04 | US20150375842A1 | 2015-12-31 | John Ciampa; Bertrand Dano |
| Lighter-than-air systems, methods, and kits for obtaining aerial images are described. For example, various methods for determining planned ascent, drift, and/or descent of a lighter-than-air system are described. In addition, various structural arrangements of lighter-than-air systems for accomplishing planned ascent, drift, and/or descent and obtaining aerial images are described. | ||||||
| 178 | Air vehicle having strakes | US13944141 | 2013-07-17 | US09132904B2 | 2015-09-15 | Michael Durham |
| An air vehicle has a gas-filled hull of a flexible sheet material. Strakes extend along an exterior of the hull, each strake comprising a gas-filled tube of a sheet of a flexible sheet material. A rigid board extends outwardly from the gas-filled tube and away from the vehicle. A further sheet of a flexible sheet material extends from one side of the strake over the board to another side of the strake, to provide a strake that is generally triangular in cross section. | ||||||
| 179 | Lighter-than-air systems, methods, and kits for obtaining aerial images | US14104059 | 2013-12-12 | US09126669B2 | 2015-09-08 | John Ciampa; Bertrand Dano |
| Lighter-than-air systems, methods, and kits for obtaining aerial images are described. For example, various methods for determining planned ascent, drift, and/or descent of a lighter-than-air system are described. In addition, various structural arrangements of lighter-than-air systems for accomplishing planned ascent, drift, and/or descent and obtaining aerial images are described. | ||||||
| 180 | 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. | ||||||
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