JP2013116719A - Device for floating hot air balloon capable of flying optionally in combination with exhaust heat of engine and electric heater - Google Patents

Device for floating hot air balloon capable of flying optionally in combination with exhaust heat of engine and electric heater Download PDF

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JP2013116719A
JP2013116719A JP2011278916A JP2011278916A JP2013116719A JP 2013116719 A JP2013116719 A JP 2013116719A JP 2011278916 A JP2011278916 A JP 2011278916A JP 2011278916 A JP2011278916 A JP 2011278916A JP 2013116719 A JP2013116719 A JP 2013116719A
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balloon
hot air
exhaust heat
electric heater
flying
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JP5650636B2 (en
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Tsunesuke Kubo
常祐 久保
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Abstract

PROBLEM TO BE SOLVED: To provide a balloon capable of flying to a destination independently of which way the wind blows and preventing the propane gas flame of a heat source for floating from catching a balloon envelope.SOLUTION: The heat source for floating is changed from conventional propane gas flame to the combination of the exhaust heat of an electric heater and a mover for generating electric power, and the balloon is provided with a blower to blow warm air into the balloon. The balloon is also provided with a propeller driven by a motor.

Description

発明の詳細な説明Detailed Description of the Invention

本発明は熱気球にプロペラを装備。目的地まで飛行可能にするため、浮上エネルギーを発電機用発動機の排気熱と電熱ヒーターに関する装置。  The present invention equips a hot air balloon with a propeller. A device related to the exhaust heat of generator generators and electric heaters, which makes it possible to fly to the destination.

従来、熱気球の熱源はプロパンガスの火炎噴射で浮上させるため、プロペラの装置が出来ません。それがため、風下しか飛行できません。  Conventionally, the hot air balloon's heat source is lifted by propane gas flame injection, so a propeller device is not possible. Because of that, you can only fly leeward.

発明が解決しようとする課題Problems to be solved by the invention

発電機用発動機の排気熱と、電熱ヒーターによって、熱気球内に暖気を送風して浮上が可能となる。  With the exhaust heat of the generator motor and the electric heater, warm air can be blown into the hot air balloon to rise.

課題を解決するための手段Means for solving the problem

ガスバーナーでは、プロペラを回すと火炎がゆれて気球幕に着火する。熱源を、発動機の排気熱と電熱の組み合わせで気球内に送気で浮上が可能で、軽量化とプロペラ（推進機）の装置が出来る。  In the gas burner, when the propeller is turned, the flame shakes and ignites the balloon curtain. The heat source can be lifted by sending air into the balloon by a combination of the exhaust heat and electric heat of the engine, reducing the weight and propeller (propulsion device).

発明実施の形態Embodiment of the Invention

図−１ 熱空気の発生概要。側面図で１は発電機用の発動機を示し、２は排気管で周囲にスパイラル式のフィン３が固着され、４のケーシングに包合。発動機側から空気が送風機の回転によって渦流となって気球内に送気される。５は電熱側のケーシングを示し、６の送風機で７の導管で気球内に送気を示し、Ｐは点火プラグを示し、Ｎは部材の結合を示し、Ｈは結合部を示し、それぞれの矢印は動きを示す。
図−２ 弓張り形状の保持部材１は破断線入りの正面図で、２の部分に気球上部との固着を示し、３は屈折点。矢印方向へのボルト穴を示し、４は気球の立ち上がり時に固定するためのボルト穴を示す。
図−３ 熱気球が立ち上がった形態の概要側面図で、１が進行方向矢印を示す。Ａの気球は懸吊部材１が前方で、２は結着部を示し、３は屈折点で着脱用のネジ穴を示し、４−１がネジを示す。５は２図の４との結合を示し５はモーター台座Ｅと弓張り部材１との隙間ライナーを示し、６は熱気球及び機器全体荷重の架体を示し、７は機関室を示し、８は送風管を示し、Ｄは搭乗員室を示し、Ｂ及びＣのロープでの支持を示し、Ｆ−１はモーターでＦ−２はプロペラを示し、矢印は動きを示し、それぞれのＮはネジ又はネジ穴を示し結合からなる。Figure 1 Overview of hot air generation. In the side view, 1 is a generator for a generator, 2 is an exhaust pipe, and spiral fins 3 are fixed around it, and are encased in a casing 4. Air is sent from the motor side into the balloon as a vortex by the rotation of the blower. 5 is a casing on the electric heating side, 6 is a blower, 7 is aired into the balloon through 7 conduits, P is a spark plug, N is a coupling of members, H is a coupling portion, and each arrow Indicates movement.
Fig.-2 A bow-shaped holding member 1 is a front view including a broken line, and shows a fixation with the upper part of the balloon in a portion 2 and a refraction point 3. A bolt hole in the direction of the arrow is shown. Reference numeral 4 denotes a bolt hole for fixing when the balloon rises.
Fig. 3 A schematic side view of a hot air balloon standing up, where 1 indicates an advancing direction arrow. In the balloon A, the suspension member 1 is the front, 2 is a binding portion, 3 is a refraction point, a screw hole for attachment / detachment, and 4-1 is a screw. 5 indicates a connection with 4 in FIG. 2, 5 indicates a gap liner between the motor base E and the bow member 1, 6 indicates a hot air balloon and a whole body load frame, 7 indicates an engine room, 8 Indicates the air duct, D indicates the passenger compartment, B and C support on the rope, F-1 indicates the motor, F-2 indicates the propeller, arrows indicate the movement, and each N indicates the screw Or it shows a screw hole and consists of a connection.

発動機用発電機に熱源を発生させるための装置の側面図で、１は発動機で裏面に発電機を要して、２の排気管に螺旋状のフィン３が固着、４が外管を示し、５が電熱包号管を示し、内部に発熱体を有し送風機６の回転によって送気管７を経て気球内に送気を示し、Ｐは点火プラグを示し、Ｈは結合部機を示し、矢印は動きを示し、それぞれのＮはネジ穴又はアーク溶接からなる。1 is a side view of an apparatus for generating a heat source in a generator for an engine. Reference numeral 1 is an engine and a generator is required on the back side, and a helical fin 3 is fixed to an exhaust pipe 2 and 4 is an outer pipe. 5 indicates an electric heat envelope tube, a heating element is provided therein, air is supplied into the balloon through the air supply tube 7 by rotation of the blower 6, P indicates an ignition plug, and H indicates a coupling unit. , Arrows indicate movement, and each N consists of a screw hole or arc welding. １は気球を直立させ飛行の安定を計るための破断線入りの懸吊部材を示し、２は気球との結合フック穴を示し、３は屈折基点矢印方向へのネジ穴を示し、４は直立時にネジ止めする穴からなる。1 is a suspension member with a broken line for standing the balloon upright and measuring flight stability, 2 is a hook hole for coupling with the balloon, 3 is a screw hole in the direction of the refraction base arrow, and 4 is upright It consists of holes that are sometimes screwed. 気球の立ち上げ状態を示す側面図で、Ａの気球はロープＢ及びＣによって１の懸吊部機に２のフック穴の上部上にロープ５が纏まる事を示し、Ｎはそれぞれのネジを示し、６は架体（フレーム）で上部に必要とする機器等が搭載。７は送気管を示し、８は機器室を示し、Ｄは搭乗員室を示し、Ｅはモーター搭載用の台座を示し、Ｆ−１はモーターを示し、左右方向に動作するＦ−２プロペラからなる。In the side view showing the rising state of the balloon, the balloon A shows that the ropes 5 and 1 are bundled on the upper part of the hook hole 2 by the rope B and C, and N shows each screw. , 6 is a frame (frame) that is equipped with necessary equipment on the top. 7 indicates an air supply pipe, 8 indicates an equipment room, D indicates a crew room, E indicates a pedestal for mounting a motor, F-1 indicates a motor, and an F-2 propeller that operates in the left-right direction. Become.

Claims (1)

発電機用発動機の排気熱と電熱ヒーターによって気球内への送気で浮上。
任意に飛行が可能な熱気球用の発熱装置。Ascends by sending air into the balloon by the exhaust heat of the generator motor and the electric heater.
Heating device for hot air balloons that can fly arbitrarily.
JP2011278916A 2011-12-02 2011-12-02 A device that can float by combining the exhaust heat of the motor and the electric heater so that the hot air balloon can fly arbitrarily. Expired - Fee Related JP5650636B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2011278916A JP5650636B2 (en) 2011-12-02 2011-12-02 A device that can float by combining the exhaust heat of the motor and the electric heater so that the hot air balloon can fly arbitrarily.

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Application Number Priority Date Filing Date Title
JP2011278916A JP5650636B2 (en) 2011-12-02 2011-12-02 A device that can float by combining the exhaust heat of the motor and the electric heater so that the hot air balloon can fly arbitrarily.

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JP2013116719A true JP2013116719A (en) 2013-06-13
JP5650636B2 JP5650636B2 (en) 2015-01-07

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Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB259371A (en) * 1925-09-23 1926-10-14 Michael Alexander Szymanski Improvements in or relating to airships
US1677308A (en) * 1928-07-17 Method of inflating and driving an aerial machine and means
JPS5083991U (en) * 1973-11-28 1975-07-18
GB1548884A (en) * 1976-06-29 1979-07-18 Walden O A R Lighterthan-air-craft of the rigid dirigible type with controllable buoyncy
JPS55113700U (en) * 1979-02-05 1980-08-11
JPH02174600A (en) * 1988-12-23 1990-07-05 Isuzu Motors Ltd Rotation stabilizer for generator engine
JPH0471995A (en) * 1990-07-11 1992-03-06 Daiji Mitsuhiro Ascending and descending method for pressurized airship
JPH06227494A (en) * 1992-11-24 1994-08-16 Minoru Yoshida In-balloon heat generating type thermal balloon
GB2297532A (en) * 1995-02-06 1996-08-07 Peter John Mckay Hot air balloon
JP2006044299A (en) * 2004-07-30 2006-02-16 Kawasaki Heavy Ind Ltd Method and device for regulating intra-fuselage gas temperature of airship

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1677308A (en) * 1928-07-17 Method of inflating and driving an aerial machine and means
GB259371A (en) * 1925-09-23 1926-10-14 Michael Alexander Szymanski Improvements in or relating to airships
JPS5083991U (en) * 1973-11-28 1975-07-18
GB1548884A (en) * 1976-06-29 1979-07-18 Walden O A R Lighterthan-air-craft of the rigid dirigible type with controllable buoyncy
JPS55113700U (en) * 1979-02-05 1980-08-11
JPH02174600A (en) * 1988-12-23 1990-07-05 Isuzu Motors Ltd Rotation stabilizer for generator engine
JPH0471995A (en) * 1990-07-11 1992-03-06 Daiji Mitsuhiro Ascending and descending method for pressurized airship
JPH06227494A (en) * 1992-11-24 1994-08-16 Minoru Yoshida In-balloon heat generating type thermal balloon
GB2297532A (en) * 1995-02-06 1996-08-07 Peter John Mckay Hot air balloon
JP2006044299A (en) * 2004-07-30 2006-02-16 Kawasaki Heavy Ind Ltd Method and device for regulating intra-fuselage gas temperature of airship

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