CN104002959A - Power airship with rotating blade propellers - Google Patents
Power airship with rotating blade propellers Download PDFInfo
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- CN104002959A CN104002959A CN201410234073.7A CN201410234073A CN104002959A CN 104002959 A CN104002959 A CN 104002959A CN 201410234073 A CN201410234073 A CN 201410234073A CN 104002959 A CN104002959 A CN 104002959A
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- blade
- main shaft
- ship body
- guides
- rachis
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Abstract
The invention provides a power airship with rotating blade propellers and belongs to the technical field of aircrafts. The power air ship is formed by an airship body, a hanging basket, an control system and a propulsion system; the airship body is filled with gas which is lighter than air; the control system is a radio control system; the propulsion system comprises the two groups of propellers which comprise the same structure and function; the propellers are symmetrically arranged under the left side and the right side of the rear portion of the airship body respectively; each propeller is formed by a motor, a lithium battery, an electronic regulator, a gear reduction gear, a main shaft, a rotating arm, a blade, a blade shaft, a guide rod and a guide; the lithium batteries are used for supplying power for the motors; rotation speed and steering regulation of the motors is performed through a radio receiver and the electric regulators; the motors are controlled by a radio remote control transmitter which is arranged in the hanging basket or on the ground; thrust is produced through rotary motion of the blades of the propellers. The power airship with the rotating blade propellers is high in propulsion efficiency, serves as an air traffic tool and is applied to aerial photography and physical recreation activities.
Description
Technical field
A kind of angle of rake power airship of rotating blade that adopts, belongs to vehicle technology field, relates in particular to a kind of dirigible.
Background technology
Traditional power airship adopts screw propeller to make propelling unit mostly, although drive conveniently, efficiency is lower, propeller producing process complexity, and can produce tail while using.
Summary of the invention
The object of the invention is to overcome the above-mentioned deficiency of traditional power dirigible, invent the angle of rake power airship of employing rotating blade that a kind of efficiency is higher.
A kind of angle of rake power airship of rotating blade that adopts, is made up of ship body, hanging basket, control system and propulsion system.In ship body, be full of the gas that is lighter than air.Control system comprises a radio telecommand projector and two radio receivers.Radio telecommand projector is placed in hanging basket or ground.Propulsion system comprises all identical propelling units of two groups of 26S Proteasome Structure and Functions, and they are symmetrically arranged in respectively the ship below of the left and right sides of portion after one's death, are arranged on the support being connected with ship body.Every group of propelling unit is furnished with a radio receiver, and every group of propelling unit is by motor, lithium cell, electronic regulator, reduction gear apparatus, main shaft, pivoted arm, blade, rachis, pilot bar and guides composition.Motor is arranged on the support being connected with ship body, and motor is by the lithium battery power supply conveniently charging, and the adjusting of being carried out rotating speed and being turned to by radio receiver and electronic regulator, by being placed in hanging basket or the radio telecommand projector on ground is controlled, motor is connected with reduction gear apparatus, in succession one end of main shaft of the mouth of reduction gear apparatus, main shaft horizontal arrangement and vertical with the longitudinal plane of symmetry of ship body, the stage casing of main shaft is connected with the support being connected under ship body by bearing, the other end of main shaft is vertical with one end of pivoted arm to be connected, the other end of pivoted arm is vertical with one end of rachis to be connected, rachis and main shaft are arranged in respectively the both sides of pivoted arm, the other end of rachis is also connected with blade by the bearing in this hole through the leading edge of the close blade on blade and the hole parallel with blade inlet edge, rachis is parallel with the leading edge of blade, the root end face of blade is vertical near the end face of one end and the leading edge of blade of pivoted arm plane of rotation, and blade is trapezoidal or rectangle at right angles, and the cross section of blade is aerofoil profile, the hypomere of pilot bar and blade are fixed on the root end face of blade overlapping with the string of a musical instrument of this end face, and the epimere of pilot bar is through guides, guides is closely bumped into oscillating bearing by linear bearing and combines, the back upper place that guides is placed in main shaft is installed on the support being connected with ship body, guides is installed near the rotation round of rachis as far as possible, but guides to the distance between main-shaft axis is greater than the maximum chord length sum of arm length and blade, so that blade rotates smoothly, the length of pilot bar should enough guarantee that its upper end is all the time in guides and do not come off.The main shaft that is placed in the main shaft in ship body left side and be placed in ship body right side is on same level straight line.The guides that is placed in ship body left side is the back upper place in main-shaft axis and parallel with main-shaft axis with the line of guides that is placed in ship body right side.
This kind of principle of work that adopts the angle of rake power airship of rotating blade is: how many dirigibles regulates lifting by the tolerance of tiny balloons in ship body, regulates flying speed and direction by propulsion system.Regulate the tolerance of tiny balloons in ship body, after dirigible lift-off, start the motor of ship body both sides simultaneously, the power of motor is passed to main shaft separately by reduction gear apparatus, the main shaft of the ship body left and right sides is the pivoted arm rotation of the synchronized in the same way drive left and right sides simultaneously, the pivoted arm of the left and right sides drives the rachis rotation of the left and right sides separately and the traction blade rotary separately air of fluttering produces the equal thrust of direction formed objects, promotes this dirigible and travels.Due to the restriction of pilot bar and guides, when blade rotary, its angle of attack revolves at a cycle of operations the interior meeting of turning around regular variation occurs, and is conducive to produce thrust.Change the size that spindle speed size can change thrust, the faster thrust of rotating speed is larger, and the slower thrust of rotating speed is less; The rotation direction that changes main shaft can change the direction of thrust.Turn right from ship body left side: two synchronized in the same way left-hand revolutions of blade, this dirigible flies before the flight of deflection arch direction; When two blade rotational speeds are different, dirigible is turned toward the slow side of blade rotational speed.The synchronized in the same way clickwise of two blades, this dirigible flies after the flight of ship tail direction; When two blade rotational speeds are different, dirigible is turned toward the slow side of blade rotational speed.If two blade rotational speed is identical but switched in opposite just can realize pivot turn.People handles radio telecommand projector and controls speed and the course of this dirigible in hanging basket, also can utilize radio telecommand projector to control dirigible on ground.
Advantage of the present invention is: this invention is a kind of can not produce the obvious tail as propeller while adopting the angle of rake power airship of rotating blade to use, and this dirigible degradation of energy is little, efficiency is high, and blade is easily made, and can adopt the straight airfoil fan of rigidity.Make for make transatmospheric vehicle and take photo by plane, amusement and recreation sports.
Brief description of the drawings
Fig. 1 is a kind of schematic rear view that adopts the angle of rake power airship of rotating blade of the present invention; Fig. 2 is the left view of Fig. 1; Fig. 3 is the enlarged drawing of propelling unit 3 in Fig. 2.
In figure, 1-ship body, 11-deflection arch, 12-ship tail; 2-support; 3-propelling unit, 31-motor, 32-reduction gear apparatus, 33-main shaft, 34-pivoted arm, 35-blade, 36-rachis, 37-pilot bar, 38-guides, 381-linear bearing, 382-oscillating bearing; 4-hanging basket; In Fig. 2, the hand of rotation of pivoted arm 34 when the hollow arrow on pivoted arm 34 represents that this invention dirigible advances; Broken circle 5 represents the rotational trajectory of rachis 36.
Detailed description of the invention
Now by reference to the accompanying drawings 1, accompanying drawing 2 and accompanying drawing 3 are illustrated the present invention for example: a kind of angle of rake power airship of rotating blade that adopts, is made up of ship body 1, hanging basket 4, control system and propulsion system.In ship body 1, be full of the gas that is lighter than air.Control system comprises a radio telecommand projector and two radio receivers.Radio telecommand projector is placed in hanging basket 4 or ground.Propulsion system comprises all identical propelling units 3 of two groups of 26S Proteasome Structure and Functions, and they are symmetrically arranged in respectively the below of the left and right sides at ship body 1 rear portion, are arranged on the support 2 being connected with ship body 1.Every group of propelling unit 3 is furnished with a radio receiver, and every group of propelling unit 3 forms by motor 31, lithium cell, electronic regulator, reduction gear apparatus 32, main shaft 33, pivoted arm 34, blade 35, rachis 36, pilot bar 37 and guides 38.Motor 31 is arranged on the support 2 being connected with ship body 1, and motor 31 is by the lithium battery power supply conveniently charging, and the adjusting of being carried out rotating speed and being turned to by radio receiver and electronic regulator, controls by being placed in hanging basket 4 radio telecommand projector interior or ground, motor 31 is connected with reduction gear apparatus 32, in succession one end of main shaft 33 of the mouth of reduction gear apparatus 32, main shaft 33 horizontal arrangement and vertical with the longitudinal plane of symmetry of ship body 1, the stage casing of main shaft 33 is connected with the support 2 being connected under ship body 1 by bearing, vertical being connected in one end of the other end of main shaft 33 and pivoted arm 34, vertical being connected in one end of the other end of pivoted arm 34 and rachis 36, rachis 36 and main shaft 33 are arranged in respectively the both sides of pivoted arm 34, the other end of rachis 36 is also connected with blade 35 by the bearing in this hole through the leading edge of the close blade 35 on blade 35 and the hole parallel with blade 35 leading edges, rachis 36 is parallel with the leading edge of blade 35, the end face of one end of close pivoted arm 34 plane of rotations of the root end face of blade 35 is vertical with the leading edge of blade 35, the rectangular trapezoidal or rectangle of blade 35, and the cross section of blade 35 is aerofoil profile, the hypomere of pilot bar 37 and blade 35 are fixed on the root end face of blade 35 overlapping with the string of a musical instrument of this end face, and the epimere of pilot bar 37 is through guides 38, guides 38 is closely bumped into oscillating bearing 382 by linear bearing 381 and combines, the top that guides 38 is placed in main shaft 33 is installed on the support 2 being connected with ship body 1, guides 38 is installed near the rotation round of rachis 36 as far as possible, but guides 38 is greater than the maximum chord length sum of pivoted arm 34 length and blade 35 to the distance between main shaft 33 axis, so that blade 35 rotates smoothly, the length of pilot bar 37 should enough guarantee that its upper end is all the time in guides 38 and do not come off.The main shaft 33 that is placed in the main shaft 33 in ship body 1 left side and be placed in ship body 1 right side is on same level straight line.The guides 38 that is placed in ship body 1 left side is the back upper place in main shaft 33 axis and parallel with main shaft 33 axis with the line of guides 38 that is placed in ship body 1 right side.
This kind of principle of work that adopts the angle of rake power airship of rotating blade is: how many dirigibles regulates lifting by the tolerance of ship body 1 interior tiny balloons, regulates flying speed and direction by propulsion system.Regulate the tolerance of ship body 1 interior tiny balloons, after dirigible lift-off, start the motor 31 of ship body 1 both sides simultaneously, the power of motor 31 is passed to main shaft 33 separately by reduction gear apparatus 32, the main shaft 33 of the ship body 1 left and right sides simultaneously pivoted arm 34 of the synchronized in the same way drive left and right sides rotates, the pivoted arm 34 of the left and right sides drives separately the rachis 36 of the left and right sides to rotate and draws the blade separately 35 rotations air of fluttering and produce the equal thrust of direction formed objects, promotes this dirigible and travels.Due to the restriction of pilot bar 37 and guides 38, when blade 35 rotates, its angle of attack revolves at a cycle of operations the interior meeting of turning around regular variation occurs, and is conducive to produce thrust.Change the size that main shaft 33 rotating speed sizes can change thrust, the faster thrust of rotating speed is larger, and the slower thrust of rotating speed is less; The rotation direction that changes main shaft 33 can change the direction of thrust.Turn right from ship body 1 left side: two synchronized in the same way left-hand revolutions of blade 35, this dirigible flies before deflection arch 11 direction flights; When two blade 35 rotating speeds differences, dirigible is turned toward the slow side of blade 35 rotating speeds.The synchronized in the same way clickwise of two blades 35, this dirigible flies after the 12 direction flights of ship tail; When two blade 35 rotating speeds differences, dirigible is turned toward the slow side of blade 35 rotating speeds.If two blade 35 rotating speeds are identical but switched in opposite just can realize pivot turn.People handles radio telecommand projector and controls speed and the course of this dirigible in hanging basket 4, also can utilize radio telecommand projector to control dirigible on ground.
This dirigible is as transatmospheric vehicle, and making physical culture recreation facility for the place such as scenic spot, large-scale parks is also a good selection.
Claims (4)
1. adopt the angle of rake power airship of rotating blade, formed by ship body (1), hanging basket (4), control system and propulsion system, it is characterized in that: ship body is full of the gas that is lighter than air in (1), control system comprises a radio telecommand projector and two radio receivers, radio telecommand projector is placed in hanging basket (4) or ground, propulsion system comprises all identical propelling units (3) of two groups of 26S Proteasome Structure and Functions, and they are symmetrically arranged in respectively the below of the left and right sides at ship body (1) rear portion, are arranged on the support (2) being connected with ship body (1), every group of propelling unit (3) is furnished with a radio receiver, and every group of propelling unit (3) is by motor (31), lithium cell, electronic regulator, reduction gear apparatus (32), main shaft (33), pivoted arm (34), blade (35), rachis (36), pilot bar (37) and guides (38) composition, motor (31) is arranged on the support (2) being connected with ship body (1), motor (31) is connected with reduction gear apparatus (32), in succession one end of main shaft (33) of the mouth of reduction gear apparatus (32), main shaft (33) horizontal arrangement and vertical with the longitudinal plane of symmetry of ship body (1), the stage casing of main shaft (33) is connected with the support (2) being connected under ship body (1) by bearing, vertical being connected in one end of the other end of main shaft (33) and pivoted arm (34), vertical being connected in one end of the other end of pivoted arm (34) and rachis (36), rachis (36) and main shaft (33) are arranged in respectively the both sides of pivoted arm (34), the other end of rachis (36) is also connected with blade (35) by the bearing in this hole through the leading edge of the close blade (35) on blade (35) and the hole parallel with blade (35) leading edge, rachis (36) is parallel with the leading edge of blade (35), the end face of one end of close pivoted arm (34) plane of rotation of the root end face of blade (35) is vertical with the leading edge of blade (35), the hypomere of pilot bar (37) and blade (35) are fixed on the root end face of blade (35) overlapping with the string of a musical instrument of this end face, and the epimere of pilot bar (37) is through guides (38), the top that guides (38) is placed in main shaft (33) is installed on the support (2) being connected with ship body (1), guides (38) is installed near the rotation round of rachis (36) as far as possible, but guides (38) is greater than the maximum chord length sum of pivoted arm (34) length and blade (35) to the distance between main shaft (33) axis, the length of pilot bar (37) should enough guarantee that its upper end is all the time in guides (38) and do not come off, the main shaft (33) that is placed in the main shaft (33) in ship body (1) left side and be placed in ship body (1) right side is on same level straight line, the guides (38) that is placed in ship body (1) left side is the back upper place in main shaft (33) axis and parallel with main shaft (33) axis with the line of guides (38) that is placed in ship body (1) right side.
2. a kind of angle of rake power airship of rotating blade that adopts according to claim 1, it is characterized in that: motor (31) is by the lithium battery power supply conveniently charging, the adjusting of being carried out rotating speed and being turned to by radio receiver and electronic regulator, controls by being placed in hanging basket (4) radio telecommand projector interior or ground.
3. a kind of angle of rake power airship of rotating blade that adopts according to claim 1, is characterized in that: guides (38) is closely bumped into oscillating bearing (382) by linear bearing (381) and combines.
4. a kind of angle of rake power airship of rotating blade that adopts according to claim 1, is characterized in that: blade (35) is trapezoidal or rectangle at right angles, and the cross section of blade (35) is aerofoil profile.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410234073.7A CN104002959B (en) | 2014-05-30 | 2014-05-30 | The angle of rake power airship of a kind of employing rotating blade |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410234073.7A CN104002959B (en) | 2014-05-30 | 2014-05-30 | The angle of rake power airship of a kind of employing rotating blade |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104002959A true CN104002959A (en) | 2014-08-27 |
| CN104002959B CN104002959B (en) | 2015-11-11 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410234073.7A Active CN104002959B (en) | 2014-05-30 | 2014-05-30 | The angle of rake power airship of a kind of employing rotating blade |
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| Country | Link |
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| CN (1) | CN104002959B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104986319A (en) * | 2015-07-21 | 2015-10-21 | 中国科学院光电研究院 | Vector propelling device, airship and installation method for vector propelling device |
| CN107804481A (en) * | 2017-10-06 | 2018-03-16 | 廖忠民 | Dirigible assist system |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB277384A (en) * | 1927-09-13 | 1928-08-23 | Wigger Meindersma | Improvements in or relating to water- and aircraft-propellers |
| GB336642A (en) * | 1929-06-18 | 1930-10-20 | Willem Petrus Van Lammeren | Improvements in rotary propellers |
| CN201329955Y (en) * | 2009-01-10 | 2009-10-21 | 安徽省华云高科技有限责任公司 | Rainwater resistance power airship |
| CN201456967U (en) * | 2009-04-02 | 2010-05-12 | 王长林 | airship |
| CN101913425A (en) * | 2010-08-07 | 2010-12-15 | 吴泽峰 | Airship |
| CN202295277U (en) * | 2011-09-29 | 2012-07-04 | 周昶锃 | Novel flying fish |
| CN203864990U (en) * | 2014-05-30 | 2014-10-08 | 佛山市神风航空科技有限公司 | Power airship with rotating blade propellers |
-
2014
- 2014-05-30 CN CN201410234073.7A patent/CN104002959B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB277384A (en) * | 1927-09-13 | 1928-08-23 | Wigger Meindersma | Improvements in or relating to water- and aircraft-propellers |
| GB336642A (en) * | 1929-06-18 | 1930-10-20 | Willem Petrus Van Lammeren | Improvements in rotary propellers |
| CN201329955Y (en) * | 2009-01-10 | 2009-10-21 | 安徽省华云高科技有限责任公司 | Rainwater resistance power airship |
| CN201456967U (en) * | 2009-04-02 | 2010-05-12 | 王长林 | airship |
| CN101913425A (en) * | 2010-08-07 | 2010-12-15 | 吴泽峰 | Airship |
| CN202295277U (en) * | 2011-09-29 | 2012-07-04 | 周昶锃 | Novel flying fish |
| CN203864990U (en) * | 2014-05-30 | 2014-10-08 | 佛山市神风航空科技有限公司 | Power airship with rotating blade propellers |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104986319A (en) * | 2015-07-21 | 2015-10-21 | 中国科学院光电研究院 | Vector propelling device, airship and installation method for vector propelling device |
| CN107804481A (en) * | 2017-10-06 | 2018-03-16 | 廖忠民 | Dirigible assist system |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104002959B (en) | 2015-11-11 |
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Effective date of registration: 20170626 Address after: 528226, Guangdong, Foshan City, Nanhai District, lion Town, Luo village, Luen Luen Industrial Zone and Industrial Road Patentee after: Foshan Nanhai Ya Shida Model Co. Ltd. Address before: Foshan City, Guangdong province 528500 city streets Gaoming District No. 78 Jiangwan Road, room 402 Fu Wan Patentee before: Shenfeng science and technology of aviation Co., Ltd of Foshan City |
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