CN102285444A - Kite airship attitude adjusting device - Google Patents

Kite airship attitude adjusting device Download PDF

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Publication number
CN102285444A
CN102285444A CN2011101497111A CN201110149711A CN102285444A CN 102285444 A CN102285444 A CN 102285444A CN 2011101497111 A CN2011101497111 A CN 2011101497111A CN 201110149711 A CN201110149711 A CN 201110149711A CN 102285444 A CN102285444 A CN 102285444A
Authority
CN
China
Prior art keywords
gear
kite
mooring
motor
rotating shaft
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN2011101497111A
Other languages
Chinese (zh)
Inventor
袁晓敏
严后选
王祥生
杨柳
黄岩慧
刘萍
王莲英
张功学
耿其亚
吴坚
李正雄
高升
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BEIFANG DIANKE GROUP Co Ltd
Original Assignee
BEIFANG DIANKE GROUP Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by BEIFANG DIANKE GROUP Co Ltd filed Critical BEIFANG DIANKE GROUP Co Ltd
Priority to CN2011101497111A priority Critical patent/CN102285444A/en
Publication of CN102285444A publication Critical patent/CN102285444A/en
Pending legal-status Critical Current

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Abstract

The invention discloses a kite airship attitude adjusting device, which comprises a chain, a first gear, a second gear, a U-shaped support, a motor, a speed reducer and a chain wheel. The chain is installed on the chain wheel. The chain wheel is installed on a rotating shaft. The rotating shaft is installed on the U-shaped support through two bearings. The first gear is installed at one end of the rotating shaft which stretches out of the external side of the U-shaped support. The first gear is engaged with the second gear. The motor and the speed reducer are fixed on the U-shaped support. The shafts of the motor and the speed reducer drive the second gear. The axes of the rotating shaft, the first gear, the second gear, the motor and the speed reducer are in parallel with each other. The kite airship attitude adjusting device has the advantages that the requirement on the control of the pitch attitude of the kite airship through effective loads can be satisfied; by increasing the pitch attitude of the kite airship, the deviation distance of the kite airship can be reduced; and by reducing the pitch attitude of the kite airship, the pulling force of a kite cable can be reduced and the wind loading rating of the kite airship can be improved.

Description

Mooring ship attitude regulating mechanism
Technical field
The invention belongs to the structure or the annex of the aircraft stabilising surface that is lighter than air, particularly a kind of mooring ship attitude regulating mechanism.
Background technology
The skyborne pitch attitude of present mooring ship both domestic and external (ball) is subjected to aspect decisions such as centre of buoyancy, center of gravity, hawser mooring position, the pneumatic effect wind-force of empennage size, after the design of mooring ship is finished, attitude when aloft moving can not active adjustment, depends on the wind-force size fully.Wind-force is big more, and the elevation angle of mooring ship is big more, and mooring ship deviation post is big more, and the pulling force of hawser is big more.The mooring ship aloft all can not be regulated the position of mooring hawser both at home and abroad at present, makes the pitch attitude of mooring ship be determined by initial designs situation and external environment fully.Aloft, the mooring ship is subjected to wind effect and produces new line, and makes the skew of mooring ship box haul.Under identical wind effect, the pitch attitude of mooring ship is identical with departure distance.When wind-force increased, the elevation angle and departure distance all increased.Along with the increase of wind-force, mooring ship cable stress also increases gradually.Operating personal can't be interfered this situation.
Summary of the invention
The object of the present invention is to provide a kind of skyborne attitude of mooring ship that makes to carry out active adjustment, so that the mooring ship attitude regulating mechanism of the pitch attitude of control mooring ship, departure distance, cable stress.
The technical solution that realizes the object of the invention is: a kind of mooring ship attitude regulating mechanism, comprise chain, first gear, second gear, U type support, motor and retarder, sprocket wheel, chain is installed on the sprocket wheel, this sprocket wheel is installed in the rotating shaft, this rotating shaft is passed through two bearing installations on U type support, on the end outside U type support is stretched out in rotating shaft first gear is installed, this first gear and second gear mesh, motor and retarder are fixed on the U type support, the axle of this motor and retarder drives second gear, rotating shaft, first gear, second gear, parallel axes between motor and the retarder.
The present invention compared with prior art, its remarkable advantage: (1) can satisfy the control requirement of capacity weight to the pitch attitude of mooring ship.(2) increase the pitch attitude of mooring ship, can reduce mooring ship deviation distance.(3) reduce the pitch attitude of mooring ship, the mooring hawser pull is reduced, improve mooring ship wind loading rating.(4) can change mooring ship hawser initial position, adapt to the variation of capacity weight.
Below in conjunction with accompanying drawing the present invention is described in further detail.
Description of drawings
Fig. 1 is the three-dimensional structure scheme drawing of mooring ship attitude regulating mechanism of the present invention.
Fig. 2 is a front view of the present invention.
Fig. 3 is a birds-eye view of the present invention.
Fig. 4 is the cutaway view of Fig. 2.
Fig. 5 is an application scheme drawing of the present invention.
The component part of Reference numeral and representative thereof is: 1 is chain, 2,4 is gear, 3 main push-towing rope rope mooring rings, and 5 is support, 6 are rotating shaft, 7 is motor and retarder, and 8 is sprocket wheel, and 9 is positioning plate, 10 are mooring ship (ball), 11 are mooring ship attitude regulating mechanism of the present invention, and 12 are mooring ship (ball) main push-towing rope rope, and 13 are mooring branch hawser.
The specific embodiment
In conjunction with Fig. 1, Fig. 2, Fig. 3 and Fig. 4, mooring ship attitude regulating mechanism of the present invention, by the sprocket wheel link chain mechanism front and back cable length ratio of mooring ship (ball) is regulated, the mooring point front and back position that changes mooring ship (ball) main push-towing rope rope changes strained condition, thereby regulates the pitch attitude of mooring ship.Concrete structure comprises chain 1, first gear 2, second gear 4, U type support 5, motor and retarder 7, sprocket wheel 8, chain 1 is installed on the sprocket wheel 8, this sprocket wheel 8 is installed in the rotating shaft 6, this rotating shaft 6 is passed through two bearing installations on U type support 5, stretch out in rotating shaft 6 first gear 2 is installed on the end in U type support 5 outsides, this first gear 2 and 4 engagements of second gear, motor and retarder 7 are fixed on the U type support 5, the axle of this motor and retarder 7 drives second gear 4, the parallel axes between rotating shaft 6, first gear 2, second gear 4, motor and the retarder 7.
Welding is used for fixing the main push-towing rope rope mooring ring 3 of mooring ship main push-towing rope rope in the U-bottom portion of the U type support 5 of mooring ship attitude regulating mechanism of the present invention.On the U type support 5 between the U-bottom portion of sprocket wheel 8 and U type support 5, prevent the positioning plate 9 that chain 1 comes off from sprocket wheel 8 by the screw installation.The reduction ratio of first gear 2 and second gear 4 is 5-3: 1
The present invention with sprocket wheel 8 by two bearing installations on U type support 5, motor and retarder 7 drive sprocket wheels 1 by second gear 4 and first gear 2 and realize rotating, and drive chain 1 again and realize adjusting to length ratio before and after mooring ship (ball) hawser.
Application mode of the present invention as shown in Figure 5.Lie in respectively on the present invention 11 the chain 1 by the front and back mooring branch hawser 13 with mooring ship (ball) 10, mooring ship (ball) main push-towing rope rope 12 lies on the present invention 11 the main push-towing rope rope mooring ring 3.By regulating motor of the present invention and retarder 7 length ratio on chain 1 both sides is changed, thereby change the pitch attitude of mooring ship (ball) 10.Under certain wind speed, when the pitch angle of mooring ship (ball) 10 reduces, thereby reduce the vertical gas dynamic lift and the horizontal gas dynamic resistance of mooring ship (ball) 10, reduce 12 suffered making a concerted effort of mooring ship (ball) main push-towing rope rope, vice versa, realizes the stressed effective control of mooring ship (ball) main push-towing rope rope 12.
Can change the stressed relation of mooring ship (ball) 10 in the time of the change of attitude, when attitude reduces, the horizontal-shift of mooring ship (ball) 10 is apart from increase, otherwise the horizontal-shift distance reduces when attitude increases, thereby realizes the effective control to the horizontal-shift distance of mooring ship (ball) 10.
There is confidential relation the initial mooring point position of mooring ship (ball) 10 and payload weight and installation site, and when effective load weight and position changed, mooring point position also needed to change thereupon.The present invention can be used to regulate mooring point position, thereby satisfies such operating needs.
What want special version here is, Fig. 1 and Fig. 5 draw with UG software, is for the ease of understanding, and is not photo or picture, with the be beyond expression relation of its 3 D stereo of CAD software.

Claims (4)

1. mooring ship attitude regulating mechanism, it is characterized in that comprising chain (1), first gear (2), second gear (4), U type support (5), motor and retarder (7), sprocket wheel (8), chain (1) is installed on the sprocket wheel (8), this sprocket wheel (8) is installed in the rotating shaft (6), this rotating shaft (6) is passed through two bearing installations on U type support (5), on the end outside U type support (5) is stretched out in rotating shaft (6) first gear (2) is installed, this first gear (2) and second gear (4) engagement, motor and retarder (7) are fixed on the U type support (5), the axle of this motor and retarder (7) drives second gear (4), rotating shaft (6), first gear (2), second gear (4), parallel axes between motor and the retarder (7).
2. mooring ship attitude regulating mechanism according to claim 1 is characterized in that welding in the U-bottom portion of U type support (5) is used for fixing the main push-towing rope rope mooring ring (3) of mooring ship main push-towing rope rope.
3. mooring ship attitude regulating mechanism according to claim 1 is characterized in that the U type support (5) between the U-bottom portion of sprocket wheel (8) and U type support (5) upward prevents the positioning plate (9) that chain (1) comes off from sprocket wheel (8) by the screw installation.
4. mooring ship attitude regulating mechanism according to claim 1 is characterized in that the reduction ratio of first gear (2) and second gear (4) is 5-3: 1
CN2011101497111A 2011-06-07 2011-06-07 Kite airship attitude adjusting device Pending CN102285444A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2011101497111A CN102285444A (en) 2011-06-07 2011-06-07 Kite airship attitude adjusting device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2011101497111A CN102285444A (en) 2011-06-07 2011-06-07 Kite airship attitude adjusting device

Publications (1)

Publication Number Publication Date
CN102285444A true CN102285444A (en) 2011-12-21

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN2011101497111A Pending CN102285444A (en) 2011-06-07 2011-06-07 Kite airship attitude adjusting device

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CN (1) CN102285444A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3062370A1 (en) * 2017-01-27 2018-08-03 Marcos Benatar AIRCRAFT
CN108438198A (en) * 2018-03-31 2018-08-24 丹阳昊天飞行器技术有限公司 A kind of pulley buncher

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0933292A2 (en) * 1998-01-28 1999-08-04 Dentsu Tec Inc. Tethered balloon
ES2174715A1 (en) * 2000-07-26 2002-11-01 Ortega Juan Carlos Pettinari System of permanent surveillance with the help of captive globes.
CN2574995Y (en) * 2002-09-13 2003-09-24 中国科学院大气物理研究所 Disc shape aerobat
US20060060695A1 (en) * 2004-06-21 2006-03-23 Walden Michael K Mass transfer system for stabilizing an airship and other vehicles subject to pitch and roll moments
CN201350969Y (en) * 2008-12-27 2009-11-25 中国特种飞行器研究所 Tethered balloon bowknot device
WO2011012996A2 (en) * 2009-07-28 2011-02-03 Noce S.R.L. Improved self-righting aerostat and relative takeoff and recovery system
CN102030100A (en) * 2009-09-28 2011-04-27 渠仁书 Pavilion leveling device
CN202244074U (en) * 2011-06-07 2012-05-30 北方电科集团有限公司 Posture adjusting device of kite-airship

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0933292A2 (en) * 1998-01-28 1999-08-04 Dentsu Tec Inc. Tethered balloon
ES2174715A1 (en) * 2000-07-26 2002-11-01 Ortega Juan Carlos Pettinari System of permanent surveillance with the help of captive globes.
CN2574995Y (en) * 2002-09-13 2003-09-24 中国科学院大气物理研究所 Disc shape aerobat
US20060060695A1 (en) * 2004-06-21 2006-03-23 Walden Michael K Mass transfer system for stabilizing an airship and other vehicles subject to pitch and roll moments
CN201350969Y (en) * 2008-12-27 2009-11-25 中国特种飞行器研究所 Tethered balloon bowknot device
WO2011012996A2 (en) * 2009-07-28 2011-02-03 Noce S.R.L. Improved self-righting aerostat and relative takeoff and recovery system
CN102030100A (en) * 2009-09-28 2011-04-27 渠仁书 Pavilion leveling device
CN202244074U (en) * 2011-06-07 2012-05-30 北方电科集团有限公司 Posture adjusting device of kite-airship

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3062370A1 (en) * 2017-01-27 2018-08-03 Marcos Benatar AIRCRAFT
CN108438198A (en) * 2018-03-31 2018-08-24 丹阳昊天飞行器技术有限公司 A kind of pulley buncher

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Application publication date: 20111221