CN107200113A - Too many levels vector promotes spout device - Google Patents

Too many levels vector promotes spout device Download PDF

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Publication number
CN107200113A
CN107200113A CN201710360881.1A CN201710360881A CN107200113A CN 107200113 A CN107200113 A CN 107200113A CN 201710360881 A CN201710360881 A CN 201710360881A CN 107200113 A CN107200113 A CN 107200113A
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China
Prior art keywords
link
face
intermediate link
gear
angled end
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CN201710360881.1A
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Chinese (zh)
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CN107200113B (en
Inventor
胡健
张维鹏
孙士丽
李聪慧
李思朋
孙嘉育
郭磊
耿冲
郭婷
刘立超
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Harbin Engineering University
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Harbin Engineering University
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Priority to CN201710360881.1A priority Critical patent/CN107200113B/en
Publication of CN107200113A publication Critical patent/CN107200113A/en
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H11/00Marine propulsion by water jets
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H11/00Marine propulsion by water jets
    • B63H11/02Marine propulsion by water jets the propulsive medium being ambient water
    • B63H11/10Marine propulsion by water jets the propulsive medium being ambient water having means for deflecting jet or influencing cross-section thereof
    • B63H11/107Direction control of propulsive fluid

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Toys (AREA)

Abstract

The present invention provides a kind of too many levels vector and promotes spout device, and it is the improvement that spout is can adjust to traditional marine propeller, including the composition such as start-up procedure, intermediate link, end link, rotate gear, motor, drive gear.The end face on all inclined-planes is circular, and start-up procedure and end link are a transverse plane, and one end inclined-plane, intermediate link two ends are inclined-plane.All links are connected by the joinery and its construction at two ends, and one end outer surface of link sets a gear in end face plane, link is rotated by the motor and gear that are connected in another link, and then produces deflection.The present invention can realize any angle of the spout between 0 ° 180 ° by three intermediate links and a start-up procedure, an end link, realize the effect that ship vector is promoted, and the mobility of ship be improved, with extraordinary prospect.

Description

Too many levels vector promotes spout device
Technical field
Spout device is promoted the present invention relates to too many levels vector, is that a kind of ship using rotatable too many levels system is sweared Amount promotes spout device.
Background technology
Vector propeller be refer to change propeller produced by thrust direction and the propeller of size, pass through change The direction of motion for the fluid that propeller is discharged can make the thrust direction and size of propeller change, and directly change thrust The mode of direction and size compared with using rudder face and adjust power set power output the mode reaction time is shorter, effect more It is good, mobility and the flexibility of propeller carrier can be effectively improved, multiple fields have been widely applied to, vector is promoted What the thrust direction regulation of device was mainly realized by adjusting spout, but existing spout structure is complicated, adjusts angular range Deficiency, therefore, it can be to be necessary and valuable in a wide range of interior vector propulsion spout device being adjusted to develop a kind of.
The content of the invention
, can be in the range of 0 ° -180 ° the invention aims to provide a kind of too many levels vector to promote spout device Adjusted at any angle, the regulation to thrust direction is realized by the regulation to spout angle, the regulation to resisting force sheet can To realize the regulation to power output.
The object of the present invention is achieved like this:Starting joint, intermediate link including interconnection, end link, institute State start-up procedure and end link is one end is angled end-face, one end is planar end surface composition column structure, intermediate link has Three, each intermediate link be two ends be angled end-face column structure, set on the angled end-face of the start-up procedure first to dash forward Go out to be provided with the first motor, the first driving motor output shaft on ring, the first protrusion ring and the first drive gear is installed, often The first rotate gear is provided with one angled end-face of the individual intermediate link, the second protrusion is provided with another angled end-face It is provided with ring, the second protrusion ring on the second motor, the output shaft of the second motor and the second drive gear is installed, institute Be provided with the second rotate gear on the angled end-face for stating end link, the first drive gear and be connected with start-up procedure first in the middle of The first rotate gear engagement of link, the second drive gear of the first intermediate link and the first rotate gear of the second intermediate link Engagement, the second drive gear of the second intermediate link and the first rotate gear engagement of the 3rd intermediate link, the 3rd intermediate link Drive gear and the second rotate gear engagement.
Present invention additionally comprises some such architectural features:
1. first protrusion ring, second protrusion ring on be respectively symmetrically provided with two be used for connect corresponding joint fixation Pawl.
2. the angled end-face of the angled end-face of start-up procedure, intermediate link and the angled end-face in end joint are circular end faces.
3. the angle between each angled end-face and the cross section of corresponding link is 67.5 °, and starting joint, intermediate link, The shape of cross section of end link is ellipse.
Compared with prior art, the beneficial effects of the invention are as follows:The present invention is to the adjustable spray of traditional marine propeller The improvement of mouth, the present invention realizes the change of thrust direction by the relative rotation between link, by the relative angle for adjusting spout Degree, it is possible to achieve the thrust of any direction in 0- ° 180 °, and rotating mechanism is added on the planar end surface of start-up procedure, or even can Exported with the thrust for realizing above-below direction, be effectively improved the effect of marine propulsion vector propulsion, improve ship Flexibility, has immense value to shipbuilding industry and shipping business.
All links of the present invention are all nearly cylinder, and the end face on all inclined-planes is circular, start-up procedure and end End ring section is a transverse plane, and one end inclined-plane, intermediate link two ends are inclined-plane.The joinery and its construction that all links pass through two ends To connect, what is passed through realizes that spout is adjusted in the range of 0 ° -180 ° using the rotary link of multiple interconnections Section.One end outer surface of link sets a gear in end face plane, passes through the motor being connected in another link Link is rotated with gear, and then produce deflection.Pass through three intermediate links and start-up procedure, an end-rings Section can realize any angle of the spout between 0 ° -180 °.The effect that ship vector is promoted is realized, the motor-driven of ship is improved Property, with extraordinary prospect.
Brief description of the drawings
Fig. 1 is the front view of the start-up procedure of the present invention, and the planar end surface using start-up procedure is used as sight plane;
Fig. 2 is the left view of the start-up procedure of the present invention;
Fig. 3 is the front view of the intermediate link of the present invention;
Fig. 4 is the left view of the intermediate link of the present invention;
Fig. 5 is the front view of the end link of the present invention;
Fig. 6 is the left view of the end link of the present invention;
Fig. 7 is the front view of 180 ° of states of the present invention;
Fig. 8 is the front view of 90 ° of states of the present invention;
Fig. 9 is the front view of 0 ° of state of the present invention;
Figure 10 is stereogram of the invention.
In figure:1 start-up procedure body, 2 planar end surfaces, 3 angled end-faces, 4 protrude ring, 5 motors, 6 drive gears, 7 fixed claws 8 Intermediate link body, 9 angled end-faces, 10 angled end-faces, 11 protrude ring, 12 motors, 13 drive gears, 14 fixed claws, 15 turning gears Take turns 16 end link bodies, 17 angled end-faces, 18 planar end surfaces, the start-up procedure of 19 rotate gear 20,21 first intermediate links, in 22 second Between link, 23 the 3rd intermediate links, 24 end links.
Embodiment
The present invention is described in further detail with embodiment below in conjunction with the accompanying drawings.
With reference to Fig. 1 to Figure 10, too many levels vector of the invention promotes spout device by start-up procedure, intermediate link, end Link, rotate gear, rotary electric machine, control system composition.Two adjacent links are contacted by angled end-face, in gear and fixation Under the constraint of pawl, adjacent link can only in the rotation with surface where angled end-face, the driving force of rotation from motor and The drive gear being connected with motor, adjacent link can be combined into any angle, pass through the cooperation between multiple links The change of fluid discharge direction can be realized.At any time, the angled end-face of adjacent two pieces of links is all brought into close contact, adjacent Only allow relative rotation between the angled end-face of two pieces of links, motor and rotate gear are each attached to angled end-face outer, drive Moving gear drives the change of angle between the rotate gear realization link engaged.Each link is near cylindrical, angled end-face Orthographic drawing be circular.The angle of the angled end-face of link and the bus of link is 67.5 °.One end of start-up procedure is connection The plane of power set, the other end is the inclined-plane that be connected with intermediate link, and inclined-plane is shaped as circular, and outside sets protrusion ring For fixed drive motor and drive gear, fixed claw is also installed on prominent ring, the two ends of intermediate link are inclined-plane, inclined-plane Shape is similarly circular, and one end of intermediate link is installed outside prominent ring and motor, drive gear and fixed claw, the other end Gear is installed in portion, and gear is engaged with the drive gear of previous link start-up procedure or central link, while by the pact of fixed claw Beam and can only be relatively rotated along the end face of a upper link, next link connected by same mode, until end link, end End ring section only one of which inclined-plane, the other end is vertical plane, and gear is installed in inclined-plane outer.
Start-up procedure is by start-up procedure body 1, planar end surface 2, angled end-face 3, protrusion ring 4, motor 5, drive gear 6 and consolidates Determine pawl 7 to constitute, intermediate link is by intermediate link body 8, angled end-face 9, angled end-face 10, prominent ring 11, motor 12, drive gear 13rd, fixed claw 14 and rotate gear 15 are constituted, and end link is by end link body 16, angled end-face 17, planar end surface 18 and turning gear Wheel 19 is constituted.Motor 5, drive gear 6 and the fixed claw 7 of start-up procedure are each attached on prominent ring 4, and prominent ring 4 is fixed In the outer of angled end-face 3 of start-up procedure body 1.The two ends of intermediate link are angled end-face, and turning gear is installed in the outer of angled end-face 10 Wheel, the outer of angled end-face 9 is installed installs motor 12, drive gear 13 and fixed claw 14 on prominent ring 11, prominent ring 11.End End ring section one end is angled end-face 17, and the other end is planar end surface 18, and rotate gear 19 is fixed in the outer of angled end-face 17.
The too many levels vector of the present invention promotes spout device by a start-up procedure, an end link and multiple middle rings Section composition, the angled end-face 3 of start-up procedure is connected with the angled end-face 10 of intermediate link, and drive gear 6 is engaged with rotate gear 15, Gu Determine the face of gear that pawl 7 is close to rotate gear 15, the angled end-face 9 of intermediate link and the angled end-face 10 of next intermediate link or end The angled end-face 17 of end ring section is connected, and drive gear 13 is engaged with rotate gear 15 or rotate gear 19, while fixed claw 14 is close to The face of gear of rotate gear 15 or rotate gear 19.
All angled end-faces are in 67.5 ° with link bus, and angled end-face is circular, the link section shape vertical with bus Shape is ellipse, and this mode ensure that the feasibility that link is mutually rotated along angled end-face.
The present invention too many levels vector promote spout device principle be:
(1) angled end-face 3 of start-up procedure 20 is connected with the angled end-face 10 of the first intermediate link 21, and planar end surface 2 is pushed away with water spray Enter, ducted propeller equal power device is connected, as the import of fluid, the first intermediate link 21 passes through in angled end-face 9 and second Between link 22 connect, the second intermediate link 22 by the intermediate link 23 of angled end-face 9 and the 3rd, the 3rd intermediate link 23 finally with end End ring section 24 is connected, and the planar end surface 18 of end link 24 is discharged the outlet of fluid by spout to power set, hydraulic jet propulsion, is led Pipe propeller equal power device is discharged in the presence of water flows through start-up procedure 20, intermediate link 21,22,23 and end link 22 Change direction;
(2) when motor 5,12 works, drive gear 6,13 is rotated, and is driven rotate gear 15,19 to rotate, is made link can To be rotated along the angled end-face of a upper link, and rotary shaft is the normal by the circular angled end-face center of circle, the effect of fixed claw It is to provide constraint for link, the angled end-face of next link is close to the angled end-face of a link all the time during rotation, the One intermediate link rotates driving force and comes from start-up procedure, and the driving force that end link is rotated comes from a connected upper middle ring Section;
(3) it is in 135 ° with the bus of start-up procedure 20 that can make the bus of the first intermediate link 21 by pinion rotation, together Sample can be 135 ° by the bus angle for rotating the second intermediate link 22 and the first intermediate link 21, and when the phase of five links When adjacent link bus angle is 135 °, the planar end surface 2 and the end-rings as outlet of the start-up procedure 20 of fluid inlet are used as At grade, water (flow) direction changes 180 ° to the planar end surface 18 of section 22, and now the direction of current is discharged with power set Water (flow) direction completely on the contrary, realizing reverse propulsion;
(4) keep start-up procedure 20, the first intermediate link 21 and the second intermediate link 22 motionless on the basis of (3), the Three intermediate links 23 and end link 24 rotate 180 ° respectively around by angled end-face 10 and the axle in the center of circle of angled end-face 17, make second When the bus angle of intermediate link 22, the 3rd intermediate link 23 and end link 24 is 0 °, the planar end surface 2 of start-up procedure 20 is with making The angle of planar end surface 18 for the end link 22 of outlet is 90 °, and the direction of current changes 90 °, realizes lateral promote;
(5) start-up procedure 20, the second intermediate link 22, the 3rd intermediate link 23 and end-rings are kept on the basis of (4) Save 24 motionless, and only make the first intermediate link 21 around rotating 180 ° by angled end-face 3 or the axle in the center of circle of angled end-face 10, now five The normal angle of individual link is 0 °, and now spout is straight line, and thrust direction is front.

Claims (5)

1. too many levels vector promotes spout device, it is characterised in that:Starting joint, intermediate link, end including interconnection Link, the start-up procedure and end link are the column structures that one end is angled end-face, one end is planar end surface composition, middle Link has three, each intermediate link be two ends be angled end-face column structure, set on the angled end-face of the start-up procedure It is provided with first protrusion ring, the first protrusion ring in the first motor, the first driving motor output shaft and the first driving is installed The first rotate gear is provided with gear, an angled end-face of each intermediate link, the is provided with another angled end-face It is provided with two protrusion rings, the second protrusion ring on the second motor, the output shaft of the second motor and the second driving is installed It is provided with the second rotate gear on gear, the angled end-face of the end link, the first drive gear and is connected with start-up procedure The first rotate gear engagement of first intermediate link, the second drive gear of the first intermediate link and the first of the second intermediate link Rotate gear is engaged, the second drive gear of the second intermediate link and the first rotate gear engagement of the 3rd intermediate link, the 3rd The drive gear of intermediate link and the engagement of the second rotate gear.
2. too many levels vector according to claim 1 promotes spout device, it is characterised in that:First protrusion ring, second dash forward Go out on ring to be respectively symmetrically provided with two be used for connect corresponding joint fixed claw.
3. too many levels vector according to claim 1 or 2 promotes spout device, it is characterised in that:The splay end of start-up procedure The angled end-face in face, the angled end-face of intermediate link and end joint is circular end face.
4. too many levels vector according to claim 1 or 2 promotes spout device, it is characterised in that:Each angled end-face with it is right It is 67.5 ° to answer the angle between the cross section of link, and starting joint, intermediate link, the shape of cross section of end link are Ellipse.
5. too many levels vector according to claim 3 promotes spout device, it is characterised in that:Each angled end-face and corresponding ring Angle between the cross section of section is 67.5 °, and starting joint, intermediate link, the shape of cross section of end link are oval Shape.
CN201710360881.1A 2017-05-22 2017-05-22 Too many levels vector promotes spout device Active CN107200113B (en)

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Application Number Priority Date Filing Date Title
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Application Number Priority Date Filing Date Title
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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108170971A (en) * 2018-01-09 2018-06-15 海南大学 A kind of design method of vector spout and vector spout
CN108945354A (en) * 2018-08-28 2018-12-07 江苏科技大学 A kind of underwater and water surface auxiliary propeller

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113501123B (en) * 2021-06-29 2022-04-26 浙江天时造船有限公司 Electric push boat

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2569232A1 (en) * 1984-08-16 1986-02-21 Rolls Royce ADJUSTABLE EXHAUST NOZZLE FOR A GAS TURBOMACHINE
GB2196587A (en) * 1980-10-31 1988-05-05 Rolls Royce Aircraft jet pipe having angularly adjustable nozzle
CN103939235A (en) * 2014-04-25 2014-07-23 西北工业大学 Rotary thrust vectoring nozzle for short-distance vertical take-off and landing engine
CN106014682A (en) * 2016-06-20 2016-10-12 李新亚 Vector nozzle of jet engine installed on submarine
CN205872443U (en) * 2016-05-10 2017-01-11 成都前沿动力科技有限公司 Rotary mechanism suitable for VTOL unmanned aerial vehicle 90 degree thrust vectoring nozzle

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2196587A (en) * 1980-10-31 1988-05-05 Rolls Royce Aircraft jet pipe having angularly adjustable nozzle
FR2569232A1 (en) * 1984-08-16 1986-02-21 Rolls Royce ADJUSTABLE EXHAUST NOZZLE FOR A GAS TURBOMACHINE
CN103939235A (en) * 2014-04-25 2014-07-23 西北工业大学 Rotary thrust vectoring nozzle for short-distance vertical take-off and landing engine
CN205872443U (en) * 2016-05-10 2017-01-11 成都前沿动力科技有限公司 Rotary mechanism suitable for VTOL unmanned aerial vehicle 90 degree thrust vectoring nozzle
CN106014682A (en) * 2016-06-20 2016-10-12 李新亚 Vector nozzle of jet engine installed on submarine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108170971A (en) * 2018-01-09 2018-06-15 海南大学 A kind of design method of vector spout and vector spout
CN108945354A (en) * 2018-08-28 2018-12-07 江苏科技大学 A kind of underwater and water surface auxiliary propeller
WO2020042686A1 (en) * 2018-08-28 2020-03-05 江苏科技大学 Underwater and surface auxiliary propeller
CN108945354B (en) * 2018-08-28 2020-06-26 江苏科技大学 Underwater and water surface auxiliary propeller

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