CN107200113B - Too many levels vector promotes spout device - Google Patents

Too many levels vector promotes spout device Download PDF

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Publication number
CN107200113B
CN107200113B CN201710360881.1A CN201710360881A CN107200113B CN 107200113 B CN107200113 B CN 107200113B CN 201710360881 A CN201710360881 A CN 201710360881A CN 107200113 B CN107200113 B CN 107200113B
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link
face
procedure
gear
intermediate link
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CN201710360881.1A
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Chinese (zh)
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CN107200113A (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
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    • 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 propulsion spout device, it is to can adjust improvement of spout to traditional marine propeller, including start-up procedure, intermediate link, end link, rotate gear, driving motor, driving gear etc. form.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 both ends are inclined-plane.All links are connected by the joinery and its construction at both ends, and a gear in end face plane is arranged in one end outer surface of link, and the motor by being connected in another link and gear make link rotate, and then generate deflection.Any angle of the spout between 0 ° -180 ° may be implemented by three intermediate links and a start-up procedure, an end link in the present invention, realizes the effect that ship vector promotes, improves the mobility of ship, has extraordinary prospect.

Description

Too many levels vector promotes spout device
Technical field
The present invention relates to too many levels vectors to promote spout device, is a kind of ship arrow using rotatable too many levels system Amount promotes spout device.
Background technique
Vector propeller is to refer to change the direction of thrust and the propeller of size caused by propeller, passes through change The direction of motion for the fluid that propeller is discharged can make the thrust direction of propeller and size change, and be directly changed thrust The mode of direction and size compared with use rudder face and adjust power device power output the mode reaction time is shorter, effect more It is good, the mobility and flexibility of propeller carrier can be effectively improved, multiple fields have been widely applied to, vector promotes What the thrust direction adjusting of device was mainly realized by adjusting spout, but existing spout structure is complicated, adjusts angular range Deficiency, therefore, develop a kind of vector that can be adjusted in a wide range of promote spout device be it is necessary to and it is valuable.
Summary of the invention
It, can be within the scope of 0 ° -180 ° the purpose of the invention is to provide a kind of too many levels vector propulsion spout device It is adjusted at any angle, the adjusting to thrust direction is realized by the adjusting to spout angle, it can to the adjusting of resisting force sheet To realize the adjusting to output power.
The object of the present invention is achieved like this: including start-up procedure interconnected, intermediate link, end link, institute It states start-up procedure and end link is the column structure that one end is angled end-face, one end is planar end surface composition, intermediate link has three A, each intermediate link is the column structure that both ends are angled end-face, and setting first is prominent on the angled end-face of the start-up procedure Ring is provided with the first driving motor on the first prominent ring, the first driving gear is equipped in the first driving motor output shaft, each It is provided with the first rotate gear on one angled end-face of the intermediate link, is provided with the second prominent ring on another angled end-face, It is provided with the second driving motor on second prominent ring, the second driving gear is installed on the output shaft of the second driving motor, it is described The second rotate gear, the first driving gear and the first intermediate ring connecting with start-up procedure are provided on the angled end-face of end link The first rotate gear engagement of section, the second driving gear of the first intermediate link and the first rotate gear of the second intermediate link are nibbled It closes, the second driving gear of the second intermediate link and the first rotate gear engagement of third intermediate link, third intermediate link Drive gear and the engagement of the second rotate gear.
The invention also includes structure features some in this way:
1. being symmetrically arranged on the first prominent ring, the second prominent ring, there are two the fixations of the correspondence link for connection Pawl.
2. the angled end-face of the angled end-face of start-up procedure, intermediate link and the angled end-face of end link are circular end faces.
3. the angle between each angled end-face and the cross section of corresponding link is 67.5 °, and start-up procedure, intermediate link, The cross-sectional shape of end link is ellipse.
Compared with prior art, the beneficial effects of the present invention are: the present invention is to the adjustable spray of traditional marine propeller The improvement of mouth, the present invention are realized the change of thrust direction by the relative rotation between link, pass through the relative angle for adjusting spout Degree, may be implemented the thrust of any direction in 0- ° 180 °, and rotating mechanism be added on the planar end surface of start-up procedure, or even can To realize the thrust output of up and down direction, the effect of marine propulsion vector propulsion is effectively improved, ship is improved 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 both ends are inclined-plane.The joinery and its construction that all links pass through both ends Connect, by realize that spout is adjusted within the scope of 0 ° -180 ° using the rotary link of multiple interconnections Section.A gear in end face plane is arranged in one end outer surface of link, passes through the motor being connected in another link So that link is rotated with gear, and then generates deflection.Pass through three intermediate links and a start-up procedure, an end-rings Any angle of the spout between 0 ° -180 ° may be implemented in section.It realizes the effect that ship vector promotes, improves the motor-driven of ship Property, there is extraordinary prospect.
Detailed description of the invention
Fig. 1 is the front view of start-up procedure of the invention, uses the planar end surface of start-up procedure as sight plane;
Fig. 2 is the left view of start-up procedure of the invention;
Fig. 3 is the front view of intermediate link of the invention;
Fig. 4 is the left view of intermediate link of the invention;
Fig. 5 is the front view of end link of the invention;
Fig. 6 is the left view of end link of the invention;
Fig. 7 is the front view of 180 ° of states of the invention;
Fig. 8 is the front view of 90 ° of states of the invention;
Fig. 9 is the front view of 0 ° of state of the invention;
Figure 10 is perspective view of the invention.
In figure: 1 start-up procedure body, 2 planar end surfaces, 3 angled end-faces, 4 prominent rings, 5 driving motors, 6 driving gears, 7 fixed jaws 8 Intermediate link body, 9 angled end-faces, 10 angled end-faces, 11 prominent rings, 12 driving motors, 13 driving gears, 14 fixed jaws, 15 turning gears Take turns 16 end link bodies, 17 angled end-faces, 18 planar end surfaces, 19 rotate gear, 20 start-up procedure, 21 first intermediate links, in 22 second Between link, 23 third intermediate links, 24 end links.
Specific embodiment
Present invention is further described in detail with specific embodiment with reference to the accompanying drawing.
In conjunction with 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 by splay end face contact, in gear and fixation Under the constraint of pawl, adjacent link can only in the rotation in surface where angled end-face, the driving force of rotation from driving motor and The driving gear being connected with driving motor, adjacent link can be combined into any angle, pass through the cooperation between multiple links The change of fluid discharge direction may be implemented.At any time, the angled end-face of adjacent two pieces of links all fits closely, adjacent Only allow opposite rotation between the angled end-face of two pieces of links, driving 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 of engagement.Each link is near cylindrical, angled end-face Orthographic drawing be circular.The angle of the bus of the angled end-face and link of link is 67.5 °.One end of start-up procedure is connection The plane of power device, the other end are the inclined-plane connecting with intermediate link, and the shape on inclined-plane is circular, and prominent ring is arranged in outside For fixing driving motor and driving gear, fixed jaw is also installed on prominent ring, the both ends of intermediate link are inclined-plane, inclined-plane Shape is similarly circular, and one end of intermediate link, which is installed, protrudes ring and driving motor, driving gear and fixed jaw, outside the other end Gear is installed in portion, and gear is engaged with the driving gear of previous link start-up procedure or central link, while the pact by fixed jaw Beam and can only be relatively rotated along the end face of a upper link, next link is connected by same mode, until end link, end Only one inclined-plane of end ring section, the other end are 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, driving motor 5, driving gear 6 and consolidates Determine the composition of pawl 7, intermediate link is by intermediate link body 8, angled end-face 9, angled end-face 10, prominent ring 11, driving motor 12, driving gear 13, fixed jaw 14 and rotate gear 15 form, and end link is by end link body 16, angled end-face 17, planar end surface 18 and turning gear 19 composition of wheel.Driving motor 5, driving gear 6 and the fixed jaw 7 of start-up procedure are each attached on prominent ring 4, and prominent ring 4 is fixed In 3 outer of angled end-face of start-up procedure body 1.The both 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 install prominent ring 11, driving motor 12, driving gear 13 and fixed jaw 14 are installed on prominent ring 11.End End ring section one end is angled end-face 17, and the other end is planar end surface 18, the fixed rotate gear 19 in the outer of angled end-face 17.
Too many levels vector of the invention promotes spout device by a start-up procedure, an end link and multiple intermediate rings Section composition, the angled end-face 3 of start-up procedure are connect with the angled end-face 10 of intermediate link, and driving 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 connects, and driving gear 13 is engaged with rotate gear 15 or rotate gear 19, while fixed jaw 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, this mode ensure that the feasibility that link is mutually rotated along angled end-face.
Too many levels vector of the invention promotes the principle of spout device are as follows:
(1) angled end-face 3 of start-up procedure 20 is connect with the angled end-face 10 of the first intermediate link 21, and planar end surface 2 is pushed away with water spray Into the connection of, ducted propeller equal power device, 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 angled end-face 9 and third intermediate link 23, third intermediate link 23 finally with end End ring section 24 connects, and the planar end surface 18 of end link 24 power device is discharged by spout the outlet of fluid, and hydraulic jet propulsion is led Pipe propeller equal power device water be discharged flows through under the action of start-up procedure 20, intermediate link 21,22,23 and end link 22 Change direction;
(2) when driving motor 5,12 works, driving gear 6,13 is rotated, and is driven rotate gear 15,19 to rotate, is made link can To rotate along the angled end-face of a upper link, and rotation axis is the effect of fixed jaw by the normal in the circular angled end-face center of circle It is to provide constraint for link, the angled end-face of next link is made to be close to the angled end-face of a upper link always in the course of rotation, the One intermediate link rotate driving power comes from start-up procedure, and the driving force of end link rotation comes from a upper intermediate ring connected to it Section;
(3) bus of the bus of the first intermediate link 21 and start-up procedure 20 can be made to be in 135 ° by gear rotation, together Sample can be 135 ° by the bus angle of the second intermediate link 22 of rotation 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 of the start-up procedure 20 as fluid inlet with as the end-rings of outlet In the same plane, water (flow) direction changes 180 ° to the planar end surface 18 of section 22, and the direction of water flow is discharged with power device at this time Water (flow) direction completely on the contrary, realize 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 make second respectively around 180 ° of the axis rotation by 17 center of circle of angled end-face 10 and angled end-face When the bus angle of intermediate link 22, third intermediate link 23 and end link 24 is 0 °, the planar end surface 2 and work of start-up procedure 20 18 angle of planar end surface for the end link 22 of outlet is 90 °, and the direction of water flow changes 90 °, realizes lateral promote;
(5) start-up procedure 20, the second intermediate link 22, third intermediate link 23 and end-rings are kept on the basis of (4) It is motionless to save 24, and only makes the first intermediate link 21 around rotating 180 ° by the axis in 10 center of circle of angled end-face 3 or angled end-face, at this time five The normal angle of a link is 0 °, and spout is straight line at this time, and thrust direction is front.

Claims (5)

1. too many levels vector promotes spout device, it is characterised in that: including start-up procedure interconnected, intermediate link, end Link, the start-up procedure and end link are the column structure that one end is angled end-face, one end is planar end surface composition, intermediate ring There are three sections, and each intermediate link is the column structure that both ends are angled end-face, and is arranged on the angled end-face of the start-up procedure One protrudes ring, is provided with the first driving motor on the first prominent ring, the first sliding tooth is equipped in the first driving motor output shaft Wheel is provided with the first rotate gear on one angled end-face of each intermediate link, is provided with second on another angled end-face Ring is protruded, the second driving motor is provided on the second prominent ring, the second sliding tooth is installed on the output shaft of the second driving motor Wheel, is provided with the second rotate gear on the angled end-face of the end link, the first driving gear and connect with start-up procedure the First rotate gear of one intermediate link engages, and the second of the first intermediate link drives first turn of gear and the second intermediate link Moving gear engagement, the second driving gear of the second intermediate link and the first rotate gear of third intermediate link engage, in third Between link driving gear and the second rotate gear engagement.
2. too many levels vector according to claim 1 promotes spout device, it is characterised in that: the first prominent ring, second dash forward Fixed jaw there are two being symmetrically arranged on ring out for the correspondence link of connection.
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 link 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 Answering the angle between the cross section of link is 67.5 °, and the cross-sectional shape of start-up procedure, intermediate link, end link is 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 the cross-sectional shape of start-up procedure, intermediate link, end link is oval Shape.
CN201710360881.1A 2017-05-22 2017-05-22 Too many levels vector promotes spout device Active CN107200113B (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113501123A (en) * 2021-06-29 2021-10-15 浙江天时造船有限公司 Electric push boat

Families Citing this family (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
CN108945354B (en) * 2018-08-28 2020-06-26 江苏科技大学 Underwater and water surface auxiliary propeller

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 (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113501123A (en) * 2021-06-29 2021-10-15 浙江天时造船有限公司 Electric push boat

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