CN103085961B - Decompression accelerator - Google Patents

Decompression accelerator Download PDF

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Publication number
CN103085961B
CN103085961B CN201110339336.7A CN201110339336A CN103085961B CN 103085961 B CN103085961 B CN 103085961B CN 201110339336 A CN201110339336 A CN 201110339336A CN 103085961 B CN103085961 B CN 103085961B
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China
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blade
outer container
helical blade
power
shaped
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Expired - Fee Related
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CN201110339336.7A
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Chinese (zh)
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CN103085961A (en
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李僖年
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Individual
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Individual
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Abstract

The invention relates to a decompression accelerator comprising an outer box, a driving wheel, a paddle fixing wheel and spiral paddles. One push-and-pull groove is reserved on the inner side wall of each spiral paddle, a power arm is mounted in each push-and-pull groove in a guide-and-slide mode, and one arc baffle is arranged on the outer side wall of each spiral paddle. One arc paddle groove is formed between each arc baffle and the outer side wall of each spiral paddle. The decompression accelerator is mounted at the front end of an underwater vehicle. Through rotation of the spiral paddles, resisting force of frontal water flow generated during sailing is changed in direction, leaves a nose and spreads out around the nose; and a transverse-moving water curtain vertical to the heading is formed in front of the nose to prevent the nose from being hindered by the resisting force of the frontal water flow, so that frontal resisting force caused by route speed is reduced to the utmost, speed of the underwater vehicle is accelerated, voyage is extended, sailing duration is prolonged, energy is saved, and a higher maneuvering level of ships is achieved.

Description

Decompression accelerator
Technical field
The present invention relates to accelerator field, the Decompression accelerator that in especially a kind of water, aircraft uses.
Background technology
In water aircraft as steamer, Submarine and torpedo etc. advance in water time, the front end due to aircraft can run into the resistance of head-on current, and therefore the speed of advance of aircraft is usually slower.In order to improve the speed that aircraft is advanced, the mode of usual employing increase power overcomes the resistance of water, thus promote aircraft advance, though aforesaid way is widely used, but the power increasing aircraft is higher to technical requirements, not easily realize, but also the use amount of the energy can be increased, improve the manufacturing cost of aircraft.
Summary of the invention
The object of the invention is to overcome the deficiencies in the prior art, provide a kind of reasonable in design, easy to use, easy to manufacture, resistance suffered by aircraft can be reduced and improve the Novel pressure relief accelerator of aircraft speed of advance.
The object of the invention is to be realized by following technological means:
A kind of Decompression accelerator, it is characterized in that: comprise outer container, drive wheel, blade tight pulley and helical blade, in outer container, an electrical motor is installed, drive wheel coaxial package is on the motor power axle being positioned at outer container outside and move axially along dynamical axis, and the outer wall of drive wheel is shaped with one group of circumferentially uniform power arm; The blade of the dynamical axis front end of blade tight pulley coaxial package outside drive wheel is fixed on wheel shaft, helical blade is arranged on blade tight pulley by stay hook that its underpart is made is uniform, the madial wall of each helical blade all makes a push/pull slot, all lead in each push/pull slot the power arm that is slidably installed, the lateral wall of each helical blade all makes a curved baffle, forms the arc blade groove that the hand of rotation of an opening direction and helical blade is identical between this curved baffle with helical blade lateral wall.
And described outer container is the barrel-shaped of sealing, and install a motor bench in outer container, electrical motor is arranged in this motor bench, the dynamical axis of this electrical motor passes the top cover of outer container and extends to outside top cover.
And, at the lateral wall of outer container top cover, the water sealing device that is positioned at dynamical axis periphery is installed, at the madial wall of outer container top cover, the water collection device that is positioned at dynamical axis periphery is installed, this water collection device is connected by distribution tube with the polywater case being arranged on outer container inner bottom part, is provided with leakage inductive device and drain tube holes in this polywater case.
And, described dynamical axis is arranged the power post of three circumferentially uniform settings, the inwall of drive wheel axis hole makes a lifting groove, the middle part of lifting groove inner lower edge is provided with power column inlet, three power posts on dynamical axis are inserted in the lifting groove of drive wheel axis hole, and along lifting groove guiding movement.
And described dynamical axis is coaxially fixedly mounted with a lifting wheel, and the inwall of this lifting wheel installs power post, and the outer wall of drive wheel spirals and is shaped with lifting groove, and power post is arranged in lifting groove, and along lifting groove guiding movement.
And a T-shaped push-and-pull head is all made in the front end of described each power arm, the made push/pull slot of each helical blade madial wall is also T-shaped, and this T-shaped push-and-pull head guiding is slidably mounted in T-shaped push/pull slot.
And have the circular wheel of axis hole centered by blade tight pulley, the outside of blade tight pulley is inclination six shapes, and the top on inclined-plane is blade anchor shaft; The stay hook undercut for stay hook activity is had in the inner side of axle.
And install a blade stay hook pressure ring on blade tight pulley, the outer wall top of this blade stay hook pressure ring is pressed on the outer wall of helical blade bottom stay hook.
And, coaxial installation one helix closing lid on described dynamical axis, this helix closing lid is shaped with the gap matched with helical blade shape and quantity, the madial wall of helix closing lid is shaped with power-assisted eaves, the outer garden of closing lid is provided with a clamping ring, makes closing lid become an entirety.
Advantage of the present invention and good effect are:
1, this accelerator is arranged on the bow position of aircraft in water, by the rotation of helical blade, change the water (flow) direction at bow place, make current before bow, form the water curtain of the cross motion vertical with course, thus reduce aircraft is subject in water head resistance, improve the speed of aircraft in water.
2, this accelerator structure simple, easy to manufacture, be easy to production and processing, easy for installation, and use this accelerator can not cause the increase of energy dissipation and productive costs.
3, this accelerator is applied widely, when adopt lifting wheel structure is installed time, this accelerator can entirety extend forward, makes to have between water curtain and naval vessel the distance that is appropriate, larger effect can be played, be applicable to be arranged on the larger bulbous bow of large ship or bow or larger plane.In addition, this structure can reduce draws bubble phenomenon, is particularly suitable for being arranged on submarine.
4, the present invention is that a kind of structure is simple, design science, safe and reliable, practical, Decompression accelerator applied widely, this acceleration device is arranged on the front end of aircraft, by the rotation of screw type blade, the head-on resistance to water-flow produced during navigation is made to change direction, leave fore, all around scattering forward, the water curtain of the cross motion vertical with course is formed before bow, bow is not stopped by the resistance of the current that head on, thus the head-on resistance to water-flow farthest reduced because route speed produces, the speed of aircraft is accelerated, voyage strengthens, cruise duration extends, save the energy simultaneously, naval vessel is made to rise to higher motor-driven horizontal level.
Accompanying drawing explanation
Fig. 1 is front view of the present invention;
Fig. 2 a is the schematic cross-section of drive wheel;
Fig. 2 b is the open and flat schematic diagram of lifting groove;
Fig. 2 c is the front view of drive wheel;
Fig. 3 a is the front view of dynamical axis;
Fig. 3 b is the right elevation of dynamical axis;
Fig. 4 a is the front view of helical blade;
Fig. 4 b is the right elevation of helical blade;
Fig. 4 c is that the A-A of Fig. 4 b is to three-dimensional cutaway view;
Fig. 4 d is the birds-eye view of blade slot part;
Fig. 5 a is the assembly drowing of blade tight pulley and blade stay hook pressure ring;
Fig. 5 b is the right elevation of Fig. 5 a;
Fig. 5 c is the front view of blade stay hook pressure ring;
Fig. 5 d is the left view of Fig. 5 c;
Fig. 6 a is the front view of helix closing lid;
Fig. 6 b is the left view of helix closing lid;
Fig. 7 a is the scheme of installation of outer container and aircraft;
Fig. 7 b is the front view of outer container;
Fig. 8 is use schematic diagram of the present invention;
Fig. 9 is the dynamical axis of another embodiment and the assembling schematic diagram of lifting wheel;
Figure 10 is the schematic diagram of the dynamical axis in Fig. 9;
Figure 11 a is the front view of lifting wheel in Fig. 9;
Figure 11 b is the right elevation of Figure 11 a;
Figure 12 is the use schematic diagram of another embodiment.
Detailed description of the invention
Embodiments of the invention are described in detail below in conjunction with accompanying drawing; It should be noted that, the present embodiment is narrative, is not determinate, can not limit protection scope of the present invention with this.
A kind of Decompression accelerator, comprises outer container 17, drive wheel 15, blade tight pulley 13 and helical blade 8, is described in detail below to each several part parts:
1. outer container:
(1). outer container is the barrel-shaped of sealing, and with longitudinal fixing groove 21 until outer box plate, there is fixing threaded hole at the groove place of base plate, makes the rear portion of outer container be fixed on hull 30 internal fixation plate; Outer container top cover eaves has fixing threaded hole, and make casing be fixedly mounted on the bulbous bow on naval vessel or naval vessel drinking water with the position of the middle of lower part, be set in the bulbous bow of ship, the pretectum of outer container and hull become plane after fixing.
(2). install a motor bench 20 in outer container, this motor bench is installed electrical motor 18, be provided with binding post 22 and the electric wire 23 of fixing also waterproof in outer container, this binding post connects with the power supply outside case, for electrical motor provides required power supply; At the lateral wall of outer container top cover 25, the water sealing device 26 that is positioned at motor power axle 1 periphery is installed, at the madial wall of outer container top cover, the water collection device 28 that is positioned at motor power axle periphery is installed, this water collection device is tightly connected by distribution tube 29 with the polywater case 24 being arranged on outer container inner bottom part, leakage inductive device and drain tube holes is provided with in this polywater case, drain tube holes fixes a drainpipe 34, this drain hose is connected with ship displacement system, makes unexpected or percolating water discharge Decompression accelerator outer container in time.
(3). the top cover center of outer container is provided with dynamical axis axis hole, bearing set 27 on the dynamical axis of electrical motor, and this dynamical axis passes the axis hole of top cover and extends to outside top cover.
2. drive wheel:
(1). drive wheel is circular wheel, and its center is drive shaft hole.The outer wall of drive wheel is shaped with one group of circumferentially uniform power arm 4, and a horizontal cylinder is all made in the front end of each power arm, forms T-shaped push-and-pull 5.
(2). drive wheel coaxial package is on the motor power axle being positioned at outer container outside and move axially along dynamical axis, the concrete structure of this drive wheel and dynamical axis is not limit, enumerate two examples in the present embodiment: (1) as depicted in figs. 1 and 2, dynamical axis is arranged the power post 2 of three circumferentially uniform settings, the inwall of drive wheel axis hole makes a lifting groove 16, this lifting groove to spiral laying at shaft hole inner wall, the middle part of lifting groove inner lower edge is provided with power column inlet, three power posts on dynamical axis are all inserted in the lifting groove of drive wheel axis hole, and along lifting groove guiding movement.(2) as shown in Figure 9, dynamical axis is coaxially fixedly mounted with a lifting wheel 31, the inwall of this lifting wheel installs power post, and the outer wall of drive wheel spirals and is shaped with lifting groove 32, and power post is arranged in lifting groove, and along lifting groove guiding movement.Helical blade near axis hole place at helical blade, arranges a closing lid and reclaims bolt 33, when Decompression accelerator quits work withdrawal, reclaims bolt and pulls closing lid to regain simultaneously.
3. helical blade
(1). helical blade is band arc, it typically is four to eight, the madial wall of each helical blade all makes a push/pull slot 6, this push/pull slot is T-shaped, and the quantity of push/pull slot is consistent with the power arm quantity on drive wheel, in each push/pull slot, all guiding is slidably installed the T-shaped push-and-pull head of a power arm front end.Enter for ease of T-shaped push-and-pull head, be shaped with one in the bottom of push/pull slot and reinforce opening 10.
(2). the lateral wall of each helical blade all makes a curved baffle 9, forms an arc blade groove 7 between this curved baffle and helical blade lateral wall.The upper end open of this arc blade groove extends to the upper surface of helical blade, and the side opening of this arc blade groove extends to the lateral edges of helical blade, and the opening direction of arc blade groove is identical with the hand of rotation of helical blade.
(3). helical blade is arranged on blade tight pulley by stay hook 12 is uniform, this stay hook is arranged on the bottom of helical blade, for the wide type hook of the flat wide mouth of hook, the mouth of hook is identical with the diameter of blade stay hook axle, width is identical with the width of blade anchor shaft 11, and helical blade Firm hook is hooked on the blade anchor shaft of blade tight pulley.
4. blade tight pulley:
(1). have the circular wheel of axis hole centered by blade tight pulley, the blade of blade tight pulley through axis hole coaxial package dynamical axis front end outside drive wheel is fixed on wheel shaft.The outside of blade tight pulley is inclination six shapes, and the top on inclined-plane is blade anchor shaft, and the angle on inclined-plane and the edge angle of blade push/pull slot match; The diameter of blade stay hook axle is identical with the diameter of stay hook internal diameter, and the length of axle is identical with the width of blade stay hook; The stay hook undercut for stay hook activity is had in the inner side of axle.
(2). on blade tight pulley, install a blade stay hook pressure ring 3, the outer wall top of this blade stay hook pressure ring is pressed on the outer wall of helical blade bottom stay hook.Blade stay hook pressure ring is outer six sides of inner circle and has the shape of circular cover, and there is a screw hole be connected with blade tight pulley at hexagonal each drift angle center, is connected and fixed by stud and blade tight pulley.Position suitable between screw and axis hole there is a fixing tenon, make it to insert in the fourth of the twelve Earthly Branches of relevant position on blade tight pulley, so that blade stay hook pressure ring is fixed on blade tight pulley; Blade stay hook pressure ring pushes down blade hook, makes it firmly be hooked on axle.
5. helix closing lid:
(1). coaxial installation one helix closing lid 14 on dynamical axis, this helix closing lid is shaped with the gap matched with helical blade shape and quantity, the madial wall of helix closing lid is shaped with power-assisted eaves 19, when helical blade rotates, its extrados 35 top is pressed on power-assisted eaves, and drive helix closing lid to rotate together with blade, work better to help helical blade.Its effect is, when blade start or at the end of, can because of the resistance of water, blade be contacted with closing lid or be separated.Meanwhile, Decompression accelerator operationally, can make between Decompression accelerator and bow, produces pressure release current, the pressure relief capability of Decompression accelerator is increased.
The radian that helix closing lid heads on, identical with the radian that helical blade and aircraft head on, supply the space left by helical blade, inlay close with helical blade normal incidence, time closed and aircraft surface quite.An axis hole is established at helix closing lid center, and be sleeved on helix closing lid axle, rotate freely, there are check screw restrictions on top.At the outer eaves of helix closing lid, there is the clamping ring of a ring shape, with the edge of reinforced closed lid.Closing lid is when surfacing, completely closed with hull, plays secret effect, is not easily found.
Principle of work of the present invention is:
When dynamical axis rotates forward, power post moves in the lifting groove of drive wheel inwall, makes the extrapolated interior endvertex walking to lifting groove of drive wheel, becomes the power resources of drive wheel, make power wheel and axle drive shaft synchronous rotary; Helical blade is released along push/pull slot by push-and-pull head, makes power arm crouch into push/pull slot, so that helical blade is fixed on power arm firmly, makes helical blade have firm power resources, makes helical blade rotary work; During drive wheel longitudinal travel, its outer rim top is pressed in the bottom surface of power-assisted eaves, and the extrados top of helical blade is pressed on power-assisted eaves, therefore can ensure helix closing lid and blade synchronous rotary.
When helical blade rotates, blade groove can make the water at its front and rear all penetrate rapidly along the hand of rotation of blade, forms mobile water curtain, makes the running resistance in aircraft front let out as deflection, thus make formation zone of negative pressure, blade groove rear, farthest reduce the resistance of navigation.
When axle drive shaft does contrarotation, contrarotation done by power post, the outer endvertex to lifting groove is rotated again along lifting groove, drive wheel is made to retract original position, push-and-pull head is inwardly regained along with drive wheel, push-and-pull head hauls the push/pull slot of blade, helical blade is regained, closes in closing lid and stash.
When using two structure embodiment illustrated in fig. 9, when dynamical axis rotates forward, separation type Decompression accelerator operationally, Decompression accelerator entirety is released and maintains a certain distance with naval vessel, water curtain is formed before naval ship water lower part and produces a zone of negative pressure, avoid as far as possible being attached to prematurely on hull, reach better acceleration effect.Also can according to circumstances determine the need of pull-out cavity; Submarine is then avoided pulling out cavity.

Claims (9)

1. a Decompression accelerator, it is characterized in that: comprise outer container, drive wheel, blade tight pulley and helical blade, in outer container, an electrical motor is installed, drive wheel coaxial package is on the motor power axle being positioned at outer container outside and move axially along dynamical axis, and the outer wall of drive wheel is shaped with one group of circumferentially uniform power arm; The blade of the dynamical axis front end of blade tight pulley coaxial package outside drive wheel is fixed on wheel shaft, helical blade is arranged on blade tight pulley by stay hook that its underpart is made is uniform, the madial wall of each helical blade all makes a push/pull slot, all lead in each push/pull slot the power arm that is slidably installed, the lateral wall of each helical blade all makes a curved baffle, forms the arc blade groove that the hand of rotation of an opening direction and helical blade is identical between this curved baffle with helical blade lateral wall.
2. Decompression accelerator according to claim 1, it is characterized in that: described outer container is the barrel-shaped of sealing, install a motor bench in outer container, electrical motor is arranged in this motor bench, and the dynamical axis of this electrical motor passes the top cover of outer container and extends to outside top cover.
3. Decompression accelerator according to claim 1, it is characterized in that: at the lateral wall of outer container top cover, the water sealing device that is positioned at dynamical axis periphery is installed, at the madial wall of outer container top cover, the water collection device that is positioned at dynamical axis periphery is installed, this water collection device is connected by distribution tube with the polywater case being arranged on outer container inner bottom part, is provided with leakage inductive device and drain tube holes in this polywater case.
4. the Decompression accelerator according to claim 1 or 2 or 3, it is characterized in that: the power post described dynamical axis being arranged three circumferentially uniform settings, the inwall of drive wheel axis hole makes a lifting groove, the middle part of lifting groove inner lower edge is provided with power column inlet, three power posts on dynamical axis are inserted in the lifting groove of drive wheel axis hole, and along lifting groove guiding movement.
5. the Decompression accelerator according to claim 1 or 2 or 3, it is characterized in that: described dynamical axis is coaxially fixedly mounted with a lifting wheel, the inwall of this lifting wheel installs power post, the outer wall of drive wheel spirals and is shaped with lifting groove, power post is arranged in lifting groove, and along lifting groove guiding movement.
6. Decompression accelerator according to claim 1, it is characterized in that: a T-shaped push-and-pull head is all made in the front end of described each power arm, the made push/pull slot of each helical blade madial wall is also T-shaped, and this T-shaped push-and-pull head guiding is slidably mounted in T-shaped push/pull slot.
7. Decompression accelerator according to claim 1, is characterized in that: the circular wheel having axis hole centered by blade tight pulley, and the outside of blade tight pulley is inclination six shapes, and the top on inclined-plane is blade anchor shaft; The stay hook undercut for stay hook activity is had in the inner side of axle.
8. the Decompression accelerator according to claim 1 or 7, is characterized in that: on blade tight pulley, install a blade stay hook pressure ring, the outer wall top of this blade stay hook pressure ring is pressed on the outer wall of helical blade bottom stay hook.
9. Decompression accelerator according to claim 1, it is characterized in that: coaxial installation one helix closing lid on described dynamical axis, this helix closing lid is shaped with the gap matched with helical blade shape and quantity, the madial wall of helix closing lid is shaped with power-assisted eaves, the outer eaves of closing lid is provided with a clamping ring, makes closing lid become an entirety.
CN201110339336.7A 2011-11-01 2011-11-01 Decompression accelerator Expired - Fee Related CN103085961B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201110339336.7A CN103085961B (en) 2011-11-01 2011-11-01 Decompression accelerator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201110339336.7A CN103085961B (en) 2011-11-01 2011-11-01 Decompression accelerator

Publications (2)

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CN103085961A CN103085961A (en) 2013-05-08
CN103085961B true CN103085961B (en) 2015-07-15

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Application Number Title Priority Date Filing Date
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Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3041992A (en) * 1960-05-10 1962-07-03 United Aircraft Corp Low drag submarine
CN2283612Y (en) * 1993-07-29 1998-06-10 宁建锦 Rotor energy-saving device installed on stem
US5934612A (en) * 1998-03-11 1999-08-10 Northrop Grumman Corporation Wingtip vortex device for induced drag reduction and vortex cancellation
US7096810B1 (en) * 2005-09-20 2006-08-29 Adams Robert D Bow mounted vessel propulsion system
EP1873055A1 (en) * 2006-06-30 2008-01-02 Technische Universiteit Delft Ship with bow control surface
CN202283974U (en) * 2011-11-01 2012-06-27 李僖年 Pressure release and acceleration device

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Address after: 6969 Wanning street, Chino, Los Angeles, USA

Patentee after: Li Xinian

Address before: 300110 Tianjin city Nankai District Weishui road Pingli road in Pingli 1-5-201

Patentee before: Li Xinian

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Granted publication date: 20150715

Termination date: 20201101

CF01 Termination of patent right due to non-payment of annual fee