WO2017173935A1 - 基于轴向空心舵杆和混气空腔舵叶的输气释放装置 - Google Patents

基于轴向空心舵杆和混气空腔舵叶的输气释放装置 Download PDF

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Publication number
WO2017173935A1
WO2017173935A1 PCT/CN2017/078082 CN2017078082W WO2017173935A1 WO 2017173935 A1 WO2017173935 A1 WO 2017173935A1 CN 2017078082 W CN2017078082 W CN 2017078082W WO 2017173935 A1 WO2017173935 A1 WO 2017173935A1
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Prior art keywords
rudder
axial hollow
release
rudder blade
gas
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PCT/CN2017/078082
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English (en)
French (fr)
Inventor
林焰
蒋晓宁
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Dalian University of Technology
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Dalian University of Technology
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Publication of WO2017173935A1 publication Critical patent/WO2017173935A1/zh
Priority to US16/130,993 priority Critical patent/US10562594B2/en
Anticipated expiration legal-status Critical
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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B1/00—Hydrodynamic or hydrostatic features of hulls or of hydrofoils
    • B63B1/32—Other means for varying the inherent hydrodynamic characteristics of hulls
    • B63B1/34—Other means for varying the inherent hydrodynamic characteristics of hulls by reducing surface friction
    • B63B1/38—Other means for varying the inherent hydrodynamic characteristics of hulls by reducing surface friction using air bubbles or air layers gas filled volumes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H25/00—Steering; Slowing-down otherwise than by use of propulsive elements; Dynamic anchoring, i.e. positioning vessels by means of main or auxiliary propulsive elements
    • B63H25/46—Steering or dynamic anchoring by jets or by rudders carrying jets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H25/00—Steering; Slowing-down otherwise than by use of propulsive elements; Dynamic anchoring, i.e. positioning vessels by means of main or auxiliary propulsive elements
    • B63H25/06—Steering by rudders
    • B63H25/08—Steering gear
    • B63H25/14—Steering gear power assisted; power driven, i.e. using steering engine
    • B63H25/18—Transmitting of movement of initiating means to steering engine
    • B63H25/24—Transmitting of movement of initiating means to steering engine by electrical means
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H25/00—Steering; Slowing-down otherwise than by use of propulsive elements; Dynamic anchoring, i.e. positioning vessels by means of main or auxiliary propulsive elements
    • B63H25/06—Steering by rudders
    • B63H25/08—Steering gear
    • B63H25/14—Steering gear power assisted; power driven, i.e. using steering engine
    • B63H25/26—Steering engines
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H25/00—Steering; Slowing-down otherwise than by use of propulsive elements; Dynamic anchoring, i.e. positioning vessels by means of main or auxiliary propulsive elements
    • B63H25/06—Steering by rudders
    • B63H25/38—Rudders
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H25/00—Steering; Slowing-down otherwise than by use of propulsive elements; Dynamic anchoring, i.e. positioning vessels by means of main or auxiliary propulsive elements
    • B63H25/52—Parts for steering not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B1/00—Hydrodynamic or hydrostatic features of hulls or of hydrofoils
    • B63B1/32—Other means for varying the inherent hydrodynamic characteristics of hulls
    • B63B1/34—Other means for varying the inherent hydrodynamic characteristics of hulls by reducing surface friction
    • B63B1/38—Other means for varying the inherent hydrodynamic characteristics of hulls by reducing surface friction using air bubbles or air layers gas filled volumes
    • B63B2001/385—Other means for varying the inherent hydrodynamic characteristics of hulls by reducing surface friction using air bubbles or air layers gas filled volumes using exhaust gas
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T70/00—Maritime or waterways transport
    • Y02T70/10—Measures concerning design or construction of watercraft hulls

Definitions

  • the present invention relates to a gas release device based on an axial hollow rudder stock and an aerated cavity rudder blade, and belongs to the technical field of ship manufacturing.
  • the rudder includes a rudder stock and a rudder blade; the rudder stock is a transmission device that connects the rudder blade with the steering gear drive mechanism and transmits the steering torque.
  • the structure and function of the existing rudder stock are relatively simple.
  • the present invention proposes a gas release device based on an axial hollow rudder stock and an aerated cavity rudder blade.
  • the device should use the rudder to release compressed air and chemical reagents to achieve energy saving and emission reduction, bubble drag reduction and defoaming stealth.
  • the technical solution adopted by the present invention is: a gas release device based on an axial hollow rudder stock and a mixed air rudder blade, which comprises a steering gear arranged in a hull tail structure, characterized in that:
  • the utility model comprises an axial hollow rudder stock, a mixed air rudder blade and a gas release system, wherein a lower part of the axial hollow rudder stock is fixedly connected to the slewing vane of the aeration cavity, and an upper part is sleeved on the tiller connected to the steering gear,
  • the rudder blade of the aeration cavity is suspended below the hull tail structure, and is connected by a key taper to the axial hollow rudder bar, and the bottom is arranged to release a gas delivery system comprising a release nozzle and a gas delivery control box, the gas delivery control box comprising a reagent delivery hose connected to the chemical
  • the axial hollow rudder stock is provided with a small diameter through hole at the center line of the shaft.
  • the lower half of the aerated cavity rudder blade adopts a separate aeration cavity structure.
  • the release nozzle adopts a streamlined structure, and the release nozzle is provided with three release holes facing different directions.
  • the gas release device based on the axial hollow rudder stock and the aerated cavity rudder blade comprises a steering gear, an axial hollow rudder stock, a mixed air rudder blade and a gas release system, and an axial hollow rudder stock
  • the lower part is fixedly connected to the aerated cavity rudder blade, and the aeration cavity rudder blade is suspended below the hull tail structure.
  • the gas delivery system includes a release nozzle and a gas transfer control box, a chemical reagent storage tank, a compressed air bottle and a console are placed in the hull tail structure with the steering gear, and the reagent delivery hose and the high pressure hose extend into the axial hollow rudder a through hole in the rod is connected to the aeration cavity of the turf blade of the aeration cavity, the release nozzle is arranged at the bottom of the rudder blade of the aeration cavity, and the compressed gas and the chemical reagent are passed through the high pressure hose and the reagent delivery hose.
  • the axial hollow rudder stock enters the aeration cavity of the turf blade of the aeration cavity and is released by releasing the nozzle.
  • the device uses a rudder to release compressed air and chemical reagents to achieve energy saving and emission reduction, bubble drag reduction and defoaming stealth.
  • FIG. 1 is a structural view of a gas release device based on an axial hollow rudder stock and an aeration cavity rudder blade.
  • FIG. 2 is a cross-sectional view taken along line A-A of FIG. 1.
  • FIG 3 is a longitudinal cross-sectional view of a mixed air rudder blade.
  • FIG. 4 is a cross-sectional view taken along line B-B of FIG. 1.
  • FIG. 5 is a cross-sectional view taken along line C-C of FIG. 1.
  • FIG. 6 is a schematic structural view of a release nozzle.
  • FIG. 7 is a rudder blade diagram of an axially uniform release aperture.
  • FIG. 8 is a top plan view of the axially uniform release orifice rudder blade.
  • Figures 1, 2, 3, 4, and 5 show structural views of a gas delivery device based on an axial hollow rudder stock and an aerated cavity rudder blade.
  • the gas release device based on the axial hollow rudder stock and the aerated cavity rudder blade comprises a steering gear 5 arranged in the hull tail structure 4, an axial hollow rudder stock 1, a mixed air rudder blade 2 and gas release system.
  • the axial hollow rudder stock 1 is provided with a small diameter through hole 16 at the center line of the shaft, and the lower part of the axial hollow rudder stock 1 is fixedly connected to the slewing blade 2 of the aeration cavity, and the upper part is sleeved on the tiller connected to the steering gear 5.
  • 6 is fixed in the hull tail structure 4 by the upper rudder carrier 7 and the lower rudder carrier 8, and the lower half of the aeration cavity rudder blade 2 adopts a structure of a separate aeration cavity 9.
  • the aeration cavity rudder blade 2 is suspended below the hull tail structure 4 and is connected to the axial hollow rudder stock 1 by a key taper, and a release nozzle 15 is arranged at the bottom.
  • the gas delivery system includes a release nozzle 15 and a gas delivery control box 17, and the gas delivery control box 17 includes a reagent delivery hose 14b connected to the chemical reagent storage tank 12, a high pressure hose 14a connected to the compressed air bottle 13,
  • the chemical reagent storage tank 12, the compressed air bottle 13 and the console 10, the chemical reagent storage tank 12, the compressed air bottle 13 and the console 10 are placed in the hull tail structure 4 provided with the steering gear 5, the reagent delivery hose 14b and the high pressure
  • the hose 14a extends into the through hole 16 in the axial hollow rudder stock 1, and is then connected to the aeration cavity 9 of the aerated cavity rudder blade 2, which is arranged in the aerated cavity rudder blade 2 At the bottom, the horizontal position of
  • the compressed gas and chemical reagent pass through the high pressure hose 14a and the reagent delivery hose 14b, from the axial hollow rudder stock 1 into the aeration cavity 9 of the aeration cavity rudder blade 2, and are released by the release nozzle 15.
  • FIG. 6 shows the structural form of the release nozzle 15.
  • the release nozzle 15 has a streamlined structure with three release holes facing in different directions.
  • FIGS. 7 and 8 show rudder blade views of axially uniform release apertures. There are 6 release pressures on both sides of the aerated cavity rudder blade 2 The uniform release orifices 19 of the gas and chemical reagents.
  • the working principle of the gas release device based on the axial hollow rudder stock and the aerated cavity rudder blade is as follows: by the chemical reagent storage tank 12 and the compressed air bottle 13 disposed in the hull tail structure 4, by connecting in the chemistry The reagent delivery hose 14b on the reagent storage tank 12 and the high-pressure hose 14a connected to the compressed air bottle 13 enter the aeration cavity of the lower portion of the culvert blade 2 of the aeration cavity from the through hole 16 of the axial hollow rudder stock 1.
  • Two rows of vertically arranged uniform release holes 19 are added on both sides of the rudder blade to increase the release area of compressed gas and chemical reagents, and to expand the effect of bubble drag reduction and defoaming stealth.
  • the gas release device based on the axial hollow rudder stock and the aerated cavity rudder blade comprises a steering gear, an axial hollow rudder stock, a mixed air rudder blade and a gas release system, and an axial hollow rudder stock
  • the lower part is fixedly connected to the aerated cavity rudder blade, and the aeration cavity rudder blade is suspended below the hull tail structure.
  • the gas delivery system includes a release nozzle and a gas transfer control box, a chemical reagent storage tank, a compressed air bottle and a console are placed in the hull tail structure with the steering gear, and the reagent delivery hose and the high pressure hose extend into the axial hollow rudder a through hole in the rod is connected to the aeration cavity of the slewing vane of the aeration cavity, the release nozzle is arranged at the bottom of the rudder blade of the aeration cavity, and the compressed gas and the chemical reagent are passed through the high pressure hose and the reagent delivery hose.
  • the axial hollow rudder stock enters the aeration cavity of the turf blade of the aeration cavity and is released by releasing the nozzle.
  • the device uses a rudder to release compressed air and chemical reagents to achieve energy saving and emission reduction, bubble drag reduction and defoaming stealth.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Toys (AREA)
  • Catching Or Destruction (AREA)

Abstract

一种基于轴向空心舵杆和混气空腔舵叶的输气释放装置，包括轴向空心舵杆（1）、混气空腔舵叶（2）和输气释放系统。轴向空心舵杆（1）的下部固定连接混气空腔舵叶（2）。化学试剂存储罐（12）、压缩空气瓶（13）和控制台（10）安放在船体尾结构（4）内。试剂输送软管（14b）和高压软管（14a）伸入轴向空心舵杆（1）内的通孔（16），连接到混气空腔舵叶（2）的混气空腔（9）内。释放喷嘴（15）布置在混气空腔舵叶（2）的底部。该装置实现了船舶的节能减排、气泡减阻和消泡隐身。

Description

说明书 发明名称：基于轴向空心舵杆和混气空腔舵叶的输气释放装置 技术领域
[0001] 本发明涉及一种基于轴向空心舵杆和混气空腔舵叶的输气释放装置， 属于船舶 制造技术领域。
背景技术
[0002] 随着船舶工业的发展和社会的进步， 船舶交通运输对我国国民经济的发展起到 了一定的促进作用。 二十一世纪的造船业， 由于海上运输革新的需求， 各种特 殊用途船舶随之产生， 相应的配套船舶设备也得到了幵发。
技术问题
[0003] 目前的大多数船舶采用船舵来改变航向， 一般来说， 船舵包括舵杆和舵叶； 舵 杆是将舵叶与舵机驱动机构连接起来， 并传递转舵扭矩的传动装置， 而现有舵 杆的结构和功能都比较单一。
问题的解决方案
技术解决方案
[0004] 为了克服现有技术中存在的问题， 本发明提出一种基于轴向空心舵杆和混气 空腔舵叶的输气释放装置。 该装置应采用舵释放压缩空气和化学试剂， 实现船 舶的节能减排、 气泡减阻和消泡隐身。
[0005] 本发明采用的技术方案是： 一种基于轴向空心舵杆和混气空腔舵叶的输气释放 装置， 它包括布置在船体尾结构中的舵机， 其特征在于： 它还包括轴向空心舵 杆、 混气空腔舵叶和输气释放系统， 所述轴向空心舵杆的下部固定连接混气空 腔舵叶， 上部套在与舵机相连接的舵柄上， 并通过上舵承和下舵承固定在船体 尾结构内， 所述混气空腔舵叶悬挂在船体尾结构下方， 并采用有键锥形连接于 轴向空心舵杆上， 底部布置有释放喷嘴； 所述输气释放系统包含释放喷嘴和输 气控制箱， 输气控制箱包含连接在化学试剂存储罐上的试剂输送软管、 连接在 压缩空气瓶上的高压软管、 化学试剂存储罐、 压缩空气瓶和控制台， 化学试剂 存储罐、 压缩空气瓶和控制台安放在设有舵机的船体尾结构内， 所述试剂输送 软管和高压软管伸入轴向空心舵杆内的通孔， 然后连接到混气空腔舵叶的混气 空腔内， 所述释放喷嘴布置在混气空腔舵叶的底部， 释放喷嘴的水平位置低于 螺旋桨； 压缩气体和化学试剂通过高压软管和试剂输送软管， 从轴向空心舵杆 进入混气空腔舵叶的混气空腔内， 并通过释放喷嘴进行释放。
[0006] 所述轴向空心舵杆在轴中线处设有一个小口径的通孔。
[0007] 所述混气空腔舵叶的下半部分采用一个独立的混气空腔结构。
[0008] 所述释放喷嘴采用流线型的结构， 释放喷嘴设有三个朝着不同方向的释放孔
[0009] 所述混气空腔舵叶的两侧设有 5-10个释放压缩气体和化学试剂的均布释放孔。
发明的有益效果
有益效果
[0010] 这种基于轴向空心舵杆和混气空腔舵叶的输气释放装置包括舵机、 轴向空心舵 杆、 混气空腔舵叶和输气释放系统， 轴向空心舵杆的下部固定连接混气空腔舵 叶， 混气空腔舵叶悬挂在船体尾结构下方。 输气释放系统包含释放喷嘴和输气 控制箱， 化学试剂存储罐、 压缩空气瓶和控制台安放在设有舵机的船体尾结构 内， 试剂输送软管和高压软管伸入轴向空心舵杆内的通孔， 连接到混气空腔舵 叶的混气空腔内， 释放喷嘴布置在混气空腔舵叶的底部， 压缩气体和化学试剂 通过高压软管和试剂输送软管， 从轴向空心舵杆进入混气空腔舵叶的混气空腔 内， 并通过释放喷嘴进行释放。 该装置采用舵释放压缩空气和化学试剂， 实现 船舶的节能减排、 气泡减阻和消泡隐身。
对附图的简要说明
附图说明
[0011] 图 1是基于轴向空心舵杆和混气空腔舵叶的输气释放装置的结构图。
[0012] 图 2是图 1中的 A-A剖视图。
[0013] 图 3是混气空腔舵叶的纵剖视图。
[0014] 图 4是图 1中的 B-B剖视图。
[0015] 图 5是图 1中的 C-C剖视图。
[0016] 图 6是释放喷嘴的结构示意图。
[0017] 图 7是轴向均布释放孔的舵叶图。 [0018] 图 8是轴向均布释放孔舵叶的俯视图。
[0019] 图中： 1、 轴向空心舵杆， 2、 混气空腔舵叶， 3、 螺旋桨， 4、 船体尾结构， 5 、 舵机， 6、 舵柄， 7、 上舵承， 8、 下舵承， 9、 混气空腔， 10、 控制台， 11、 控制阀门， 12、 化学试剂存储罐， 13、 压缩空气瓶， 14a、 高压软管， 14b、 试剂 输送软管， 15、 释放喷嘴， 16、 通孔， 17、 输气控制箱， 18轴向均布气体释放 舵叶， 19、 均布释放孔。
实施该发明的最佳实施例
本发明的最佳实施方式
[0020] 以下参照附图对本发明的结构做进一步描述。
[0021] 图 1、 2、 3、 4、 5示出了基于轴向空心舵杆和混气空腔舵叶的输气释放装置的 结构图。 图中， 这种基于轴向空心舵杆和混气空腔舵叶的输气释放装置， 包括 布置在船体尾结构 4中的舵机 5、 轴向空心舵杆 1、 混气空腔舵叶 2和输气释放系 统。 轴向空心舵杆 1在轴中线处设有一个小口径的通孔 16， 轴向空心舵杆 1的下 部固定连接混气空腔舵叶 2， 上部套在与舵机 5相连接的舵柄 6上， 并通过上舵承 7和下舵承 8固定在船体尾结构 4内， 混气空腔舵叶 2的下半部分采用一个独立的 混气空腔 9结构。 混气空腔舵叶 2悬挂在船体尾结构 4下方， 并采用有键锥形连接 于轴向空心舵杆 1上， 底部布置有释放喷嘴 15。 输气释放系统包含释放喷嘴 15和 输气控制箱 17， 输气控制箱 17包含连接在化学试剂存储罐 12上的试剂输送软管 1 4b、 连接在压缩空气瓶 13上的高压软管 14a、 化学试剂存储罐 12、 压缩空气瓶 13 和控制台 10， 化学试剂存储罐 12、 压缩空气瓶 13和控制台 10安放在设有舵机 5的 船体尾结构 4内， 试剂输送软管 14b和高压软管 14a伸入轴向空心舵杆 1内的通孔 16 ， 然后连接到混气空腔舵叶 2的混气空腔 9内， 所述释放喷嘴 15布置在混气空腔 舵叶 2的底部， 释放喷嘴 15的水平位置低于螺旋桨 3。 压缩气体和化学试剂通过 高压软管 14a和试剂输送软管 14b， 从轴向空心舵杆 1进入混气空腔舵叶 2的混气空 腔 9内， 并通过释放喷嘴 15进行释放。
[0022] 图 6示出了释放喷嘴 15的结构形式。 释放喷嘴 15采用流线型的结构， 设有 3个朝 着不同方向的释放孔。
[0023] 图 7、 8示出了轴向均布释放孔的舵叶图。 混气空腔舵叶 2的两侧设有 6个释放压 缩气体和化学试剂的均布释放孔 19。
[0024] 基于轴向空心舵杆和混气空腔舵叶的输气释放装置的工作原理如下： 由安置在 船体尾结构 4内的化学试剂存储罐 12和压缩空气瓶 13， 通过连接在化学试剂存储 罐 12上的试剂输送软管 14b和连接在压缩空气瓶 13上的高压软管 14a， 由轴向空心 舵杆 1的通孔 16进入混气空腔舵叶 2下部的混气空腔 9内， 然后由释放喷嘴 15上的 三个不同朝向的幵孔进行释放， 实现个别船舶节能减排、 气泡减阻和消泡隐身 的要求， 同吋整个输送释放过程可由输气控制装置进行操控。 在舵叶的两侧增 加两排竖直布置的均布释放孔 19， 可增大压缩气体和化学试剂的释放区域， 扩 大气泡减阻和消泡隐身的功效。
本发明的实施方式
[0025] 本发明的实施方式同最佳实施方式。
工业实用性
[0026] 这种基于轴向空心舵杆和混气空腔舵叶的输气释放装置包括舵机、 轴向空心舵 杆、 混气空腔舵叶和输气释放系统， 轴向空心舵杆的下部固定连接混气空腔舵 叶， 混气空腔舵叶悬挂在船体尾结构下方。 输气释放系统包含释放喷嘴和输气 控制箱， 化学试剂存储罐、 压缩空气瓶和控制台安放在设有舵机的船体尾结构 内， 试剂输送软管和高压软管伸入轴向空心舵杆内的通孔， 连接到混气空腔舵 叶的混气空腔内， 释放喷嘴布置在混气空腔舵叶的底部， 压缩气体和化学试剂 通过高压软管和试剂输送软管， 从轴向空心舵杆进入混气空腔舵叶的混气空腔 内， 并通过释放喷嘴进行释放。 该装置采用舵释放压缩空气和化学试剂， 实现 船舶的节能减排、 气泡减阻和消泡隐身。
序列表自由内容
[0027] 无。

Claims

权利要求书
[权利要求 1] 一种基于轴向空心舵杆和混气空腔舵叶的输气释放装置， 它包括布置 在船体尾结构 （4) 中的舵机 （5) ， 其特征在于： 它还包括轴向空心 舵杆 （1) 、 混气空腔舵叶 （2) 和输气释放系统， 所述轴向空心舵杆
( 1) 的下部固定连接混气空腔舵叶 （2) ， 上部套在与舵机 （5) 相 连接的舵柄 （6) 上， 并通过上舵承 （7) 和下舵承 （8) 固定在船体 尾结构 （4) 内， 所述混气空腔舵叶 （2) 悬挂在船体尾结构 （4) 下 方， 并采用有键锥形连接于轴向空心舵杆 （1) 上， 底部布置有释放 喷嘴 （15) ； 所述输气释放系统包含释放喷嘴 （15) 和输气控制箱 ( 17) ， 输气控制箱 （17) 包含连接在化学试剂存储罐 （12) 上的试剂 输送软管 （14b) 、 连接在压缩空气瓶 （13) 上的高压软管 （14a) 、 化学试剂存储罐 （12) 、 压缩空气瓶 （13) 和控制台 (10)， 化学试剂 存储罐 （12) 、 压缩空气瓶 （13) 和控制台 (10)安放在设有舵机 （5
) 的船体尾结构 （4) 内， 所述试剂输送软管 （14b) 和高压软管 （14 a) 伸入轴向空心舵杆 （1) 内的通孔 （16) ， 然后连接到混气空腔舵 叶 （2) 的混气空腔 (9)内， 所述释放喷嘴 （15) 布置在混气空腔舵叶
(2) 的底部， 释放喷嘴 （15) 的水平位置低于螺旋桨 （3) ； 压缩气 体和化学试剂通过高压软管 （14a) 和试剂输送软管 （14b) ， 从轴向 空心舵杆 （1) 进入混气空腔舵叶 （2) 的混气空腔 （9) 内， 并通过 释放喷嘴 (15)进行释放。
[权利要求 2] 根据权利要求 1所述的基于轴向空心舵杆和混气空腔舵叶的输气释放 装置， 其特征在于： 所述轴向空心舵杆 （1) 在轴中线处设有一个小 口径的通孔 ( 16) 。
[权利要求 3] 根据权利要求 1所述的基于轴向空心舵杆和混气空腔舵叶的输气释放 装置， 其特征在于： 所述混气空腔舵叶 （2) 的下半部分采用一个独 立的混气空腔 (9)结构。
[权利要求 4] 根据权利要求 1所述的基于轴向空心舵杆和混气空腔舵叶的输气释放 装置， 其特征在于： 所述释放喷嘴 （15) 采用流线型的结构， 释放喷 嘴 （15) 设有三个朝着不同方向的释放孔
[权利要求 5] 根据权利要求 1所述的基于轴向空心舵杆和混气空腔舵叶的输气释放 装置， 其特征在于： 所述混气空腔舵叶 （2) 的两侧设有 5- 10个释放 压缩气体和化学试剂的均布释放孔 （19) 。
PCT/CN2017/078082 2016-04-06 2017-03-24 基于轴向空心舵杆和混气空腔舵叶的输气释放装置 Ceased WO2017173935A1 (zh)

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