CN109263628A - It is a kind of improve aircushion vehicle and bow bury first bow Effuser device - Google Patents

It is a kind of improve aircushion vehicle and bow bury first bow Effuser device Download PDF

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Publication number
CN109263628A
CN109263628A CN201810869552.4A CN201810869552A CN109263628A CN 109263628 A CN109263628 A CN 109263628A CN 201810869552 A CN201810869552 A CN 201810869552A CN 109263628 A CN109263628 A CN 109263628A
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China
Prior art keywords
bow
nozzle
swivelling
aircushion vehicle
head
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CN201810869552.4A
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Chinese (zh)
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CN109263628B (en
Inventor
薛彦卓
齐柏澄
刘仁伟
徐述
陈自旺
狄少丞
王庆
倪宝玉
鞠磊
曾令东
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Harbin Engineering University
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Harbin Engineering University
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Priority to CN201810869552.4A priority Critical patent/CN109263628B/en
Publication of CN109263628A publication Critical patent/CN109263628A/en
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Publication of CN109263628B publication Critical patent/CN109263628B/en
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60VAIR-CUSHION VEHICLES
    • B60V3/00Land vehicles, waterborne vessels, or aircraft, adapted or modified to travel on air cushions
    • B60V3/06Waterborne vessels

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Vehicle Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)
  • Nozzles (AREA)

Abstract

The invention belongs to ship domains, and in particular to be related to a kind of improvement aircushion vehicle and bow to bury first bow Effuser device.The device is made of swivelling-nozzle, head, fixed jet pipe and air cushion vehicle hull, wherein head adjusts its working condition according to aircushion vehicle by control device system under the conditions of the different speed of a ship or plane: when aircushion vehicle is in middle lowsteaming, head is in compressive state, and bow jet pipe sprays high pressure gas according to aircushion vehicle difference Control requirements around;When aircushion vehicle is in high speed operation, head is in bending stretch state, bow jet pipe spout is downward, high pressure gas is sprayed downwards, and bowing to bury so as to improve aircushion vehicle appears for the first time as the present invention can make air cushion stem jet pipe while retaining original function, increase the freedom degree of bow Effuser device, it rotate bow jet pipe can along two axis directions, so that aircushion vehicle be made to utilize regardless of that can realize to bow jet pipe in lower-speed state or fast state, further increase the maneuverability and safety of aircushion vehicle.

Description

It is a kind of improve aircushion vehicle and bow bury first bow Effuser device
Technical field
The invention belongs to ship domains, and in particular to be related to a kind of improvement aircushion vehicle and bow to bury first bow Effuser device.
Background technique
Air cushion vehicle pad state navigation when, hull is suspended on running surface, thus have minimum frictional force with Higher travel speed is obtained, however reduces maneuverability while improving rapidity, anti-side wind energy power is poor when high speed, low speed When the small steerage of airvane incoming flow it is poor.Currently, the aircushion vehicle of English, Mei Deng state is respectively arranged with bow Effuser device to improve the manipulation of aircushion vehicle Property, it solves the above problems, but this bow jet pipe can only be rotated in fixed pan to realize different maneuverability patterns.And work as aircushion vehicle When running at high speed, easily occurring bowing burying is appeared for the first time as causing Ship Structure damage, apron to destroy, reducing safety, general bow Jet pipe can not realize the adjustment of maneuverability for this phenomenon, improve the driving status of ship.
Summary of the invention
The purpose of the present invention buries first bow Effuser device providing a kind of improvement aircushion vehicle and bow.
It is a kind of improve aircushion vehicle and bow bury first bow Effuser device, by swivelling-nozzle 1, head 2, fixed 3 and of jet pipe Air cushion vehicle hull 5 is constituted, and swivelling-nozzle 1, head 2 and fixed jet pipe 3 constitute bow Effuser device, swivelling-nozzle 1 lower half portion is hollow circular-tube, and the top half of swivelling-nozzle 1 is bending hollow circular-tube, i.e., when 1 lower semisection of swivelling-nozzle is hollow When round tube is disposed vertically, for the upper semisection nozzle of swivelling-nozzle 1 towards horizontal plane oblique upper, fixed jet pipe 3 is to remove upper face cone Hollow tetragonous Taper Pipe after point, head 2 are cylindrical telescopic rubber, and 2 two-port of head is by swivelling-nozzle 1 and fixes Jet pipe 3 is connected, and two sets of bow Effuser devices are symmetrically mounted on 5 two sides of air cushion vehicle hull, by fixing jet pipe 3 and hovering entirely Air cushion vessel hull 5 is connected, and wherein head 2 is adjusted under the conditions of the different speed of a ship or plane by control device system according to aircushion vehicle Its working condition.
When aircushion vehicle is in middle lowsteaming, head 2 is in compressive state, i.e. 2 rubber tube of head is not stretched State that is long, compressing completely, 1 lower half hollow circular-tube of swivelling-nozzle is upright, 1 upper half hollow bent pipe nozzle direction of swivelling-nozzle The oblique upper of horizontal direction, swivelling-nozzle 1 spray high pressure gas according to aircushion vehicle difference Control requirements around.Work as aircushion vehicle In when running at high speed, head 2 is controlled by control device system, and head 2 is axial be bent with captain direction It stretches, head 2 is in bending stretch state, and 1 nozzle of swivelling-nozzle downward, sprays downwards high pressure gas, swivelling-nozzle 1 Axis and vertical line have an angle value, and the size of the angle value is carried out according to aircushion vehicle speed difference by control device system Adjustment.The two bow Effuser devices in left and right along the longitudinally asymmetric arrangement of aircushion vehicle, swivelling-nozzle 1 spout downward when, two bow jet pipes dress Angle value between the swivelling-nozzle 1 set and vertical line is equal in magnitude.
The beneficial effects of the present invention are:
The present invention can make air cushion stem jet pipe while retaining original function, increase the freedom degree of bow Effuser device, make Bow jet pipe can be rotated along two axis directions, to make aircushion vehicle regardless of can be to bow jet pipe in lower-speed state or fast state It realizes and utilizes, further increase the maneuverability and safety of aircushion vehicle.
Detailed description of the invention
Structure principle chart when Fig. 1 (a) is low speed upright state of the present invention.
Structure principle chart when Fig. 1 (b) is high speed bending state of the present invention.
Front view when Fig. 2 (a) is low speed upright state of the present invention.
Front view when Fig. 2 (b) is high speed bending state of the present invention.
Fig. 3 is integral arrangement operation schematic diagram of the invention.
Specific embodiment
The present invention will be further described with reference to the accompanying drawing.
It is a kind of improve aircushion vehicle and bow bury first bow Effuser device.It is mainly used in ship domain, being related to one kind can basis Air cushion vehicle adjusts the angle between bow Effuser device spout and horizontal plane, under the conditions of the different speed of a ship or plane to improve air cushion Ship bowing in high-speed cruising, which is buried, to be appeared for the first time as so that air cushion vehicle when running at high speed, by control device system, is adjusted Save the angle between bow jet pipe spout and horizontal plane.It includes the components such as swivelling-nozzle, head, fixed jet pipe, wherein living Dynamic device adjusts its working condition according to aircushion vehicle by control device system under the conditions of the different speed of a ship or plane: in aircushion vehicle is in When lowsteaming, head is in compressive state, and bow jet pipe sprays high pressure gas according to aircushion vehicle difference Control requirements around Body;When aircushion vehicle is in high speed operation, head is in bending stretch state, and bow jet pipe spout downward, sprays downwards high It calms the anger body, bowing to bury so as to improve aircushion vehicle appears for the first time as increasing the maneuverability and safety of aircushion vehicle.
The bow jet pipe that existing air cushion vehicle uses can only rotate in fixed horizontal plane around vertical axes, be single-degree-of-freedom Device bows the present invention provides a kind of improvement aircushion vehicle and buries first bow Effuser device.Bow jet pipe is adjusted in the bow Effuser device Angle between spout and horizontal plane makes bow jet pipe that can not only spray pressure-air along peripheral direction under middle low-speed situations, obtains Air thrust, adjust the driving direction of air cushion vehicle, moreover it is possible to adjusted by control system, make spout towards side-lower, Lift is provided for air cushion ship bow part, improves Operation Performance of Air Cushion Vehicle, increases drive safety.
The technical solution that the present invention realizes:
On the basis of common bow jet pipe, increase head between rotary body and fixed jet pipe.When aircushion vehicle is general When speed state downward driving, head is in inoperative (compression) state, and bow jet pipe can be the same as previous common bow jet pipe dress at this time It sets and equally rotates in a circumferential direction;When aircushion vehicle, which is in, runs at high speed, head is controlled by control device system, with captain side Bend tension is carried out to be axial, makes spout downward, sprays pressure-air, to provide stem upward power, to improve Aircushion vehicle bowing when running at high speed buries indictment state.
Of the invention has the prominent advantages that:
The present invention can make air cushion stem jet pipe while retaining original function, increase the freedom degree of bow Effuser device, make Bow jet pipe can be rotated along two axis directions, to make aircushion vehicle regardless of can be to bow jet pipe in lower-speed state or fast state It realizes and utilizes, further increase the maneuverability and safety of aircushion vehicle.
The present invention is that a kind of improvement aircushion vehicle bows and buries first bow Effuser device, bow Effuser device installation on the quarter two Side can adjust head by control device system, to change bow jet pipe spout and level in aircushion vehicle high speed operation Angle between face, so that the bow Effuser device increases one degree of freedom on the basis of general bow jet pipe, it is characterized in that: movable Angle of the device by control device system according to aircushion vehicle under the conditions of the different speed of a ship or plane, between control bow jet pipe spout and horizontal plane Degree improves aircushion vehicle safety to increase hovercraft handling.
1. swivelling-nozzle in figure, 2. heads, 3. fixed jet pipes, 4. a certain angle values, 5. air cushion vehicle hulls.
In Fig. 1, swivelling-nozzle 1 is linked together with fixed jet pipe 3 by head 2, when aircushion vehicle is in low speed When, bow Effuser device is in upright state, and head is in compressive state;When aircushion vehicle is in high speed, head is by controlling Apparatus system control processed is in bending stretch state, and bow jet pipe spout is downward.
In Fig. 2, when aircushion vehicle be in high speed and bow Effuser device spout downward when, the axis of swivelling-nozzle 1 and vertical The size of line value 4 at an angle, the angle value can be adjusted according to aircushion vehicle speed difference by control device system.
In Fig. 3, the two bow Effuser devices in left and right along the longitudinally asymmetric arrangement of aircushion vehicle, two bow jet pipes spout downward when, It should ensure that a certain angle value 4 between the swivelling-nozzle 1 and vertical line of two bow jet pipes is equal in magnitude, to realize stress balance.

Claims (4)

1. a kind of improvement aircushion vehicle, which is bowed, buries first bow Effuser device, it is characterised in that: the device is by swivelling-nozzle (1), activity Device (2), fixation jet pipe (3) and air cushion vehicle hull (5) are constituted, swivelling-nozzle (1), head (2) and fixation Jet pipe (3) constitutes bow Effuser device, and swivelling-nozzle (1) lower half portion is hollow circular-tube, and the top half of swivelling-nozzle (1) is curved Bent hollow circular-tube, i.e., when swivelling-nozzle (1) lower semisection hollow circular-tube is disposed vertically, the upper semisection nozzle court of swivelling-nozzle (1) To horizontal plane oblique upper, fixed jet pipe (3) are the hollow tetragonous Taper Pipe after removing cone above, and head (2) is cylinder Swivelling-nozzle (1) is connected by shape telescopic rubber, head (2) two-port with fixed jet pipe (3), two sets of bow Effuser devices pair Title is mounted on air cushion vehicle hull (5) two sides, is connected by fixed jet pipe (3) with air cushion vehicle hull (5), wherein Head (2) adjusts its working condition according to aircushion vehicle by control device system under the conditions of the different speed of a ship or plane.
2. a kind of improvement aircushion vehicle according to claim 1, which is bowed, buries first bow Effuser device, it is characterised in that: work as air cushion When ship is in middle lowsteaming, head (2) is in compressive state, i.e. head (2) rubber tube is not extended, compressed completely State, swivelling-nozzle (1) lower half hollow circular-tube is upright, and swivelling-nozzle (1) upper half hollow bent pipe nozzle is towards level side To oblique upper, swivelling-nozzle (1) according to spraying high pressure gas to aircushion vehicle difference Control requirements around.
3. a kind of improvement aircushion vehicle according to claim 1, which is bowed, buries first bow Effuser device, it is characterised in that: work as air cushion Ship is in when running at high speed, and head (2) is controlled by control device system, head (2) with captain direction be it is axial into Row bend tension, head (2) are in bending stretch state, and swivelling-nozzle (1) nozzle downward, sprays downwards high pressure gas, The axis and vertical line of swivelling-nozzle (1) have an angle value, and the size of the angle value passes through control according to aircushion vehicle speed difference Apparatus system processed is adjusted.
4. a kind of improvement aircushion vehicle according to claim 1, which is bowed, buries first bow Effuser device, it is characterised in that: left and right two A bow Effuser device along the longitudinally asymmetric arrangement of aircushion vehicle, swivelling-nozzle (1) spout downward when, the rotation spray of two bow Effuser devices The angle value managed between (1) and vertical line is equal in magnitude.
CN201810869552.4A 2018-08-02 2018-08-02 Bow jet pipe device for improving low head and countersunk head of hovercraft Active CN109263628B (en)

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CN201810869552.4A CN109263628B (en) 2018-08-02 2018-08-02 Bow jet pipe device for improving low head and countersunk head of hovercraft

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Application Number Priority Date Filing Date Title
CN201810869552.4A CN109263628B (en) 2018-08-02 2018-08-02 Bow jet pipe device for improving low head and countersunk head of hovercraft

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CN109263628B CN109263628B (en) 2020-11-20

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Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1087543A (en) * 1964-05-28 1967-10-18 Hovercraft Dev Ltd Improvements relating to gas-cushion vehicles
US5195602A (en) * 1991-07-26 1993-03-23 Weiland Carl W Stabilized air cushion vehicle
CN1268455A (en) * 2000-05-29 2000-10-04 范振汝 Hovercraft
CN1363500A (en) * 2002-02-05 2002-08-14 周勃 Jet air-cushion ship with higher speed
CN202574208U (en) * 2012-07-06 2012-12-05 上海飞浪气垫船有限公司 Longitudinal balance control balanced rudder mechanism for air cushion vehicle
CN103552680A (en) * 2013-11-12 2014-02-05 中交天津航道局有限公司 Fan-shaped bow jet positioning and control method for trailing suction hopper dredger
CN103723239A (en) * 2013-12-17 2014-04-16 哈尔滨工程大学 Partially-air-cushion-supported shallow-draft high-speed catamaran
CN105856994A (en) * 2016-05-23 2016-08-17 中国船舶重工集团公司第七○二研究所 Air-propelled ship automatic trim adjustment device
CN106005394A (en) * 2016-07-22 2016-10-12 中国航空工业集团公司西安飞机设计研究所 Rescue aircraft
KR20180042473A (en) * 2016-10-07 2018-04-26 강성광 Air-Jet Propelled Ship has Hovercraft Function And The Composition Method

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1087543A (en) * 1964-05-28 1967-10-18 Hovercraft Dev Ltd Improvements relating to gas-cushion vehicles
US5195602A (en) * 1991-07-26 1993-03-23 Weiland Carl W Stabilized air cushion vehicle
CN1268455A (en) * 2000-05-29 2000-10-04 范振汝 Hovercraft
CN1363500A (en) * 2002-02-05 2002-08-14 周勃 Jet air-cushion ship with higher speed
CN202574208U (en) * 2012-07-06 2012-12-05 上海飞浪气垫船有限公司 Longitudinal balance control balanced rudder mechanism for air cushion vehicle
CN103552680A (en) * 2013-11-12 2014-02-05 中交天津航道局有限公司 Fan-shaped bow jet positioning and control method for trailing suction hopper dredger
CN103723239A (en) * 2013-12-17 2014-04-16 哈尔滨工程大学 Partially-air-cushion-supported shallow-draft high-speed catamaran
CN105856994A (en) * 2016-05-23 2016-08-17 中国船舶重工集团公司第七○二研究所 Air-propelled ship automatic trim adjustment device
CN106005394A (en) * 2016-07-22 2016-10-12 中国航空工业集团公司西安飞机设计研究所 Rescue aircraft
KR20180042473A (en) * 2016-10-07 2018-04-26 강성광 Air-Jet Propelled Ship has Hovercraft Function And The Composition Method

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
方胜: "全垫升气垫船升沉-横倾解耦控制研究", 《中国优秀硕士学位论文全文数据库工程科技II辑》 *

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