CN106167081B - Combined type aircraft carrier - Google Patents
Combined type aircraft carrier Download PDFInfo
- Publication number
- CN106167081B CN106167081B CN201610530021.3A CN201610530021A CN106167081B CN 106167081 B CN106167081 B CN 106167081B CN 201610530021 A CN201610530021 A CN 201610530021A CN 106167081 B CN106167081 B CN 106167081B
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- subhull
- unit
- subhull unit
- male connector
- water
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
- B63G11/00—Aircraft carriers
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- 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
- B63B1/02—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement
- B63B1/10—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement with multiple hulls
- B63B1/12—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement with multiple hulls the hulls being interconnected rigidly
- B63B1/121—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving lift mainly from water displacement with multiple hulls the hulls being interconnected rigidly comprising two hulls
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B21/00—Tying-up; Shifting, towing, or pushing equipment; Anchoring
- B63B21/56—Towing or pushing equipment
- B63B21/62—Towing or pushing equipment characterised by moving of more than one vessel
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B43/00—Improving safety of vessels, e.g. damage control, not otherwise provided for
- B63B43/02—Improving safety of vessels, e.g. damage control, not otherwise provided for reducing risk of capsizing or sinking
- B63B43/04—Improving safety of vessels, e.g. damage control, not otherwise provided for reducing risk of capsizing or sinking by improving stability
- B63B43/06—Improving safety of vessels, e.g. damage control, not otherwise provided for reducing risk of capsizing or sinking by improving stability using ballast tanks
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B43/00—Improving safety of vessels, e.g. damage control, not otherwise provided for
- B63B43/18—Improving safety of vessels, e.g. damage control, not otherwise provided for preventing collision or grounding; reducing collision damage
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- Engineering & Computer Science (AREA)
- Ocean & Marine Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Health & Medical Sciences (AREA)
- Public Health (AREA)
- Fluid Mechanics (AREA)
- Measuring Fluid Pressure (AREA)
- Pressure Vessels And Lids Thereof (AREA)
- Force Measurement Appropriate To Specific Purposes (AREA)
- Manipulator (AREA)
- Connector Housings Or Holding Contact Members (AREA)
Abstract
The invention discloses a kind of combined type aircraft carrier, including the first subhull unit and the second subhull unit, the side of the first subhull unit is equipped with the first female connector；The respective side of the second subhull unit is equipped with and matched first male connector of first female connector；First female connector has the first inner chamber for being suitable for receiving first male connector, the inner wall of the first inner chamber is equipped with first pressure sensing device, the first pressure sensing device and first male connector of insertion coordinate, for detecting the first pressure value on the vertical direction that first male connector applies the first inner chamber, subhull unit is additionally provided with the plumbing equipment with pressure sensor device compounding practice simultaneously, two subhull units can be preferably kept in a relatively fixed position by the present invention, it avoids two subhull units and causes connecting component to be broken because horizontal position is different.
Description
Technical field
The present invention relates to a kind of Ship Structures, and in particular to a kind of combined type aircraft carrier.
Background technology
Aircraft carrier is a kind of with the large-scale water surface naval vessels that carrier-borne aircraft is main operational weapon, is aircraft carrier group
Core, other ships in fleet provide its protection and supply, and aircraft carrier then provides air umbrella and long-range strike ability.Hair
So far, aircraft carrier has been one of the indispensable weapon of Modern Navy and the most important naval vessels of sea warfare for exhibition.Current aviation
Mother ship carrier is all integrally-built huge monster, because target is big, to realize that hidden action, surprise attack are nearly impossible,
Equally also because target is big, it is easy to it is under attack, in addition, can also encounter various technologic difficulties in building course.
A kind of building block type aircraft carrier is disclosed in the Chinese patent literature of Publication No. CN101259876.The building blocks
Formula aircraft carrier is made of a control vessel and more unit warship interconnections.Connection between control vessel and more unit warships and
It is separately to be realized by being installed on the Zhan Tianyou of warship body sidewall.The places of helping Zhan Tian are corresponded on warship body sidewall processes circular cone shape
Boss or pit, be fixed with buffer rubber gasket in boss or pit surface, when the side wall of two warship bodies is connected, a side
Boss on wall is just inserted into the pit on another side wall, and is mutually coincide, the Zhan Tianyou being mounted in boss and pit
Just it is a set of, is connected with the actuator for being fixed in warship body on side wall wherein a Zhan Tian is helped.Pass through this connection type
The lengthening that aircraft carrier longitudinal direction runway may be implemented, to be conducive to the takeoff and landing of carrier-borne aircraft.
The aircraft carrier of above-mentioned building block system, only the boss on two unit warships and pit component are respectively away from the water surface
It is highly identical, and when water surface calmness, be likely to realize the docking by predetermined way of unit.However, the aircraft carrier one after docking
Tote weight declines on a denier wherein unit warship, which can then float, if another unit warship does not mitigate equally
More totes then will appear floating warship and be coordinated by upward boss and pit, levers up non-rising warship upwards, so very
It is likely to result in phenomenon of rupture occur at boss and pit cooperation；Similarly, if the weight of wherein one warship tote increases, and
The weight of another warship tote is constant or declines, and also will appear this phenomenon.In order to avoid there is phenomenon of rupture, connect without passing through
Fitting carries out being relatively fixed connection, once wherein a unit warship floats, another maintains draft constant, then can not be fine
Ground realizes that two unit warships are in relatively fixed position, and then can not realize that the takeoff and landing for carrier-borne aircraft is continuous well
Longitudinal lengthen runway.
Invention content
For this purpose, can preferably realize that two unit warships keep phase technical problem to be solved by the present invention lies in one kind is provided
To fixed position, and the combined type aircraft carrier that two unit warship connecting components can be avoided to be broken well.
Another technical problem to be solved by this invention is to provide a kind of combined type quickly connected convenient for unit warship
Aircraft carrier.
In order to solve the above technical problems, the present invention provides a kind of combined type aircraft carrier, including the first subhull unit and second
Subhull unit,
The side of the first subhull unit is equipped with the first female connector；
The respective side of the second subhull unit is equipped with public even with first female connector matched first
Fitting；
First female connector has the first inner chamber for being suitable for receiving first male connector, the first inner chamber
Inner wall is equipped with first pressure sensing device, and first male connector of the first pressure sensing device and insertion coordinates,
For detecting the first pressure value on the vertical direction that first male connector applies the first inner chamber；
The first subhull unit includes：
First Lower Hold, first Lower Hold have the first water inlet connect with water phase；
First plumbing equipment, first plumbing equipment include the first plumbing being set to inside first Lower Hold
Device, and the first control of water supply and drainage being connect respectively with first water feeding and draining device and the first pressure sensing device fill
It sets, the first control of water supply and drainage device is according to the pressure signal for the first pressure value received, control described the
One water feeding and draining device introduces the water into and is discharged first Lower Hold by first water inlet, to adjust the described first sub- ship
The draft of body unit, and then two subhull units are maintained at preset relative position.
Said combination formula aircraft carrier, wherein the side of the second subhull unit is equipped with the second female connector；Described
The respective side of one subhull unit is equipped with and matched second male connector of second female connector；Described second is female
There is connector the second inner chamber for being suitable for receiving second male connector, the inner wall of the second inner chamber to be equipped with second pressure
Second male connector of sensing device, the second pressure sensing device and insertion coordinates, public for detecting described second
Second pressure value on the vertical direction that connector applies the second inner chamber；The second subhull unit includes：Second
Lower Hold, second Lower Hold have the second water inlet connect with water phase；Second plumbing equipment, the second plumbing equipment packet
Include the second water feeding and draining device inside second Lower Hold, and respectively with second water feeding and draining device and described second
Second control of water supply and drainage device of pressure sensor device connection, the second control of water supply and drainage device are directed to institute according to what is received
State the pressure signal of second pressure value, control the second control of water supply and drainage device introduced the water by second water inlet and
The second Lower Hold is discharged, to adjust the draft of the second subhull unit, and then by two subhull lists
Member is maintained at preset relative position.
Said combination formula aircraft carrier, wherein the first pressure sensing device includes the upper inner wall set on the first inner chamber
With on lower inner wall for detect the first upward pressure value first on pressure sensor device and for detection first be pressed downward force value
First time pressure sensor device；The first control of water supply and drainage device is believed according to the pressure of pressure sensor device on described first
First Lower Hold of the first subhull unit number is discharged to control first water feeding and draining device by water, and according to described
The pressure signal of first time pressure sensor device introduces the water into the first subhull list to control first water feeding and draining device
First Lower Hold of member, until on described first detected by pressure sensor device or first time pressure sensor device
Pressure value reaches preset range.
Said combination formula aircraft carrier, wherein the second pressure sensing device includes the upper inner wall set on the second inner chamber
With on lower inner wall for detect the second upward pressure value second on pressure sensor device and for detection second be pressed downward force value
Second time pressure sensor device；The second control of water supply and drainage device is believed according to the pressure of pressure sensor device on described second
Second Lower Hold of the second subhull unit number is discharged to control second water feeding and draining device by water, and according to described
The pressure signal of second time pressure sensor device introduces the water into the second subhull list to control second water feeding and draining device
Second Lower Hold of member, until on described second detected by pressure sensor device or second time pressure sensor device
Pressure value reaches preset range.
Said combination formula aircraft carrier, wherein pressure sensor device includes on described first：Buffer unit on first, one end branch
It supports on the inner wall of the first inner chamber；Snubber contact component on first is connected with the other end of buffer unit on described first
It connects, coordinates with buffer unit on described first, realize the inner wall to the first inner chamber to snubber contact component on described first
The buffering of movement；Pressure signal generation device on first is connect with snubber contact component on described first, will be delayed on described first
It rushes the stroke that contact component is moved to the inner wall of the first inner chamber and is converted into pressure signal, and this is exported in a manner of electric signal
Pressure signal；First time pressure sensor device include：First time buffer unit, one end are supported in the interior of the first inner chamber
On wall；First time snubber contact component is connected with the other end of first time buffer unit, with first time buffer part
Part coordinates, and realizes the buffering moved to the inner wall of the first inner chamber to first time snubber contact component；First time pressure
Signal generation device is connect with first time snubber contact component, by first time snubber contact component to described first
The stroke of the inner wall movement of inner cavity is converted into pressure signal, and the pressure signal is exported in a manner of electric signal.
Said combination formula aircraft carrier, wherein pressure sensor device includes on described second：Buffer unit on second, one end branch
It supports on the inner wall of the second inner chamber；Snubber contact component on second is connected with the other end of buffer unit on described second
It connects, coordinates with buffer unit on described second, realize the inner wall to the second inner chamber to snubber contact component on described second
The buffering of movement；Pressure signal generation device on second is connect with snubber contact component on described second, will be delayed on described second
It rushes the stroke that contact component is moved to the inner wall of the second inner chamber and is converted into pressure signal, and this is exported in a manner of electric signal
Pressure signal；Second time pressure sensor device include：Second time buffer unit, one end are supported in the interior of the second inner chamber
On wall；Second time snubber contact component is connected with the other end of second time buffer unit, with second time buffer part
Part coordinates, and realizes the buffering moved to the inner wall of the second inner chamber to second time snubber contact component；Second time pressure
Signal generation device is connect with second time snubber contact component, by second time snubber contact component to described second
The stroke of the inner wall movement of inner cavity is converted into pressure signal, and the pressure signal is exported in a manner of electric signal.
Said combination formula aircraft carrier, wherein it is installed with the first pulling equipment on the first subhull unit, described
Equipped with recyclable and release the first drag rope, the second subhull unit is equipped with to be suitable for and described the one pulling equipment
One drag rope carries out the first rope fixture of detachable connection.
Said combination formula aircraft carrier, wherein be formed with first through hole on first male connector, on the female connector at
Shape has the second through-hole, is respectively adapted to pass through for first drag rope；Described in being mounted on when first drag rope one end
On pulling equipment, the other end is each passed through the first through hole and second through-hole is connect with first rope fixture
When, first pulling equipment recycles the drag rope by the first through hole, to pull another ship
Body unit is moved along the drag rope direction of recession, and then first male connector is made to be connect with first female connector
It closes, realizes the docking of two hull units.
Said combination formula aircraft carrier, wherein first male connector has tapered protrusion structure or spherical surface hill structure；Institute
State the first female connector with conical indentation structure corresponding with the tapered protrusion structure or with the spherical surface hill structure phase
Corresponding spherical depression structure；And the first through hole is located at the central part of the tapered protrusion structure or spherical surface hill structure
Position, second through-hole are located at the centre of the conical indentation structure or the spherical depression structure.
The above technical solution of the present invention has the following advantages over the prior art：
1. the combined type aircraft carrier of the present invention, including the first subhull unit and the second subhull unit, the first sub- ship
The side of body unit is equipped with the first female connector；The respective side of the second subhull unit is equipped with and first mother
Matched first male connector of connector；It, can by using the connection type of the male connector and female connector that match each other
Easily two sub- hull units to be fixed together, and it is simple in structure, it is solid and reliable；Meanwhile first mother is even
There is fitting the first inner chamber for being suitable for receiving first male connector, the inner wall of the first inner chamber to be passed equipped with first pressure
First male connector of induction device, the first pressure sensing device and insertion coordinates, for detecting first public affairs even
First pressure value on the vertical direction that fitting applies the first inner chamber；The first subhull unit includes：First bottom
Storehouse, first Lower Hold have the first water inlet connect with water phase；First plumbing equipment, first plumbing equipment include
The first water feeding and draining device inside first Lower Hold, and pressed respectively with first water feeding and draining device and described first
The control of water supply and drainage device of Force sensor connection, the control of water supply and drainage device are directed to the first pressure according to what is received
The pressure signal of value controls first water feeding and draining device and introduces the water into and be discharged first bottom by first water inlet
Two subhull units to adjust the draft of the first subhull unit, and then are maintained at preset by storehouse
Relative position；The subhull unit of the combined type aircraft carrier of the present invention uses the design of pressure sensor device so that be connected two ships
When the difference of body horizontal position, pressure sensor sends pressure signal to the control of water supply and drainage device, control of water supply and drainage device root
Draining or the water-supplying operation of the water feeding and draining device are adjusted according to the pressure signal, similarly, such regulative mode is also applied for described
Second subhull unit or other subhull units being connected, so as to adjust wherein relevant one or more hulls
Draft cause sub- ship when avoiding the hull carrier-borne aircraft quantity in group hull unit there are larger gap
Body unit draft is inconsistent, causes male connecting elements and female connecting elements to be not on a horizontal plane, and then be easy to lead
The phenomenon that causing connector fracture, ensure that the fastness of subhull unit connection, and simple in structure, easy to adjust.
2. the combined type aircraft carrier of the present invention, the first pressure sensing device includes the upper inner wall set on the first inner chamber
With on lower inner wall for detect the first upward pressure value first on pressure sensor device and for detection first be pressed downward force value
First time pressure sensor device；The first control of water supply and drainage device is believed according to the pressure of pressure sensor device on described first
First Lower Hold of the first subhull unit number is discharged to control first water feeding and draining device by water, and according to described
The pressure signal of first time pressure sensor device introduces the water into the first subhull list to control first water feeding and draining device
First Lower Hold of member, until on described first detected by pressure sensor device or first time pressure sensor device
Pressure value reaches preset range；Equally, the second pressure sensing device include set on the second inner chamber upper inner wall and
It is used to detect pressure sensor device on the second of the second upward pressure value on lower inner wall and is pressed downward force value for detecting second
Second time pressure sensor device；The second control of water supply and drainage device is according to the pressure signal of pressure sensor device on described second
Second Lower Hold of the second subhull unit is discharged to control second water feeding and draining device by water, and according to described
The pressure signal of two times pressure sensor devices introduces the water into the second subhull unit to control second water feeding and draining device
Second Lower Hold, until the pressure on described second detected by pressure sensor device or second time pressure sensor device
Force value reaches preset range；By the setting of upper pressure sensor and lower pressure sensor enable pressure sensor more
Sensitively the variation of hull draft is detected consequently facilitating the draining water supply of hull is adjusted.
3. pressure sensor device includes on described first：Buffer unit on first, one end are supported in the first inner chamber
On inner wall；Snubber contact component on first is connected with the other end of buffer unit on described first, is buffered on described first
Component coordinates, and realizes the buffering moved to the inner wall of the first inner chamber to snubber contact component on described first；It is pressed on first
Force signal generation device is connect with snubber contact component on described first, by snubber contact component on described first to described
The stroke of the inner wall movement of one inner cavity is converted into pressure signal, and the pressure signal is exported in a manner of electric signal；Described first
Lower pressure sensor device includes：First time buffer unit, one end are supported on the inner wall of the first inner chamber；First time buffering connects
Contact portion part is connected with the other end of first time buffer unit, coordinates with first time buffer unit, realizes to described
The buffering that first time snubber contact component is moved to the inner wall of the first inner chamber；First time pressure signal generation device, with institute
State first time snubber contact component connection, the row that first time snubber contact component is moved to the inner wall of the first inner chamber
Journey is converted into pressure signal, and the pressure signal is exported in a manner of electric signal；Similarly, on described second pressure sensor device and
Second time pressure sensor device is also the setting side using buffer unit, snubber contact component and pressure signal generation device
The stroke that snubber contact component moves is converted into pressure signal, and is exported the pressure signal in a manner of electric signal by formula；This hair
The setting of buffer unit and snubber contact component in bright to occur to deposit when relative motion between male connector and female connector
Buffering, will not jolt because of hull or other reasons lead to that violent collision occurs between connector, avoid connector by
Impact force and fracture, the reliability for the connection being further ensured that.
4. the combined type aircraft carrier of the present invention is installed with the first pulling equipment on the first subhull unit, described
First pulling equipment equipped with it is recyclable and release the first drag rope, the second subhull unit be equipped be suitable for it is described
First drag rope carries out the first rope fixture of detachable connection, and it is logical that first is formed on first male connector
Hole is formed with the second through-hole on first female connector, is respectively adapted to pass through for first drag rope；When described first
Drag rope one end is mounted on first pulling equipment, and the other end is each passed through the first through hole and second through-hole
When being connect with first rope fixture, first pulling equipment by the first through hole to the drag rope into
Row recycling, to pull another second hull unit to be moved along the drag rope direction of recession, and then makes described first
Male connector is engaged with first female connector, realizes the docking of two hull units；For designing above, even at hull
In the environment of more jolting, two hulls is made to be moved along the direction that drag rope recycles, that is, male connecting elements and female connection structure
Part is mutually drawn close along drag rope, also conveniently can smoothly complete engagement.
5. the combined type aircraft carrier of the present invention, first male connector has tapered protrusion structure or spherical surface hill structure；
First female connector have conical indentation structure corresponding with the tapered protrusion structure or with the spherical surface hill structure
Corresponding spherical depression structure；And the first through hole is located at the central part of the tapered protrusion structure or spherical surface hill structure
Position, second through-hole are located at the centre of the conical indentation structure or the spherical depression structure；Above taper is convex
Rise structure or spherical surface hill structure without alignment conical indentation structure corresponding with the tapered protrusion completely or with the spherical surface
The corresponding spherical depression structure of bulge-structure, it is only necessary to which the head of bulge-structure enters in sunk structure, you can passes through
The matched conical surface or spherical surface, which take advantage of a situation to slide into, forms engagement in sunk structure；Even if in being in larger in hull and jolting,
It can also realize docking.
Description of the drawings
In order to make the content of the present invention more clearly understood, it below according to specific embodiments of the present invention and combines
Attached drawing, the present invention is described in further detail, wherein
Fig. 1 is the subhull cellular construction schematic diagram of the present invention；
Fig. 2 is the subhull unit connection diagram of the present invention；
Fig. 3 is subhull unit connection signal Fig. 1 of embodiment；
Fig. 4 is subhull unit connection signal Fig. 2 of embodiment；
Fig. 5 is subhull unit connection signal Fig. 3 of embodiment；
Fig. 6 is male connector and female connector structural representation Fig. 1；
Fig. 7 is male connector and female connector structural representation Fig. 2；
Reference numeral is expressed as in figure：A- the first subhull units, the first pulling equipments of 1A-, the first drag ropes of 11A-,
The second male connectors of 21A-, the first female connectors of 22A-, 23A- first inner chambers, 24A- first pressure sensing devices, 24A1- first
Upper pressure sensor device, first time pressure sensor device of 24A2-, the second through-holes of 25A-, 3- pulleys, the first Lower Holds of 4A-, 5A-
One water inlet, the first plumbing equipments of 6A-, B- the second subhull units, the first rope fixtures of 1B-, 21B- first are public even
Fitting, the second female connectors of 22B-, 25B- first through hole, the second Lower Holds of 4B-, the second water inlets of 5B-, the second plumbing of 6B- are set
It is standby, 211- tapered protrusion structures, 212- spherical surface hill structures, 221- conical indentation structures, 222- spherical depression structures.
Specific implementation mode
A kind of combined type aircraft carrier of the present invention is specifically described with reference to specific embodiment：
As shown in Figures 1 and 2, a kind of combined type aircraft carrier, including the first subhull unit A and the second subhull unit B, institute
The side for stating the first subhull unit A is equipped with the first female connector 22A；In the respective side of the second subhull unit B
It is suitable for equipped with having with the matched first male connector 21B of the first female connector 22A, the first female connector 22A
The inner wall for receiving the first inner chamber 23A, the first inner chamber 23A of the first male connector 21B is sensed equipped with first pressure
Device 24A, the first pressure sensing device 24A and the first male connector 21B of insertion coordinate, for detecting described the
The first pressure value on vertical direction that one male connector 21B applies the first inner chamber 24A；The first subhull unit
A includes：First Lower Hold 4A, the first Lower Hold 4A has the first water inlet 5A connect with water phase；First plumbing equipment 6A, institute
It includes the first water feeding and draining device being set to inside the first Lower Hold 4A to state the first plumbing equipment 6A, and respectively with described the
The first control of water supply and drainage device that one water feeding and draining device is connected with the first pressure sensing device 24A, first plumbing
Control device controls first water feeding and draining device and passes through institute according to the pressure signal for the first pressure value received
It states the first water inlet 5A and introduces the water into and be discharged the first Lower Hold 4A, to adjust the drinking water of the first subhull unit A
Depth, and then two sub- hull units are maintained at preset relative position.
The side of the second subhull unit B is equipped with the second female connector 22B；The first subhull unit A's
Respective side is equipped with and the matched second male connector 21A of the second female connector 22B；Equally, second mother connects
There is fitting 22B the second inner chamber for being suitable for receiving the second male connector 21A, the inner wall of the second inner chamber to be equipped with second
The second male connector 21A of pressure sensor device, the second pressure sensing device and insertion coordinates, described for detecting
The second pressure value on vertical direction that second male connector 21A applies the second inner chamber；The second subhull unit B
Including：Second Lower Hold 4B, the second Lower Hold 4B has the second water inlet 5B connect with water phase；Second plumbing equipment 6B, institute
It includes the second water feeding and draining device being set to inside the second Lower Hold 4B to state the second plumbing equipment 6B, and respectively with described the
The second control of water supply and drainage device that two water feeding and draining devices are connected with the second pressure sensing device, second control of water supply and drainage
Device controls the second control of water supply and drainage device and passes through institute according to the pressure signal for the second pressure value received
It states the second water inlet 5B and introduces the water into and be discharged the second Lower Hold 4B, to adjust the drinking water of the second subhull unit B
Depth, and then two subhull unit Bs are maintained at preset relative position.
When hull carrier-borne aircraft quantity in group hull unit is there are larger gap, hull unit can be caused to absorb water
Depth is inconsistent, causes male connecting elements and female connecting elements to be not on a horizontal plane, for a long time in this way, being easy to cause connection
The fracture of part, influence subhull unit connection fastness, and the present invention hull, made by the setting of pressure sensor device
When connected two sub- hull unit horizontal position differences, pressure sensor sends pressure signal to control of water supply and drainage device, gives
Drain control unit adjusts draining or the water-supplying operation of water feeding and draining device according to the pressure signal, by adjusting one of them or two
The draft of a hull makes two connecting elements be on a horizontal surface, and avoids connector because of horizontal position difference
And the phenomenon that leading to damage；Simultaneously, it should be noted that the combined type aircraft carrier of the present embodiment is made of several subhull units,
Foregoing first subhull unit and described two sub- hull units of the second subhull unit are not limited to, it is adjacent
It is linked together by several male connectors to match each other and female connector between subhull unit, it can be simultaneously between subhull
Row's connection, front and back can also connect, simple and strong in structure and easy to connect.
Also, as shown in figure 5, female connector, the public connection of other side setting can be separately provided in side in subhull unit
Part, such as the sides the first subhull unit A are provided with the first female connector 22A, and with the second subhull list
The first male connector 21B matchings of first B sides adjacents are connected, to which subhull unit side by side be combined, structure
Simply；However, in order to enable along different directions navigation the more convenient docking of subhull unit, as shown in Figure 3-4, Ke Yitong
When the subhull unit side setting male connector female connector is set again, so that hull difference towards when still
Can rapid abutting joint, without the operations such as turn around.
In the present embodiment, the first pressure sensing device 24A include be respectively arranged on the first inner chamber 23A it is upper in
It is used to detect pressure sensor device 24A1 on the first of the first upward pressure value on wall and lower inner wall and is used to detect first downwards
First time pressure sensor device 24A2 of pressure value；The first control of water supply and drainage device is filled according to pressure sensing on described first
It sets the pressure signal of 24A1 and water is discharged to described the first of the first subhull unit A to control first water feeding and draining device
Lower Hold 4A, and first water feeding and draining device is controlled by water according to the pressure signal of first time pressure sensor device 24A2
The first Lower Hold 4A of the first subhull unit A is introduced, until pressure sensor device 24A1 or described on described first
Pressure value detected by first time pressure sensor device 24A2 reaches preset range；The second pressure sensing device includes
It is used to detect pressure sensor device on the second of the second upward pressure value on the upper inner wall and lower inner wall of the second inner chamber
With for detecting second second time pressure sensor device for being pressed downward force value；The second control of water supply and drainage device is according to described
To control second water feeding and draining device the second subhull unit B is discharged in water by the pressure signal of pressure sensor device on two
The second Lower Hold 4B, and control according to the pressure signal of second time pressure sensor device the second plumbing dress
The the second Lower Hold 4B for introducing the water into the second subhull unit B is set, until pressure sensor device or institute on described second
It states the pressure value detected by second time pressure sensor device and reaches preset range.
Meanwhile pressure sensor device 24A1 includes on described first：Buffer unit on first, one end are supported in described first
On the inner wall of inner cavity；Snubber contact component on first is connected with the other end of buffer unit on described first, with described first
The buffering moved to the inner wall of the first inner chamber to snubber contact component on described first is realized in the cooperation of upper buffer unit；The
Pressure signal generation device on one is connect with snubber contact component on described first, by snubber contact component on described first to
The stroke of the inner wall movement of the first inner chamber is converted into pressure signal, and the pressure signal is exported in a manner of electric signal；Institute
Stating first time pressure sensor device 24A2 includes：First time buffer unit, one end are supported on the inner wall of the first inner chamber；The
Snubber contact component once is connected with the other end of first time buffer unit, coordinates with first time buffer unit,
Realize the buffering moved to the inner wall of the first inner chamber to first time snubber contact component；First time pressure signal generates
Device is connect with first time snubber contact component, by first time snubber contact component into the first inner chamber
The stroke of wall movement is converted into pressure signal, and the pressure signal is exported in a manner of electric signal.
Equally, pressure sensor device includes on described second：Buffer unit on second, one end are supported in the second inner chamber
Inner wall on；Snubber contact component on second is connected with the other end of buffer unit on described second, delays on described second
Component cooperation is rushed, realizes the buffering moved to the inner wall of the second inner chamber to snubber contact component on described second；On second
Pressure signal generation device is connect with snubber contact component on described second, by snubber contact component on described second to described
The stroke of the inner wall movement of second inner chamber is converted into pressure signal, and the pressure signal is exported in a manner of electric signal；Described
Two times pressure sensor device includes：Second time buffer unit, one end are supported on the inner wall of the second inner chamber；Second time buffering
Contact component is connected with the other end of second time buffer unit, coordinates with second time buffer unit, realizes to institute
State the buffering that second time snubber contact component is moved to the inner wall of the second inner chamber；Second time pressure signal generation device, with
Second time snubber contact component connection, second time snubber contact component is moved to the inner wall of the second inner chamber
Stroke is converted into pressure signal, and the pressure signal is exported in a manner of electric signal.
Make that opposite fortune occurs between male connector and female connector using the setting of buffer unit and snubber contact component
There is buffering when dynamic, will not jolt because of hull or other reasons lead to that violent collision occurs between connector, avoid connecting
Part is fractureed by impact force, the reliability for the connection being further ensured that.
The first pulling equipment 1A is installed on the first subhull unit A, the first pulling equipment 1A is furnished with
Recyclable and release the first drag rope 11A, the second subhull unit B, which is equipped with, to be suitable for and first drag rope
11A carries out the first rope fixture 1B of detachable connection；Specifically, being formed on the first male connector 21B
It is formed with the second through-hole 25A on one through-hole 25B, the first female connector 22A, is respectively adapted to supply first drag rope
11A is passed through；When described one end first drag rope 11A is mounted on the pulling equipment 1A, the other end is each passed through described the
The two through-hole 25A and first through hole 25B and when being connect with the first rope fixture 1B, the first pulling equipment 1A
The drag rope 11A is recycled by the first through hole 23B, to pull the second hull unit B along described
Drag rope 11A direction of recession moves, and then the first male connector 21B is made to be engaged with the first female connector 22A, real
The docking of existing two hull units.
In the present embodiment, the first male connector 21B has tapered protrusion structure 211 or spherical surface hill structure 212；
The first female connector 22A have conical indentation structure 221 corresponding with the tapered protrusion structure 211 or with the spherical surface
212 corresponding spherical depression structure 222 of bulge-structure；And the first through hole 23B be located at the tapered protrusion structure 211 or
The centre of spherical surface hill structure 212, the second through-hole 23A is located at the conical indentation structure 221 or the spherical surface is recessed
It is convex with the taper without alignment completely to fall into the centre of structure 222, above tapered protrusion structure or spherical surface hill structure
Play corresponding conical indentation structure or spherical depression structure corresponding with the spherical surface hill structure, it is only necessary to bulge-structure
Head enters in sunk structure, you can taking advantage of a situation to slide into be formed in sunk structure by the matched conical surface or spherical surface engages；
Even if in being in larger in hull and jolting, docking can also be realized, however male connector and female connector of the invention
Structure be not limited thereto, connection can be needed as needed to adjust connector shape and size, as long as so that public connection
Part and female connector just meet the requirement of the present invention convenient for engagement and sound construction.
Obviously, the above embodiments are merely examples for clarifying the description, and does not limit the embodiments.It is right
For those of ordinary skill in the art, can also make on the basis of the above description it is other it is various forms of variation or
It changes.There is no necessity and possibility to exhaust all the enbodiments.And it is extended from this it is obvious variation or
It changes still within the protection scope of the invention.
Claims (1)
1. a kind of combined type aircraft carrier, including the first subhull unit (A) and the second subhull unit (B), it is characterised in that：
The side of the first subhull unit (A) is equipped with the first female connector (22A)；
The respective side of the second subhull unit (B) is equipped with and first female connector (22A) matched first
Male connector (21B)；
First female connector (22A) has the first inner chamber (23A) for being suitable for receiving first male connector (21B), institute
State first inner chamber (23A) inner wall be equipped with first pressure sensing device (24A), the first pressure sensing device (24A) with
First male connector (21B) cooperation being inserted into, for detecting first male connector (21B) to the first inner chamber
The first pressure value on vertical direction that (23A) applies；
The first subhull unit (A) includes：
First Lower Hold (4A), first Lower Hold (4A) have the first water inlet (5A) connect with water phase；
First plumbing equipment (6A), first plumbing equipment (6A) include be set to first Lower Hold (4A) it is internal the
One water feeding and draining device, and connect respectively with first water feeding and draining device and the first pressure sensing device (24A)
One control of water supply and drainage device, the first control of water supply and drainage device are believed according to the pressure for the first pressure value received
Number, it controls first water feeding and draining device and introduces the water into and be discharged first Lower Hold by first water inlet (5A)
(4A), to adjust the draft of the first subhull unit (A), and then by the first subhull unit (A) and institute
It states the second subhull unit (B) and is maintained at preset relative position；
The first pulling equipment (1A) is installed on the first subhull unit (A), first pulling equipment (1A) is matched
There is recyclable and release the first drag rope (11A), the second subhull unit (B), which is equipped with, to be suitable for leading with described first
Messenger rope (11A) carries out the first rope fixture (1B) of detachable connection；
It is formed with first through hole (25B) on first male connector (21B), is formed on first female connector (22A)
Second through-hole (25A) is respectively adapted to pass through for first drag rope (11A)；When described first drag rope (11A) one end
On first pulling equipment (1A), the other end is each passed through second through-hole (25A) and the first through hole
When (25B) is connect with first rope fixture (1B), first pulling equipment (1A) passes through the first through hole
(25B) recycles first drag rope (11A), to pull the second subhull unit (B) along described first
Drag rope direction of recession moves, and then first male connector (21B) is made to be engaged with first female connector (22A),
Realize the docking of two hull units.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610530021.3A CN106167081B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410179838.1A CN103921919B (en) | 2014-04-30 | 2014-04-30 | A kind of combination type aircraft carrier |
| CN201610530021.3A CN106167081B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410179838.1A Division CN103921919B (en) | 2014-04-30 | 2014-04-30 | A kind of combination type aircraft carrier |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106167081A CN106167081A (en) | 2016-11-30 |
| CN106167081B true CN106167081B (en) | 2018-07-27 |
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ID=51140373
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| CN201610327543.3A Active CN105966580B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610555645.0A Active CN106043638B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610529900.4A Pending CN106184668A (en) | 2014-04-30 | 2014-04-30 | Combination type aircraft carrier |
| CN201610327541.4A Active CN105947158B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610416257.4A Active CN106081027B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610559516.9A Active CN106081028B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610530021.3A Active CN106167081B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201410179838.1A Expired - Fee Related CN103921919B (en) | 2014-04-30 | 2014-04-30 | A kind of combination type aircraft carrier |
| CN201610327443.0A Expired - Fee Related CN106043637B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610529899.5A Active CN106184667B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610555988.7A Active CN106114786B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610559519.2A Active CN106184670B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610555987.2A Active CN106043639B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610327370.5A Active CN105882927B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610529898.0A Active CN106184666B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610555989.1A Active CN106114787B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610555986.8A Active CN106184669B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610416259.3A Expired - Fee Related CN106005329B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201610327444.5A Active CN105947157B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610327543.3A Active CN105966580B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610555645.0A Active CN106043638B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610529900.4A Pending CN106184668A (en) | 2014-04-30 | 2014-04-30 | Combination type aircraft carrier |
| CN201610327541.4A Active CN105947158B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610416257.4A Active CN106081027B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610559516.9A Active CN106081028B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201410179838.1A Expired - Fee Related CN103921919B (en) | 2014-04-30 | 2014-04-30 | A kind of combination type aircraft carrier |
| CN201610327443.0A Expired - Fee Related CN106043637B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610529899.5A Active CN106184667B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610555988.7A Active CN106114786B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610559519.2A Active CN106184670B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610555987.2A Active CN106043639B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610327370.5A Active CN105882927B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610529898.0A Active CN106184666B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610555989.1A Active CN106114787B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610555986.8A Active CN106184669B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
| CN201610416259.3A Expired - Fee Related CN106005329B (en) | 2014-04-30 | 2014-04-30 | Combined type aircraft carrier |
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Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105947157B (en) * | 2014-04-30 | 2018-07-03 | 王海龙 | Combined type aircraft carrier |
| CN106741708B (en) * | 2017-01-04 | 2018-07-13 | 大连理工大学 | A kind of honeycomb air bag device for preventing the inclination of nuclear power platform damage from sinking |
| CN110552339A (en) * | 2019-08-15 | 2019-12-10 | 王静波 | Island-type offshore combined airport and construction method thereof |
| CN111017167B (en) * | 2020-01-02 | 2020-10-02 | 山东交通学院 | Intelligent underwater search and rescue robot |
| CN114212198B (en) * | 2021-12-15 | 2022-10-11 | 上海大学 | Impact-resistant automatic docking mechanism and method for unmanned water platform |
| CN114932979A (en) * | 2022-06-14 | 2022-08-23 | 刘红才 | Energy-saving emission-reducing segmented pushing combined cargo ship |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1291572A (en) * | 1999-10-12 | 2001-04-18 | 张承普 | Combined aircraft carrier |
| CN102139752A (en) * | 2010-02-03 | 2011-08-03 | 陈世文 | Novel aircraft carrier |
| CN103043196A (en) * | 2012-12-27 | 2013-04-17 | 王海龙 | Ship of quickly assembled separation-type aircraft carrier |
Family Cites Families (32)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2387367A1 (en) * | 1977-04-12 | 1978-11-10 | Lerolland Marcel | Locking mechanism for misaligned doors - has aligning arrangement for loosely fitted socket for ensuring lock connection |
| JPH08230795A (en) * | 1995-02-27 | 1996-09-10 | Toshio Matsubara | Runway with reduced ground run |
| CN1049633C (en) * | 1996-03-30 | 2000-02-23 | 朱绍祥 | Variable-load water float system engineering |
| US6196151B1 (en) * | 1997-02-24 | 2001-03-06 | Bechtel Group, Inc. | Device and method for an independent module offshore mobile base |
| US5988932A (en) * | 1997-07-31 | 1999-11-23 | Mcdermott Technology, Inc. | Marine connector |
| RU2176968C1 (en) * | 2000-09-05 | 2001-12-20 | Местон Вячеслав Александрович | Spacecraft carrier-trimaran |
| RU2201378C2 (en) * | 2000-10-10 | 2003-03-27 | Халидов Гамид Юсупович | Heavy aircraft carrier "tsunami" |
| US6550408B1 (en) * | 2001-12-19 | 2003-04-22 | Hermann J. Janssen | Method and apparatus for loading and unloading cargo from a twin-hull sea-going ship |
| CN1291572C (en) * | 2003-04-30 | 2006-12-20 | 北京盈美高科数字媒体网络科技有限公司 | Media content distributing method and system thereof |
| CN2642669Y (en) * | 2003-09-18 | 2004-09-22 | 袁晓纪 | Waterborne float airdrome capable of diving |
| JP2008519221A (en) * | 2004-11-08 | 2008-06-05 | シエル・インターナシヨネイル・リサーチ・マーチヤツピイ・ベー・ウイ | Liquefied natural gas floating storage regasifier |
| CN201058956Y (en) * | 2006-07-22 | 2008-05-14 | 张永福 | Track connection without vibration and noise |
| CN101259876A (en) * | 2007-03-07 | 2008-09-10 | 左学禹 | Building block type aircraft carrier |
| CN201058656Y (en) * | 2007-04-04 | 2008-05-14 | 刘伟通 | Energy-saving train ship |
| US20080306642A1 (en) * | 2007-06-08 | 2008-12-11 | Aqualogic Marine, Inc. | Remote controlled position sensing and auto-leveling boat lift controller |
| KR20100008652A (en) * | 2008-07-16 | 2010-01-26 | 인천대학교 산학협력단 | A manless vessel system using catamaram |
| KR101066670B1 (en) * | 2009-12-24 | 2011-09-21 | 최용호 | An air cushion ship with a flowing ballast structure for freely controlling a draft line |
| JP4868338B1 (en) * | 2010-08-26 | 2012-02-01 | ワタナベ株式会社 | Airfield ship |
| CN102079381A (en) * | 2010-10-08 | 2011-06-01 | 朱惠芬 | End-to-end double-aircraft carrier battle group |
| CN102152842A (en) * | 2011-02-10 | 2011-08-17 | 刘佳 | Design scheme of connecting and assembling dual-use ultra large ships in series into marine maneuvering airport |
| CN102794637B (en) * | 2011-05-27 | 2015-04-15 | 旭东机械(昆山)有限公司 | Rim steel wire positioning machine |
| US9061742B2 (en) * | 2011-08-05 | 2015-06-23 | Great Lakes Dredge and Dock Company, LLC | Articulated tug barge, trailing suction hopper dredge system |
| CN102936888B (en) * | 2012-11-09 | 2015-01-28 | 中国水电顾问集团华东勘测设计研究院 | Self-installation type offshore booster station structure and installation method thereof |
| CN103354433B (en) * | 2013-02-22 | 2016-02-03 | 北京纳米能源与***研究所 | A kind of spring nano generator and self-driven dynamometer |
| CN103452748B (en) * | 2013-09-23 | 2015-09-30 | 东北农业大学 | Suspension type vertical axis wind turbine |
| CN103542962A (en) * | 2013-10-31 | 2014-01-29 | 张丹丹 | Pressure testing device |
| CN103557983A (en) * | 2013-11-15 | 2014-02-05 | 安阳市荣诚石油矿山机械有限公司 | Piston type pressure sensor |
| CN203902826U (en) * | 2014-04-30 | 2014-10-29 | 王海龙 | A combined type aircraft carrier |
| CN203902824U (en) * | 2014-04-30 | 2014-10-29 | 王海龙 | A combined type aircraft carrier |
| CN203902825U (en) * | 2014-04-30 | 2014-10-29 | 王海龙 | A combined type aircraft carrier |
| CN105947157B (en) * | 2014-04-30 | 2018-07-03 | 王海龙 | Combined type aircraft carrier |
| CN203902827U (en) * | 2014-04-30 | 2014-10-29 | 王海龙 | A combined type aircraft carrier |
-
2014
- 2014-04-30 CN CN201610327444.5A patent/CN105947157B/en active Active
- 2014-04-30 CN CN201610327543.3A patent/CN105966580B/en active Active
- 2014-04-30 CN CN201610555645.0A patent/CN106043638B/en active Active
- 2014-04-30 CN CN201610529900.4A patent/CN106184668A/en active Pending
- 2014-04-30 CN CN201610327541.4A patent/CN105947158B/en active Active
- 2014-04-30 CN CN201610416257.4A patent/CN106081027B/en active Active
- 2014-04-30 CN CN201610559516.9A patent/CN106081028B/en active Active
- 2014-04-30 CN CN201610530021.3A patent/CN106167081B/en active Active
- 2014-04-30 CN CN201410179838.1A patent/CN103921919B/en not_active Expired - Fee Related
- 2014-04-30 CN CN201610327443.0A patent/CN106043637B/en not_active Expired - Fee Related
- 2014-04-30 CN CN201610529899.5A patent/CN106184667B/en active Active
- 2014-04-30 CN CN201610555988.7A patent/CN106114786B/en active Active
- 2014-04-30 CN CN201610559519.2A patent/CN106184670B/en active Active
- 2014-04-30 CN CN201610555987.2A patent/CN106043639B/en active Active
- 2014-04-30 CN CN201610327370.5A patent/CN105882927B/en active Active
- 2014-04-30 CN CN201610529898.0A patent/CN106184666B/en active Active
- 2014-04-30 CN CN201610555989.1A patent/CN106114787B/en active Active
- 2014-04-30 CN CN201610555986.8A patent/CN106184669B/en active Active
- 2014-04-30 CN CN201610416259.3A patent/CN106005329B/en not_active Expired - Fee Related
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1291572A (en) * | 1999-10-12 | 2001-04-18 | 张承普 | Combined aircraft carrier |
| CN102139752A (en) * | 2010-02-03 | 2011-08-03 | 陈世文 | Novel aircraft carrier |
| CN103043196A (en) * | 2012-12-27 | 2013-04-17 | 王海龙 | Ship of quickly assembled separation-type aircraft carrier |
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Effective date of registration: 20181113 Address after: 313023 No. 26 innovation road, Dai Xi District, Wuxing Economic Development Zone, Huzhou, Zhejiang Patentee after: HUZHOU YUFAN COSMETIC TECHNOLOGY CO.,LTD. Address before: 325600 No. 260 Longxiang Second Road, Qiancheng Village, North Baixiang Town, Yueqing City, Wenzhou City, Zhejiang Province Patentee before: Wang Hailong |
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Effective date of registration: 20221221 Address after: 276800 R&D Building No. 8, Electronic Information Industrial Park, Gaoxin 7th Road, Rizhao Hi tech Zone, Shandong Province 237, Xueyuan Road, Rizhao Hi tech Zone, Shandong Province Patentee after: Rizhao Xinrui Investment Promotion Development Co.,Ltd. Address before: 313023 No. 26 innovation road, Dai Xi District, Wuxing Economic Development Zone, Huzhou, Zhejiang Patentee before: HUZHOU YUFAN COSMETIC TECHNOLOGY CO.,LTD. |
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