CN108177793A - Aircraft carrier elevator - Google Patents
Aircraft carrier elevator Download PDFInfo
- Publication number
- CN108177793A CN108177793A CN201711398723.1A CN201711398723A CN108177793A CN 108177793 A CN108177793 A CN 108177793A CN 201711398723 A CN201711398723 A CN 201711398723A CN 108177793 A CN108177793 A CN 108177793A
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- turntable
- side turntable
- axis
- rotary body
- aircraft carrier
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- 238000005183 dynamical system Methods 0.000 claims abstract description 34
- 238000000034 method Methods 0.000 claims abstract description 8
- 230000007704 transition Effects 0.000 claims description 28
- 239000011148 porous material Substances 0.000 claims description 8
- 230000002093 peripheral effect Effects 0.000 claims description 6
- 238000000926 separation method Methods 0.000 claims description 3
- 238000013459 approach Methods 0.000 claims 1
- 230000005484 gravity Effects 0.000 abstract description 4
- 230000001737 promoting effect Effects 0.000 description 3
- 230000007547 defect Effects 0.000 description 2
- 230000007423 decrease Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/22—Ground or aircraft-carrier-deck installations for handling aircraft
- B64F1/24—Adaptations of turntables
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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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/22—Ground or aircraft-carrier-deck installations for handling aircraft
- B64F1/222—Ground or aircraft-carrier-deck installations for handling aircraft for storing aircraft, e.g. in hangars
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Specific Conveyance Elements (AREA)
Abstract
The present invention relates to a kind of aircraft carrier elevator, upper deck containing aircraft carrier (16), hangar lower decks (17), shaft (2), rotary body, axle bed component, dynamical system.The machine plate (3) that holds on rotary body is rotated with rotary body, and with the aircraft lifting and landing being stopped at thereon；Rotary body holds machine plate (3) and remains horizontality, boarding a plane will not overturn in rotation process；Aircraft can be entered smoothly on rotary body from aircraft carrier or be entered on aircraft carrier from rotary body；The effect that gravity torque is cancelled out each other is utilized, saves significantly on the energy；It promotes aircraft or aircraft enters hangar, quickly, efficiency is very high for speed；The invention quickly launches an attack for aircraft carrier and creates condition, can greatly promote the fighting capacity of aircraft carrier.
Description
Technical field
The present invention relates to a kind of aircraft carrier elevators, and especially lifting aircraft carrier is quick, saves the aircraft carrier of the energy flies
Machine elevator.The invention further relates to the application methods of the aircraft carrier elevator.
Background technology
The elevator that current aircraft carrier lifting generally uses, although can aircraft carrier be promoted to upper deck from hangar,
Also aircraft carrier can be down to hangar from upper deck, but its there are major defects.
First, energy consumption is big.Even if elevator zero load rises, also to overcome gravity, also consume compared with multiple-energy-source.
Second, speed is slow.When promoting aircraft, elevator carries aircraft and rises to upper deck, then waits for aircraft from lifting
In machine out, elevator drops to hangar again, then waits for aircraft into elevator.In a cycle for promoting aircraft, it experienced
Rise, wait for, decline, wait for Four processes, elapsed time is long, thus speed is slow.Aircraft cannot quickly launch an attack, and constrain boat
The performance of female fighting capacity.
Speed is major defect slowly.Aircraft carrier is used military forces and is valued for rapidly for fighting.It is envisioned that it is promoted tens of
Airplane will be how long.The time of present air battle is very short, and aircraft below rises to upper deck not yet, and air battle just terminates,
How this battle beats！In order to change this situation, need to try every possible means.
How aircraft carrier is quickly set out, can started with from many aspects, be one by elevator progress technological innovation.
Invention content
Lift that aircraft carrier is quick, saves the aircraft carrier liter of the energy the technical problem to be solved in the present invention is to provide a kind of
Drop machine.Another technical problems to be solved is the method using the aircraft carrier elevator.
In order to solve the above technical problems, the technical scheme is that：
A kind of aircraft carrier elevator, containing flying in the upper deck of aircraft carrier landing, aircraft carrier hangar on aircraft carrier for aircraft carrier
Lower decks that machine is parked, shaft, rotary body, axle bed component, dynamical system.
There is window on rectangle on the upper deck.
There is window under rectangle on the lower decks, which is located at the underface of the upper window on the upper deck, the lower window
The longitudinal length of mouth is more than the longitudinal length of window on this, and the transverse width of the lower window is more than the transverse width of window on this.
The rotary body contains turntable, holds machine plate.
In two turntables of the rotary body, a turntable is located at left side, is called left side turntable, another turntable is located at the right side
Side, is called right side turntable, which overlaps with the axis horizontal of the right side turntable；The left side turntable or the right side turntable,
Its center there are one round center hole, be uniformly distributed in disk close on the same circumference at edge four it is lateral opening, axis with
The axis of the centre bore overlaps, and axis is parallel with this four one of lateral opening axis, and vertex is close to the following table of the upper deck
Face, the arcuate section of its underpart are put in the lower window of the lower decks and the cavity of the lower beneath window；On the left side turntable
Four lateral opening four lateral opening mirror symmetries on the right side turntable；The interior lateral face of the left side turntable on this window it is vertical
Left window wall flushes；The interior lateral face of the right side turntable is flushed with the vertical right window wall of window on this, the vertical right window of the lower window
Wall and the outer lateral face of the right side turntable of corresponding position are opposed and close.
There are four rounded transitional holes, this four transitional pores on the left side turntable to be located at centre bore on the left side turntable respectively
With four one of lateral opening middles；The axis of the left side turntable is parallel with the axis of one of this four transitional pores respectively.
Four left side axis, four square wheels, four side gears, four transition gears, four transition are installed on the left side turntable
Axis.
Four left side axis on the left side turntable, during be respectively fixedly connected on the left of this on turntable four one of lateral opening；
One of this four left side axis, inner end are stretched out from the interior lateral face of the left side turntable, outer end from the left side turntable it is outer laterally
Face is stretched out.
The roomy outer lateral face of four cuboid square wheels on the left side turntable, it is snugly coaxially connected respectively
On the inner end of one of four left side axis on the left of this on turntable；One of this four square wheels, outer lateral face turn with the left side
The interior lateral face of disk is opposed and close, is located at extreme higher position, and upper horizontal surface is stretched to except the left side disk edge, and
In the upper window of the upper deck, the transverse width of upper horizontal surface is more than the vertical height of end face.
Four side gears on the left side turntable are snugly sleeved on four left side axis on the left side turntable respectively
One of outer end on；One of this four side gears in the axis rotary course of the left side axis where it, edge without departing from
The edge of the left side turntable.
Four transition axises on the left side turntable, four transition being snugly connected to respectively on the left side turntable
In one of hole；One of this four transition axises, inner end are flushed with the interior lateral face of the left side turntable of corresponding position, outer end
It is stretched out from the outer lateral face of the left side turntable.
Four transition gears on the left side turntable are fixedly set on the left side turntable one of four transition axises respectively
On outer end；This four transition gears engage respectively with one of four side gears on the left side turntable.
Four the right axis, four square wheels are installed on the right side turntable.
Four on right side turntable the right axis, during be respectively fixedly connected on the right side of this on turntable four one of lateral opening；
One of axis on the right of in the of this four, inner end are stretched out from the interior lateral face of the right side turntable, and outer end face is outer with the right side turntable
Lateral face flushes.
The roomy outer lateral face of four cuboid square wheels on the right side turntable, it is snugly coaxially connected respectively
On the right side of this on inner end of one of four the right axis of turntable；One of this four square wheels, outer lateral face and the right side turntable
Interior lateral face it is opposed and close, be located at extreme higher position, upper horizontal surface is stretched to except the right side disk edge and position
In the upper window of the upper deck, the transverse width of upper horizontal surface is more than the vertical height of end face.
Have on the right side turntable for aircraft carrier by four entrances, this four entrances are located at the right side turn respectively
Centre bore and four one of lateral opening centres on disk；One of this four entrances, are hexagon, and the hexagon is close to the center
The part in hole is in antiparallelogram, and the part far from the centre bore is rectangular, angle of one of the trapezoidal two sides with bottom thereon
Equal to or more than 135 °；One of this four entrances, when being located at the underface of centre bore on the right side turntable, height is more than
The height of aircraft carrier, the transverse width of its underpart rectangle are more than the width of aircraft carrier, bottom surface and the upper table of the lower decks
Face flushes.
Four pieces of levels on the rotary body are installed and hold machine plate；This four pieces are held one of machine plate, and longitudinal length is more than aircraft carrier
Length, transverse width be more than aircraft carrier width；This four pieces are held machine plate, and the lower surface near left end is respectively with close-fitting
Conjunction mode is connected on the left side turntable in the upper horizontal surface right over one of four square wheels axis, the following table near right end
Face is snugly connected to respectively in the upper horizontal surface on the right side turntable right over one of corresponding four square wheels axis,
One of four square wheels on the left side turntable or the right side turntable, the transverse width of upper horizontal surface are more than the vertical height of its end face
Degree；This four pieces are held one of machine plate, in extreme lower position, are located in the lower window of the lower decks, upper surface and corresponding positions
The bottom surface of the entrance on the right side turntable put flushes；This four pieces are held one of machine plate, and when being located at extreme higher position, being located at should
In the upper window of upper deck, the upper surface flush of upper surface and the upper deck, window on this of left side and corresponding position
Left window wall it is opposed and close.
Axle bed component axle bed containing left side, right side axle bed, the quiet gear.
The left side axle bed of the axle bed component, is quadrangular, is erected in the outside of the left side turntable and close to the left side
Nearby there are circular shaft bore in turntable, the upper end；The axle bed hole, internal diameter be equal to or more than the left side turntable on centre bore it is interior
Diameter, axis are overlapped with the axis of the centre bore；The lower face of the left side axle bed and the upper surface of the lower decks of corresponding position
Snugly connect.
The right side axle bed of the axle bed component is doorframe shape, and two vertical column separations are before the right side turntable is lateral
Afterwards, the interior lateral face of cuboid horizontal gird is parallel and close with the outer lateral face of the right side turntable；The middle part of the crossbeam
There is crossbeam hole；The crossbeam hole, internal diameter are equal to or more than the internal diameter of centre bore on the right side turntable, axis and the centre bore
Axis overlaps；The lower face of two columns of the right side axle bed respectively the upper surface with the lower decks of corresponding position with tight fit side
Formula connects.
The quiet gear of the axle bed component is circular ring shape, and internal diameter is more than the internal diameter in axle bed hole on the left side axle bed, outside
Diameter is equal to the outer diameter of side gear on the left side turntable, and the number of teeth on external peripheral surface is equal on the side gear external peripheral surface
The number of teeth, axial width are more than the axial width of transition gear on the left side turntable, and axis is overlapped with the axis in the axle bed hole,
The interior lateral face of its outer lateral face and the left side axle bed of corresponding position snugly links together.
The shaft, outer diameter are equal to the internal diameter of centre bore on the left side turntable or the right side turntable, are inserted into the left side and turn
The centre bore of disk, the centre bore of the right side turntable, the axle bed hole of the left side axle bed, the right side axle bed upper beam crossbeam hole in,
It snugly links together with the left side turntable or the right side turntable, fixes and connects with the left side axle bed or the crossbeam
It is connected together, left end laterally faces out stretching from the outer of the left side axle bed；Quiet gear on the left side axle bed, in
Lateral face is opposed with the outer lateral face of the left side turntable of corresponding position but does not contact, with four transition on the left side turntable
Gear engages.
The dynamical system is containing shaft gear, motor, motor gear.
The shaft gear of the dynamical system is snugly sleeved on the shaft from the external part of the left side axle bed.
The motor of the dynamical system, there is horizontal power output shaft thereon, is snugly connected to the left-hand axis
On the upper surface of the lower decks in seat outside.
The motor gear of the dynamical system, outer diameter are less than the outer diameter of the shaft gear, are snugly set with
On the power output shaft of the motor, engaged with the shaft gear.
During the dynamical system drives the corner that the rotary body is rotated around the axis of the shaft relative to the aircraft carrier as θ,
Four pieces on the rotary body are held one of machine plate, are on the one hand θ with respect to the corner that the aircraft carrier rotates synchronously, on the other hand relatively should again
The corner of rotary body negative direction rotation is-θ, and it is zero that this four pieces, which are held one of machine plate with respect to the corner of the aircraft carrier, that is to say, that rotation
Although body rotates, this four pieces are held one of machine plate and remain horizontality.
The application method of the aircraft carrier elevator is such：
Aircraft carrier rises to the upper deck from the lower decks：
The dynamical system drives the rotary body to be rotated around the axis of the shaft, when the rotary body lastblock holds the upper table of machine plate
During the upper surface flush of face and the lower decks, which, which is stopped, makes the rotary body stop operating, aircraft carrier from this
Lower decks is entered this and is held on machine plate by the corresponding entrance of right side turntable and the right end for holding machine plate on the rotary body；The power
System drives the rotary body to rotate again, when this holds the upper surface of machine plate and the upper surface flush of the upper deck, the dynamical system
Being stopped makes the rotary body stop operating, and aircraft carrier is entered by the left end for holding machine plate on the upper deck.
90 ° of every turn of the rotary body, the rotary body receive a frame aircraft carrier to enter in it from the lower decks, send out frame boat
Female aircraft is interior to the upper deck from it, and receiving and submitting are carried out at the same time.
Aircraft carrier is down to the lower decks from the upper deck：
The dynamical system drives the rotary body to be rotated around the axis of the shaft, when the rotary body lastblock holds the upper table of machine plate
During the upper surface flush of face and the upper deck, which, which is stopped, makes the rotary body stop operating, aircraft carrier from this
Upper deck enters this by the left end for holding machine plate and holds on machine plate；The dynamical system drives the rotary body to rotate again, when this holds machine
When the upper surface of plate and the upper surface flush of the lower decks, which, which is stopped, makes the rotary body stop operating, aircraft carrier
Aircraft holds the right end of machine plate and the corresponding entrance of the right side turntable by this, enters on the lower decks.
90 ° of every turn of the rotary body, the rotary body receive a frame aircraft carrier to enter in it from the upper deck, send out frame boat
Female aircraft is interior to the lower decks from it, and receiving and submitting are carried out at the same time.
After such structure, since rotary body can rotate, machine strip of holding thereon aircraft carrier and is rotated with it
And hangar can be down to by aircraft carrier slave qurush to upper deck and by aircraft carrier from upper deck by lifting.
After such structure, since the cooperation of quiet gear, transition gear, side gear cooperates with, due to quiet gear and side
The outer diameter of gear, the number of teeth are identical, make to hold machine plate rotated in company with rotary body with respect to aircraft carrier it is big with the angle that is rotated relative to the rotary body
Small equal, rotation direction remains horizontality on the contrary, this holds machine plate, which will not overturn.
After such structure, when being located at extreme higher position due to holding machine plate, the upper surface of upper surface and upper deck is neat
Flat, aircraft carrier, which smoothly can enter this from the upper deck and hold on machine plate or hold machine plate from this, to be entered on the upper deck；Due to
When holding machine plate and being located at extreme lower position, the upper surface flush of upper surface and lower decks, aircraft carrier can be smoothly from the lower decks
It enters this and holds on machine plate or hold machine plate from this and enter on the lower decks.
After such structure, since the torque of the opposite shaft axis of the gravity of rotary body is zero, there are four frame phases thereon
During with aircraft carrier, the gravity of this four framves aircraft carrier is zero, thus rotate the rotary body needs with respect to the torque of shaft axis
The torque of external force need only overcome the torque of resistance.Although in the case of rotary body underload, the torque for needing external force is larger,
At least rotating unloaded rotary body needs the torque very little of external force, saves significantly on the energy.This is better than conventional elevator, conventional elevator
Zero load is also consumed when rising compared with multiple-energy-source.
After such structure, when promoting aircraft carrier, 90 ° of every turn of rotary body, the rotary body receives a frame aircraft carrier to fly
Machine enters from the lower decks in it, sends out a frame aircraft carrier out of it to the upper deck, and receiving and submitting are carried out at the same time；Boat
When female aircraft enters hangar, 90 ° of every turn of the rotary body, the rotary body receives a frame aircraft carrier to enter in it from the upper deck, send
Go out a frame aircraft carrier out of it to the lower decks, and receiving and submitting are carried out at the same time.The time that rotary body turns 90 ° of needs is short,
In addition it receives and submitting is carried out at the same time, because regardless of promotion aircraft carrier or aircraft carrier enter hangar, quickly, efficiency is very for speed
Height, this is that conventional elevator can not be compared.
Aircraft carrier is for fighting.It uses military forces and is valued for rapidly.The invention quickly launches an attack for aircraft carrier and creates condition,
After such structure, the fighting capacity of aircraft carrier can be undoubtedly promoted.
Description of the drawings
The specific embodiment of the present invention is described in further detail below in conjunction with the accompanying drawings.
Fig. 1 is the sectional elevation schematic diagram along the aircraft carrier elevator of shaft axis.
Fig. 2 is the schematic cross section of the line A-A along Fig. 1.
Fig. 3 is the schematic cross section of the line B-B along Fig. 1.
Fig. 4 is the schematic cross section of the line C-C along Fig. 1.
Fig. 5 is the schematic cross section of the line D-D along Fig. 1.
Specific embodiment
As shown in respectively scheming Fig. 1 to Fig. 5, a kind of aircraft carrier elevator, the upper deck containing aircraft carrier landing on aircraft carrier
16th, the lower decks 17 parked in aircraft carrier hangar for aircraft carrier, shaft 2, rotary body, axle bed component, dynamical system.
As shown in Figure 1, there is window 16a on rectangle on the upper deck 16.
As shown in Figure 1, having window 17a under rectangle on the lower decks 17, which is located at upper on the upper deck 16
The underface of window 16a, the longitudinal length of the lower window 17a are more than the longitudinal length of window 16a on this, the lower window 17a's
Transverse width is more than the transverse width of window 16a on this.
As shown in respectively scheming Fig. 1 to Fig. 5, which contains turntable 1, holds machine plate 3.
As shown in respectively scheming Fig. 1 to Fig. 5, in two turntables 1 of the rotary body, a turntable 1 is located at left side, is called left side and turns
Disk 1, another turntable 1 are located at right side, are called right side turntable 1, which overlaps with the axis horizontal of the right side turntable 1.
The left side turntable 1 or the right side turntable 1, center is there are one round center hole 1a, close to the same circumference at edge in disk
On be uniformly distributed four lateral opening 1b, axis is overlapped with the axis of centre bore 1a, one of axis and this four lateral opening 1b's
Axis is parallel, and vertex puts in the lower window of the lower decks 17 close to the lower surface of the upper deck 16, the arcuate section of its underpart
In cavity below the 17a and lower window 17a.Four lateral opening 1b on the left side turntable 1 and four sides on the right side turntable 1
Hole 1b mirror symmetries.The interior lateral face of the left side turntable 1 is flushed with the vertical left window wall of window 16a on this.The right side turntable 1
Interior lateral face is flushed with the vertical right window wall of window 16a on this, the vertical right window wall of the lower window 17a and the right side of corresponding position
The outer lateral face of side turntable 1 is opposed and close.
As shown in Figure 1, Figure 3, there are four rounded transitional hole 1c, this four transitional pore 1c difference positions on the left side turntable 1
In the middle of one of centre bore 1a on the left side turntable 1 and four lateral opening 1b.The axis of the left side turntable 1 respectively with this four
The axis of one of transitional pore 1c is parallel.
As shown in Figure 1, Figure 2, Figure 3 shows, four left side axis 4a, four square wheels, 5, four side gears are installed on the left side turntable 1
6th, four transition gears, 7, four transition axises 8.
As shown in Figure 1 and Figure 2, four left side axis 4a on the left side turntable 1, are respectively fixedly connected on the left of this on turntable 1
One of four lateral opening 1b in.One of this four left side axis 4a, inner end are stretched out from the interior lateral face of the left side turntable 1, outside
It holds from the outer lateral face of the left side turntable 1 and stretches out.
As shown in Figure 1, Figure 2, Figure 3 shows, the roomy outer lateral face of four cuboid square wheels 5 on the left side turntable 1, respectively
Snugly on the inner end of one of four left side axis 4a on coaxially connected turntable on the left of this 1.This four square wheels 5 it
One, outer lateral face and the interior lateral face of the left side turntable 1 are opposed and close, are located at extreme higher position, upper horizontal surface
It stretches to except 1 edge of left side turntable, and in the upper window 16a of the upper deck 16, the transverse width of upper horizontal surface
More than the vertical height of end face.
As shown in Figure 1 and Figure 2, four side gears 6 on the left side turntable 1, are snugly sleeved on the left side respectively
On turntable 1 on the outer end of one of four left side axis 4a.Axis of one of this four side gears 6 in the left side axis 4a where it revolves
During turning, edge is without departing from the edge of the left side turntable 1.
As shown in Figure 1, Figure 2, Figure 3 shows, four transition axises 8 on the left side turntable 1, are snugly connected to this respectively
In one of four transitional pore 1c on left side turntable 1.One of this four transition axises 8, the left side of inner end and corresponding position
The interior lateral face of turntable 1 flushes, and outer end is stretched out from the outer lateral face of the left side turntable 1.
As shown in Figure 1 and Figure 2, four transition gears 7 on the left side turntable 1, are fixedly set in the left side turntable 1 respectively
On the outer end of one of upper four transition axises 8.This four transition gears 7 are respectively one of with four side gears 6 on the left side turntable 1
Engagement.
As shown in Figure 1, Figure 4, Figure 5, four the right axis 4b, four square wheels 5 are installed on the right side turntable 1.
As Figure 1 and Figure 4, four the right axis 4b on the right side turntable 1, are respectively fixedly connected on the right side of this on turntable 1
One of four lateral opening 1b in.One of axis 4b on the right of in the of this four, inner end are stretched out from the interior lateral face of the right side turntable 1,
Outer end face is flushed with the outer lateral face of the right side turntable 1.
As shown in Figure 1, Figure 4, Figure 5, the roomy outer lateral face of four cuboid square wheels 5 on the right side turntable 1, respectively
Snugly on the inner end of one of four the right axis 4b of coaxially connected turntable on the right side of this 1.This four square wheels 5 it
One, outer lateral face and the interior lateral face of the right side turntable 1 are opposed and close, are located at extreme higher position, upper horizontal surface
It stretches to except 1 edge of right side turntable and in the upper window 16a of the upper deck 16, the transverse width of upper horizontal surface is big
Vertical height in end face.
As shown in Figure 1, Figure 4, Figure 5, have on the right side turntable 1 for aircraft carrier by four entrances 15, this four
Entrance 15 is located at the centre of one of centre bore 1a and four lateral opening 1b on the right side turntable 1 respectively.This four entrances 15 it
One, it is hexagon, for the hexagon close to the part of centre bore 1a in antiparallelogram, the part far from centre bore 1a is in square
One of shape, the trapezoidal two sides and the angle at bottom thereon are equal to or more than 135 °.One of this four entrances 15, being located at should
On right side turntable 1 during the underface of centre bore 1a, height is more than the height of aircraft carrier, and the transverse width of its underpart rectangle is big
In the width of aircraft carrier, bottom surface and the upper surface flush of the lower decks 17.
Four pieces of levels are installed as shown in respectively scheming Fig. 1 to Fig. 5, on the rotary body and hold machine plate 3.This four pieces are held one of machine plate 3,
Longitudinal length is more than the length of aircraft carrier, and transverse width is more than the width of aircraft carrier.This four pieces are held machine plate 3, left end
Neighbouring lower surface is snugly connected on the left side turntable 1 level right over one of four square wheels 5 axis respectively
On upper surface, the lower surface near right end be snugly connected to respectively on the right side turntable 1 corresponding four square wheels 5 it
In upper horizontal surface right over one axis, one of four square wheels 5, horizontal upper table on the left side turntable 1 or the right side turntable 1
The transverse width in face is more than the vertical height of its end face.This four pieces are held one of machine plate 3, in extreme lower position, are located under this
In the lower window 17a on deck 17, upper surface is flushed with the bottom surface of the entrance 15 on the right side turntable 1 of corresponding position.This
Four pieces are held one of machine plate 3, when being located at extreme higher position, are located in the upper window 16a of the upper deck 16, on upper surface and this
The upper surface flush on deck 16, left side and the left window wall of window 16a on this of corresponding position are opposed and close.
As shown in Figure 1, axle bed component axle bed containing left side 9, right side axle bed, the quiet gear 14.
As shown in Figure 1, the left side axle bed 9 of the axle bed component, is quadrangular, it is erected in the outside of the left side turntable 1
And close to the left side turntable 1, nearby there is circular shaft bore 9a in the upper end.Axle bed hole 9a, internal diameter are equal to or more than the left side
The internal diameter of centre bore 1a on turntable 1, axis are overlapped with the axis of centre bore 1a.The lower face of the left side axle bed 9 with it is corresponding
The upper surface of the lower decks 17 of position snugly connects.
As shown in Figure 1, the right side axle bed of the axle bed component, is doorframe shape, two vertical column separations turn in the right side
Lateral front and rear of disk 1, the interior lateral face of cuboid horizontal gird 18 is parallel with the outer lateral face of the right side turntable 1 and connects
Closely.There is crossbeam hole 18a at the middle part of the crossbeam 18.Crossbeam hole 18a, internal diameter are equal to or more than centre bore on the right side turntable 1
The internal diameter of 1a, axis are overlapped with the axis of centre bore 1a.The lower face of two columns of the right side axle bed respectively with corresponding positions
The upper surface of the lower decks 17 put snugly connects.
As shown in Figure 1 and Figure 2, the quiet gear 14 of the axle bed component, is circular ring shape, and internal diameter is more than on the left side axle bed 9
The internal diameter of axle bed hole 9a, outer diameter are equal to the outer diameter of side gear 6 on the left side turntable 1, and the number of teeth on external peripheral surface is equal to
The number of teeth on 6 external peripheral surface of side gear, axial width are more than the axial width of transition gear 7 on the left side turntable 1,
Axis is overlapped with the axis of axle bed hole 9a, and the interior lateral face of the left side axle bed 9 of outer lateral face and corresponding position is with close-fitting
Conjunction mode links together.
As shown in Figure 1, the shaft 2, outer diameter is equal to the internal diameter of centre bore 1a on the left side turntable 1 or the right side turntable 1,
It is inserted into the centre bore 1a of the left side turntable 1, the centre bore 1a of the right side turntable 1, the axle bed hole 9a of the left side axle bed 9, the right side
In the crossbeam hole 18a of side axle seat upper beam 18, one is snugly connected to the left side turntable 1 or the right side turntable 1
It rises, is fixed together with the left side axle bed 9 or the crossbeam 18, left end is laterally faced out from the outer of the left side axle bed 9
It stretches out.The outer lateral face of the left side turntable 1 of the quiet gear 5 on the left side axle bed 9, interior lateral face and corresponding position
It is opposed but do not contact, it is engaged with four transition gears 7 on the left side turntable 1.
As shown in Figure 1, the dynamical system is containing shaft gear 10, motor 11, motor gear 13.
As shown in Figure 1, the shaft gear 10 of the dynamical system is snugly sleeved on the shaft 2 from the left side axle bed
On 9 external part.
As shown in Figure 1, the motor 11 of the dynamical system, has horizontal power output shaft 12, snugly thereon
It is connected on the upper surface of the lower decks 17 in 9 outside of left side axle bed.
As shown in Figure 1, the motor gear 13 of the dynamical system, outer diameter is less than the outer diameter of the shaft gear 10, with
Tight fit mode is sleeved on the power output shaft 12 of the motor 11, is engaged with the shaft gear 10.
As shown in Figure 1 and Figure 2, which drives the rotary body to turn around the axis of the shaft 2 relative to what the aircraft carrier rotated
During angle is θ, four pieces on the rotary body are held one of machine plate 3, are on the one hand θ with respect to the corner that the aircraft carrier rotates synchronously,
On the other hand the corner rotated again relative to the rotary body negative direction is-θ, this four pieces are held corners of one of the machine plate 3 with respect to the aircraft carrier
It is zero, that is to say, that although rotary body rotates, this four pieces are held one of machine plate 3 and remain horizontality.
The application method of the aircraft carrier elevator is such：
As shown in Figure 1, aircraft carrier rises to the upper deck 16 from the lower decks 17：
The dynamical system drives the rotary body to be rotated around the axis of the shaft 2, when the rotary body lastblock holds the upper of machine plate 3
When surface and the upper surface flush of the lower decks 17, which, which is stopped, makes the rotary body stop operating, aircraft carrier
It enters this from the lower decks 17 by the corresponding entrance 15 of right side turntable 1 and the right end for holding machine plate 3 on the rotary body and holds machine
On plate 3.The dynamical system drive again the rotary body rotate, when this hold machine plate 3 upper surface and the upper surface of the upper deck 16 it is neat
Usually, which, which is stopped, makes the rotary body stop operating, and the left end that aircraft carrier holds machine plate 3 by this is entered on this
On deck 16.
90 ° of every turn of the rotary body, the rotary body receive a frame aircraft carrier to enter in it from the lower decks 17, send out a frame
Aircraft carrier is interior to the upper deck 16 from it, and receiving and submitting are carried out at the same time.
As shown in Figure 1, aircraft carrier is down to the lower decks 17 from the upper deck 16：
The dynamical system drives the rotary body to be rotated around the axis of the shaft 2, when the rotary body lastblock holds the upper of machine plate 3
When surface and the upper surface flush of the upper deck 17, which, which is stopped, makes the rotary body stop operating, aircraft carrier
This is entered from the upper deck 16 by the left end for holding machine plate 3 to hold on machine plate 3.The dynamical system drives the rotary body to rotate again,
When this holds the upper surface of machine plate 3 and the upper surface flush of the lower decks 17, which, which is stopped, stops the rotary body
Rotation stop is moved, and aircraft carrier holds the right end of machine plate 3 and the corresponding entrance 15 of the right side turntable 1 by this, enters the lower decks 17
On.
90 ° of every turn of the rotary body, the rotary body receive a frame aircraft carrier to enter in it from the upper deck 16, send out a frame
Aircraft carrier is interior to the lower decks 17 from it, and receiving and submitting are carried out at the same time.
Really, which can also be used for lifting other weapons, goods and materials, vehicle, mechanical equipment, personnel.
Embodiments of the present invention are explained in detail above in conjunction with attached drawing.The present invention is not limited to above-mentioned embodiment party
Formula, can also be before present inventive concept not be departed from the knowledge having in technical field those of ordinary skill
Put that various changes can be made.The various change made under the premise of present inventive concept is not departed from, still falls within the scope of the present invention.
Claims (2)
1. a kind of aircraft carrier elevator, aircraft carrier is supplied in upper deck (16) and aircraft carrier hangar containing aircraft carrier landing on aircraft carrier
The lower decks (17) that aircraft is parked, it is characterised in that：
There is window on rectangle (16a) on the upper deck (16)；
There is window under rectangle (17a) on the lower decks (17), the lower window (17a) is upper on the upper deck (16)
The underface of window (16a), the longitudinal length of the lower window (17a) is more than the longitudinal length of the upper window (16a), described
The transverse width of lower window 1 (17a) is more than the transverse width of the upper window (16a)；
The aircraft carrier elevator is also containing shaft (2), rotary body, axle bed component, dynamical system；
The rotary body contains turntable (1), holds machine plate (3)；
In two turntables (1) of the rotary body, a turntable (1) is called left side turntable (1), another turntable positioned at left side
(1) positioned at right side, it is called right side turntable (1), the left side turntable (1) overlaps with the axis horizontal of the right side turntable (1)；Institute
State left side turntable (1) or the right side turntable (1), center is there are one round center hole (1a), close to edge in disk
Four lateral opening (1b) is uniformly distributed on same circumference, axis is overlapped with the axis of the centre bore (1a), axis with this four
The axis of one of a lateral opening (1b) is parallel, and close to the lower surface of the upper deck (16), the arcuate section of its underpart stretches on vertex
Into in the cavity below the lower window (17a) of the lower decks (17) and the lower window (17a)；On the left side turntable (1)
Four lateral opening (1b) and the right side turntable (1) on four lateral opening (1b) mirror symmetries；The inside of the left side turntable (1)
It is flushed to face with the vertical left window wall of the upper window (16a)；The interior lateral face of the right side turntable (1) and the upper window
The vertical right window wall of (16a) flushes, the vertical right window wall of the lower window (17a) and the right side turntable (1) of corresponding position
Outer lateral face it is opposed and close；
There are four rounded transitional holes (1c), this four transitional pores (1c) on the left side turntable (1) to be located at the left side respectively
The middle of one of centre bore (1a) and four lateral opening (1b) on turntable (1)；The axis of the left side turntable (1) respectively with this four
The axis of one of a transitional pore (1c) is parallel；
Four left side axis (4a), four square wheels (5), four side gears (6), four transition teeth are installed on the left side turntable (1)
Take turns (7), four transition axises (8)；
Four left side axis (4a) on the left side turntable (1), are respectively fixedly connected with four sides on the left side turntable (1)
In one of hole (1b)；One of this four left side axis (4a), inner end are stretched out from the interior lateral face of the left side turntable (1), outside
It holds from the outer lateral face of the left side turntable (1) and stretches out；
The roomy outer lateral face of four cuboid square wheels (5) on the left side turntable (1), it is snugly coaxial respectively
It is connected on the inner end of one of four left side axis (4a) on the left side turntable (1)；One of this four square wheels (5), outside
Lateral face and the interior lateral face of the left side turntable (1) are opposed and close, are located at extreme higher position, upper horizontal surface is stretched to
Except left side turntable (1) edge, and in the upper window (16a) of the upper deck (16), the horizontal stroke of upper horizontal surface
It is more than the vertical height of end face to width；
Four side gears (6) on the left side turntable (1), are snugly sleeved on respectively on the left side turntable (1)
On the outer end of one of four left side axis (4a)；One of this four side gears (6) are revolved in the axis of the left side axis (4a) where it
During turning, edge is without departing from the edge of the left side turntable (1)；
Four transition axises (8) on the left side turntable (1), are snugly connected to respectively on the left side turntable (1)
One of four transitional pores (1c) in；The left side turntable of one of this four transition axises (8), inner end and corresponding position
(1) interior lateral face flushes, and outer end is stretched out from the outer lateral face of the left side turntable (1)；
Four transition gears (7) on the left side turntable (1) are fixedly set in upper four mistakes of the left side turntable (1) respectively
It crosses on the outer end of one of axis (8)；This four transition gears (7) respectively with four side gears (6) on the left side turntable (1) it
One engagement；
Four the right axis (4b), four square wheels (5) are installed on the right side turntable (1)；
Four the right axis (4b) on the right side turntable (1), are respectively fixedly connected with four sides on the right side turntable (1)
In one of hole (1b)；One of axis (4b) on the right of in the of this four, inner end are stretched out from the interior lateral face of the right side turntable (1),
Outer end face is flushed with the outer lateral face of the right side turntable (1)；
The roomy outer lateral face of four cuboid square wheels (5) on the right side turntable (1), it is snugly coaxial respectively
It is connected on the inner end of one of four the right axis (4b) of the right side turntable (1)；One of this four square wheels (5), outside
It is opposed and close to face and the interior lateral face of the right side turntable (1), it is located at extreme higher position, upper horizontal surface stretches to institute
State right side turntable (1) edge except and positioned at the upper deck (16) upper window (16a) in, upper horizontal surface it is laterally wide
Degree is more than the vertical height of end face；
Have on the right side turntable (1) for aircraft carrier by four entrances (15), this four entrances (15) positions respectively
In the centre of one of centre bore (1a) on the right side turntable (1) and four lateral opening (1b)；One of this four entrances (15),
For hexagon, the hexagon is close to the part of the centre bore (1a) in antiparallelogram, the part of the separate centre bore (1a)
Rectangular, one of described trapezoidal two sides and the angle at bottom thereon are equal to or more than 135 °；One of this four entrances (15),
When it is located at the underface of centre bore (1a) on the right side turntable (1), height is more than the height of aircraft carrier, its underpart square
The transverse width of shape is more than the width of aircraft carrier, bottom surface and the upper surface flush of the lower decks (17)；
Four pieces of levels on the rotary body are installed and hold machine plate (3)；This four pieces are held one of machine plate (3), and longitudinal length is more than aircraft carrier
The length of aircraft, transverse width are more than the width of aircraft carrier；This four pieces are held machine plate (3), the lower surface near left end point
It is not connected to snugly in the upper horizontal surface right over one of upper four square wheels (5) of the left side turntable (1) axis,
Lower surface near its right end is snugly connected to one of corresponding four square wheels (5) on the right side turntable (1) respectively
In upper horizontal surface right over axis, one of the left side turntable (1) or upper four square wheels (5) of the right side turntable (1),
The transverse width of upper horizontal surface is more than the vertical height of its end face；This four pieces are held one of machine plate (3), in extreme lower position,
It is located in the lower window (17a) of the lower decks (17), going out on the right side turntable (1) of upper surface and corresponding position
The bottom surface of entrance (15) flushes；This four pieces are held one of machine plate (3), when being located at extreme higher position, are located at the upper deck (16)
Upper window (16a) in, the upper surface flush of upper surface and the upper deck (16), left side and corresponding position it is described
The left window wall of upper window (16a) is opposed and close；
Axle bed component axle bed containing left side (9), right side axle bed, quiet gear (14)；
The left side axle bed (9) of the axle bed component, is quadrangular, is erected in the outside of the left side turntable (1) and approaches
Nearby there are circular shaft bore (9a) in the left side turntable (1), the upper end；The axle bed hole (9a), internal diameter are equal to or more than institute
The internal diameter of centre bore (1a) on left side turntable (1) is stated, axis is overlapped with the axis of the centre bore (1a)；The left side axle bed
(9) lower face and the upper surface of the lower decks (17) of corresponding position snugly connects；
The right side axle bed of the axle bed component is doorframe shape, and two vertical column separations are in the right side turntable (1) transverse direction
Front and rear, the interior lateral face of cuboid horizontal gird (18) is parallel and close with the outer lateral face of the right side turntable (1)；Institute
Stating has crossbeam hole (18a) in the middle part of crossbeam (18)；The crossbeam hole (18a), internal diameter are equal to or more than the right side turntable (1)
The internal diameter of upper centre bore (1a), axis are overlapped with the axis of the centre bore (1a)；Under two columns of the right side axle bed
Upper surface of the end face respectively with the lower decks of corresponding position (17) is snugly connect；
The quiet gear (14) of the axle bed component, is circular ring shape, and internal diameter is more than axle bed hole (9a) on the left side axle bed (9)
Internal diameter, outer diameter is equal to the outer diameter of side gear (6) on the left side turntable (1), and the number of teeth on external peripheral surface is equal to institute
The number of teeth on side gear (6) external peripheral surface is stated, axial width is more than the axis of transition gear (7) on the left side turntable (1)
To thickness, axis is overlapped with the axis of the axle bed hole (9a), the left side axle bed (9) of outer lateral face and corresponding position
Interior lateral face snugly link together；
The shaft (2), outer diameter are equal to the internal diameter of centre bore (1a) on the left side turntable (1) or the right side turntable (1),
It is inserted into centre bore (1a), the left side axle bed (9) of the centre bore (1a) of the left side turntable (1), the right side turntable (1)
Axle bed hole (9a), the right side axle bed upper beam (18) crossbeam hole (18a) in, with the left side turntable (1) or described
Right side turntable (1) snugly links together, and is fixedly connected on the left side axle bed (9) or the crossbeam (18)
Together, left end laterally faces out stretching from the outer of the left side axle bed (9)；Quiet tooth on the left side axle bed (9)
It takes turns (5), interior lateral face is opposed with the outer lateral face of the left side turntable (1) of corresponding position but does not contact, with the left side
Four transition gears (7) engagement on side turntable (1)；
The dynamical system is containing shaft gear (10), motor (11), motor gear (13)；
The shaft gear (10) of the dynamical system is snugly sleeved on the shaft (2) from the left side axle bed (9)
External part on；
The motor (11) of the dynamical system, has horizontal power output shaft (12), is snugly connected to institute thereon
On the upper surface for stating the lower decks (17) on the outside of left side axle bed (9)；
The motor gear (13) of the dynamical system, outer diameter is less than the outer diameter of the shaft gear (10), with tight fit
Mode is sleeved on the power output shaft (12) of the motor (11), is engaged with the shaft gear (10)；
It around the axis of the shaft (2) is θ's relative to the corner that the aircraft carrier rotate that the dynamical system, which drives the rotary body,
In the process, four pieces on the rotary body hold one of machine plate (3), and the corner that on the one hand relatively described aircraft carrier rotates synchronously is θ, separately
On the one hand the corner again relative to rotary body negative direction rotation is-θ, this four pieces are held the relatively described aircraft carrier of one of machine plate (3)
Corner is zero, that is to say, that although rotary body rotates, this four pieces are held one of machine plate (3) and remain horizontality.
A kind of 2. method using aircraft carrier elevator described in claim 1：
Aircraft carrier rises to the upper deck (16) from the lower decks (17)：
The dynamical system drives the rotary body to be rotated around the axis of the shaft (2), when the rotary body lastblock holds machine
When the upper surface of plate (3) and the upper surface flush of the lower decks (17), the dynamical system, which is stopped, makes the rotary body
It stops operating, aircraft carrier passes through the corresponding entrance (15) of right side turntable (1) on the rotary body from the lower decks (17)
Described hold on machine plate (3) is entered with the right end for holding machine plate (3)；The dynamical system drives the rotary body to rotate again, when
When the upper surface for holding machine plate (3) and the upper surface flush of the upper deck (16), the dynamical system, which is stopped, makes institute
It states rotary body to stop operating, aircraft carrier is entered by the left end for holding machine plate (3) on the upper deck (16)；
90 ° of every turn of the rotary body, the rotary body receive a frame aircraft carrier to be sent out from the lower decks (17) into it
One frame aircraft carrier is interior to the upper deck (16) from it, and receiving and submitting are carried out at the same time；
Aircraft carrier is down to the lower decks (17) from the upper deck (16)：
The dynamical system drives the rotary body to be rotated around the axis of the shaft (2), when the rotary body lastblock holds machine
When the upper surface of plate (3) and the upper surface flush of the upper deck (17), the dynamical system, which is stopped, makes the rotary body
It stops operating, aircraft carrier enters described hold on machine plate (3) from the upper deck (16) by the left end for holding machine plate (3)；
The dynamical system drives the rotary body to rotate again, upper when the upper surface for holding machine plate (3) and the lower decks (17)
When surface flushes, the dynamical system, which is stopped, makes the rotary body stop operating, and aircraft carrier holds machine plate (3) by described
Right end and the right side turntable (1) corresponding entrance (15), enter on the lower decks (17)；
90 ° of every turn of the rotary body, the rotary body receive a frame aircraft carrier to be sent out from the upper deck (16) into it
One frame aircraft carrier is interior to the lower decks (17) from it, and receiving and submitting are carried out at the same time.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711398723.1A CN108177793A (en) | 2017-12-13 | 2017-12-13 | Aircraft carrier elevator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711398723.1A CN108177793A (en) | 2017-12-13 | 2017-12-13 | Aircraft carrier elevator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108177793A true CN108177793A (en) | 2018-06-19 |
Family
ID=62547112
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711398723.1A Pending CN108177793A (en) | 2017-12-13 | 2017-12-13 | Aircraft carrier elevator |
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| Country | Link |
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| CN (1) | CN108177793A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111470015A (en) * | 2020-05-19 | 2020-07-31 | 济南环太机电技术有限公司 | Lifting deck type aircraft carrier |
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Application publication date: 20180619 |