CN107826263A - Helicopter parks pivoted frame - Google Patents
Helicopter parks pivoted frame Download PDFInfo
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- CN107826263A CN107826263A CN201711110893.5A CN201711110893A CN107826263A CN 107826263 A CN107826263 A CN 107826263A CN 201711110893 A CN201711110893 A CN 201711110893A CN 107826263 A CN107826263 A CN 107826263A
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- 230000007704 transition Effects 0.000 claims abstract description 63
- 230000005540 biological transmission Effects 0.000 claims abstract description 6
- 238000000034 method Methods 0.000 claims abstract description 6
- 239000011148 porous material Substances 0.000 claims description 12
- 230000002093 peripheral effect Effects 0.000 claims description 7
- 230000004323 axial length Effects 0.000 claims description 6
- 208000031872 Body Remains Diseases 0.000 claims description 5
- 230000000694 effects Effects 0.000 claims description 5
- 230000001360 synchronised effect Effects 0.000 claims description 3
- 239000000203 mixture Substances 0.000 claims description 2
- 230000007306 turnover Effects 0.000 claims description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims description 2
- 238000010276 construction Methods 0.000 abstract description 2
- 230000005484 gravity Effects 0.000 abstract description 2
- 238000012423 maintenance Methods 0.000 abstract description 2
- 238000005516 engineering process Methods 0.000 description 5
- 238000010586 diagram Methods 0.000 description 2
- 230000003068 static effect Effects 0.000 description 2
- FGRBYDKOBBBPOI-UHFFFAOYSA-N 10,10-dioxo-2-[4-(N-phenylanilino)phenyl]thioxanthen-9-one Chemical compound O=C1c2ccccc2S(=O)(=O)c2ccc(cc12)-c1ccc(cc1)N(c1ccccc1)c1ccccc1 FGRBYDKOBBBPOI-UHFFFAOYSA-N 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
- B64F1/02—Arresting gear; Liquid barriers
Abstract
The present invention relates to a kind of helicopter to park pivoted frame, its body containing frame, axle bed component, motor (11), transmission device.Frame body is made up of rotating disk (1), rotating shaft (2), shutdown plate (3), sheave (4), side gear (6), transition gear (7), transition axis (8).The resultant couple very little of the gravity of frame body and the helicopter parked thereon, the external force torque very little that rotating turret body needs, save the energy；The angle that frame body rotates is no more than 180 °, and with regard to helicopter can be allowed to land or taken off, principle rapidly is valued in accordance with using military forces；Frame body shuts down plate (3) and remains horizontality, the helicopter parked thereon will not inclination in rotation process；Originally the naval vessels deck of a frame helicopter, which can only be parked, can park two frame helicopters, improve deck utilization rate, fighting capacity greatly enhances；Simple in construction, easy to maintenance, cost is relatively low.
Description
Technical field
The present invention relates to a kind of helicopter to park pivoted frame, and can only especially park can on the naval vessels deck of a frame helicopter
The helicopter for parking two frame helicopters parks pivoted frame.The invention further relates to the application method that the helicopter parks pivoted frame.
Background technology
Special parking area delimited for helicopter on current naval vessels deck, can only park a frame in the region goes straight up to
Machine.The main function of naval vessels man the helo is antisubmarine.If the region of delimitation can park two frame helicopters, one-plus-one is more than
Two, two frame helicopters perform task, and hunting zone is bigger, and faster, fighting capacity significantly increases search progress.
The content of the invention
It can be parked on the naval vessels deck for parking a frame helicopter the technical problem to be solved in the present invention is to provide a kind of
The helicopter of two frame helicopters parks pivoted frame.Another technical problems to be solved is that the side of pivoted frame is parked using the helicopter
Method.
In order to solve the above technical problems, the technical scheme is that：
A kind of helicopter parks pivoted frame, its body containing frame, axle bed component, motor, transmission device.
This body shuts down plate, 4 sheaves, 4 side gears, 4 transition gears, 4 by two rotating disks, 1 rotating shaft, two pieces
Individual transition axis composition.
The rotating shaft is elongated cylinder, its axis horizontal, and its axial length is more than the length of helicopter.
In the two rotating disks, a rotating disk is located at right side, and another rotating disk is located at left side；The two rotating disks, its axis water
Flat to overlap, the distance between its interior lateral face is more than the length of helicopter；One of the two rotating disks, there is a circular central thereon
Hole, two circles are lateral opening, two rounded transitional holes, and its axis overlaps with the axis of the centre bore, and the internal diameter of the centre bore is equal to
The external diameter of the rotating shaft, the two transitional pores are respectively positioned at the centre bore centre one of lateral opening with the two；The two are lateral opening
One of the distance between the axis of axis and the centre bore be more than the height of helicopter；Two sides on the rotating disk on right side
Hole and two lateral opening speculars on the rotating disk in left side；4 lateral opening, 4 transitional pores are shared on the two rotating disks.
One of this 4 sheaves, it is made up of coaxial overall sheave disk and fluted roller shaft；The sheave disk, its external diameter, which is more than, goes straight up to
The width of machine, there is radial level race on its interior lateral face, and the lateral length of the race is equal to the external diameter of the sheave disk；The sheave
Axle, its axis horizontal, its axial length are more than the axial width of one of the two rotating disks, and its external diameter is equal to or less than the two turns
Lateral opening internal diameter on disk；Fluted roller shaft on this 4 sheaves insert respectively 4 on the two rotating disks it is one of lateral opening in, this 4 grooves
Fluted roller shaft on one of wheel, it is fixed together with the rotating disk where it, rotating disk of its outer end where it is outer lateral
Towards overhanging；The outer lateral face of sheave disk on one of this 4 sheaves is interior lateral with the rotating disk of the relevant position where it
Face is opposed；In the two rotating disks, there are two sheaves on the rotating disk positioned at right side or the rotating disk positioned at left side, be total on the two rotating disks
4 sheaves are installed.
This two pieces are shut down one of plate, and it is horizontal rectangular plate, and its longitudinal length is less than in the two rotating disks between lateral face
Distance, its transverse width be equal to sheave on race lateral length, its vertical thickness be equal to the race vertical width；This two
Block shuts down plate, and its right-hand member is respectively embedded into the two rotating disks in the race of one of two sheaves on the rotating disk on right side and therewith
Snugly link together, its left end is respectively embedded into the two rotating disks two grooves corresponding on the rotating disk in left side
Link together therewith in the race of one of wheel and snugly, this two pieces horizontal axis for shutting down one of plate connect with it
The axis of two sheaves connect overlaps.
One of this 4 side gears, there is circular edges gear hole at its center, and its axis overlaps with the axis of the heel teeth wheel bore, should
The internal diameter of heel teeth wheel bore is equal to the external diameter of fluted roller shaft on sheave；The heel teeth wheel bore of this 4 side gears, is set in the two turns
On disk on the protruding end of the fluted roller shaft of one of 4 sheaves, and snugly link together therewith, this 4 sheaves
One of the outer face of fluted roller shaft flushed with being set with the outer lateral face of side gear thereon.
The external diameter of one of this 4 transition axises is equal to the internal diameter of transitional pore on the two rotating disks；The inner end of this 4 transition axises,
Insert on the two rotating disks in one of 4 transitional pores, and snugly link together therewith respectively；This 4 transition axises
One of, its inner end flushes with the interior lateral face of its rotating disk being connected, outer lateral face of its outer end from its rotating disk connected
It is protruding；4 transition axises are installed altogether on the two rotating disks.
One of this 4 transition gears, its axial width are equal to the axial width of side gear, and there is rounded transitional gear at its center
Hole, its axis overlap with the axis in the transition gear hole, and the internal diameter in the transition gear hole is equal to or more than mistake on the two rotating disks
Cross the external diameter of axle；The transition gear hole of this 4 transition gears, be set on the two rotating disks one of 4 transition axises to
Overhang on end, and fixed thereto link together；One of this 4 transition axises, transition gear of its outer face with suit thereon
Outer lateral face flush；One of this 4 transition gears engage on the rotating disk where it with the side gear of adjacent same radial direction.
The axle bed component is containing two axle beds, two quiet gears.
The two axle beds are respectively positioned at the outside of one of the two rotating disks；One of the two axle beds, its vertical height are less than
Nearby there is circular shaft bore the external diameter of rotating disk but the radius for being more than rotating disk, its upper end, and the internal diameter in the axle bed hole is equal to or more than should
The external diameter of rotating shaft；The axis in axle bed hole overlaps with the axis horizontal of the two rotating disks on the two axle beds, one of the two axle beds
Lower surface and the naval vessels deck of relevant position snugly link together.
One of the two quiet gears, it is annular, and its internal diameter is more than the external diameter of the rotating shaft, and its external diameter is equal to rotating disk top
The external diameter of gear, the number of teeth on its external peripheral surface are equal to the number of teeth on the side gear external peripheral surface, and its axial width is more than
The axial width of the side gear；The two quiet gears, axis of its axis respectively with the upper axle bed hole of one of the two axle beds overlap,
Its outer lateral face snugly links together with the interior lateral face of one of the two axle beds respectively.
The rotating shaft, it is inserted in the axle bed hole of the centre bore of the two rotating disks and the two axle beds, itself and the two rotating disks
Snugly link together, it is fixed together with the two axle beds, its horizontal axis and the two rotating disks
The axis in axle bed hole overlaps on axis or the two axle beds, and its one end laterally faces out stretching from the outer of the axle bed of Same Name of Ends；This
One of two quiet gears, its interior lateral face is opposed with the outer lateral face of the rotating disk of relevant position but does not contact, its phase with surrounding
Two transition gears engagement on the adjacent rotating disk.
There is horizontal power output shaft on the motor.
The transmission device is made up of big sprocket wheel, minor sprocket, chain.
There is circular big sprocket wheel hole at the big sprocket wheel, its center, and its axis overlaps with the axis in the big sprocket wheel hole, the big sprocket wheel hole
Internal diameter be equal to the rotating shaft external diameter；The big sprocket wheel borehole jack of the big sprocket wheel is mounted in the external part of rotating shaft lateral face outside axle bed
On, and snugly link together therewith.
The minor sprocket, it is located on same perpendicular with the big sprocket wheel, its external diameter be less than the big sprocket wheel external diameter, its with
Tight fit mode is arranged on the power output shaft of the motor.
The chain is sleeved on the big sprocket wheel and the minor sprocket.
The motor is powered after rotation, passes through the minor sprocket and chain-driving big sprocket wheel rotation, big sprocket wheel driving
Rotating shaft and two rotating disk synchronous rotaries on this body, so that two pieces on this body are shut down one of plates and followed in rotation
Ring lifts；At the same time, the effect quilt for the quiet gear that two transition gears rotated with one of the two rotating disks are engaged with
Compel to rotate, the two transition gears drive two side gears being engaged with to rotate respectively, and the two side gears drive respectively again
Two sheaves being attached thereto rotate；4 sheaves on the two rotating disks drive two blocks of shutdown plates anti-with respect to the two rotating disks again
Direction rotates, and shuts down the angle that the two relative rotating disks of one of plate reversely turn over for this two pieces and is equal to the two rotating disks with respect to ground turn
The angle crossed, so as to which one of this two blocks shutdown plates remain horizontality.
The application method that the helicopter parks pivoted frame is such：
First, helicopter is parked：
This body is rotated, shutdown plate vacant thereon is gone into extreme higher position, then makes this body remains stationary, directly
The machine of liter is dropped on the shutdown plate.
Second, helicopter takes off：
This body is rotated, the shutdown plate for parking helicopter thereon is gone into extreme higher position, then protects this body
Hold static, helicopter takes off from the shutdown plate.
After such structure, because quiet gear remains inactive state, its external diameter is equal to the external diameter of side gear, its
The number of teeth on external peripheral surface is equal to the number of teeth of side gear.When frame body rotates, with the transition gear that two rotating disks rotate by with
The effect of quiet gear of engagement be forced to rotate, and drive the side gear being engaged with to rotate, the side gear drives corresponding groove again
Wheel rotates；Sheave on the two rotating disks drives corresponding plate of shutting down to be rotated relative to the two rotating disk opposite directions again so that the two
Rotating disk is equal to the angle shut down plate and rotated relative to the two rotating disk opposite directions relative to the angle of ground rotation, shuts down plate with respect to ground
The angle of rotation is zero, thus shut down plate remain horizontality, the helicopter parked thereon will not inclination will not more roll.
After such structure, when frame body remains static, remain inactive state quiet gear prevent with
The transition gear of engagement rotate, it is impossible to the side gear rotation that the transition gear of rotation prevents to be engaged with again, side gear hinder again
Only the sheave of its connection rotates, and sheave prevents its shutdown plate connected from rotating again, even if the relative position gone straight up to is on plate is shut down
It is not placed in the middle, shut down plate and there will not be big deflection；When frame body rotates, the rotation for shutting down plate is controlled, and can only be rotated in order,
And it can not tamper.
The fit precision of each gear is high, and effect will be apparent upon.
Above-mentioned quiet gear, transition gear, side gear, sheave, the mutual cooperation and collaboration for shutting down plate, it is the key of the present invention
One of technology and important innovations.
After such structure, the quality of frame body is although larger, but its gravity is several with respect to the resultant couple of shaft axis
It is zero, it is rotated the external force torque very little of needs, thus saves significantly on the energy.After two frame helicopters are parked on frame body,
Although the gross mass of frame body and two frame helicopters is very big, total force makes it with respect to the resultant couple still very little of shaft axis
The external force torque very little needed is rotated, still saves significantly on the energy.Save significantly on the key technology and important that the energy is the present invention
The two of innovation.
After such structure, helicopter landing or helicopter is whether met to take off, frame body needs what is rotated
Angle is no more than 180 °, and it is very short to turn 180 ° of time.Soldier can shift to an earlier date man the helo, side rotating turret body, and soldier side prepares.Drop
Fall it is fast, rise it is very fast, this be the present invention key technology and important innovations three.
After such structure, can only park the naval vessels deck of a frame helicopter originally can park two frame helicopters,
Deck utilization rate is improved, fighting capacity greatly enhances.This be the present invention key technology and important innovations four.
After such structure, component is few, simple in construction, easy to maintenance, low cost.
Brief description of the drawings
The 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 that pivoted frame is parked along the helicopter of shaft axis.
Fig. 2 is the upper centre bore of one of two rotating disks, lateral opening, transitional pore relative position schematic diagram in Fig. 1.
Fig. 3 is the schematic cross section of the line A-A along Fig. 1.
Fig. 4 is rotating shaft, quiet gear, transition axis, transition gear, fluted roller shaft, side gear on the outer lateral face of one of two rotating disks
Structural representation.
Embodiment
As shown in Figure 1 to Figure 4 shown in each figure, a kind of helicopter parks pivoted frame, its body containing frame, axle bed component, motor 11, biography
Dynamic device.
As shown in Figure 1 to Figure 4 shown in each figure, this body by two 2, two pieces of rotating shafts of rotating disk 1,1 shut down 3,4 sheaves 4 of plate,
4 transition axises 8 of transition gear 7,4 of side gear 6,4 form.
As shown in figure 1, the rotating shaft 2 is elongated cylinder, its axis horizontal, its axial length is more than the length of helicopter.
As shown in Figure 1 and Figure 2, in the two rotating disks 1, a rotating disk 1 is located at right side, and another rotating disk 1 is located at left side.This
Two rotating disks 1, its axis horizontal overlap, and the distance between its interior lateral face is more than the length of helicopter.The two rotating disks 1 it
One, there are a round center hole 1a, the lateral opening 1b of two circles, two rounded transitional hole 1c, its axis and centre bore 1a thereon
Axis overlap, centre bore 1a internal diameter is equal to the external diameter of the rotating shaft 2, and the two transitional pores 1c is located at centre bore 1a respectively
With one of the two lateral opening 1b centre.The distance between one of the two lateral opening 1b axis and the centre bore 1a axis
More than the height of helicopter.Two lateral opening 1b and two lateral opening 1b on the rotating disk 1 in left side on the rotating disk 1 on right side
Specular.4 lateral opening 1b, 4 transitional pore 1c are shared on the two rotating disks 1.
As shown in Fig. 1, Fig. 3, Fig. 4, one of this 4 sheaves 4, it is made up of coaxial overall sheave disk 4a and fluted roller shaft 4b.
Sheave disk 4a, its external diameter are more than the width of helicopter, have radial level race 4c, race 4c horizontal stroke on its interior lateral face
It is equal to sheave disk 4a external diameter to length.Fluted roller shaft 4b, its axis horizontal, its axial length be more than the two rotating disks 1 it
One axial width, its external diameter are equal to or less than the internal diameter of lateral opening 1b on the two rotating disks 1.Fluted roller shaft 4b on this 4 sheaves 4
Insert respectively in one of 4 lateral opening 1b on the two rotating disks 1, the fluted roller shaft 4b on one of this 4 sheaves 4, where itself and its
Rotating disk 1 be fixed together, the outer of rotating disk 1 of its outer end where it laterally faces out stretching.One of this 4 sheaves 4
On sheave disk 4a outer lateral face and the rotating disk 1 of the relevant position where it interior lateral face it is opposed.In the two rotating disks 1,
There are two sheaves 4 on rotating disk 1 positioned at right side or the rotating disk 1 positioned at left side, 4 sheaves 4 are installed altogether on the two rotating disks 1.
As shown in Figure 1, Figure 3, one of plate 3 is shut down for this two pieces, it is horizontal rectangular plate, and its longitudinal length is less than the two turns
The distance between lateral face in disk 1, its transverse width are equal to the lateral length of race 4c on sheave 4, and its vertical thickness is equal to should
Race 4c vertical width.This two blocks shutdown plates 3, its right-hand member are respectively embedded into the two rotating disks 1 two on the rotating disk 1 on right side
Link together therewith in the race 4c of one of individual sheave 4 and snugly, its left end is respectively embedded into the two rotating disks 1
In link together therewith in the race 4c of one of two sheaves 4 corresponding on the rotating disk 1 in left side and snugly,
This two pieces horizontal axis for shutting down one of plate 3 overlap with the axis of its two sheave 4 being connected.
As Figure 1 and Figure 4, there are circular edges gear hole 6a, its axis and the heel teeth in one of this 4 side gears 6, its center
Wheel bore 6a axis overlaps, and heel teeth wheel bore 6a internal diameter is equal to the external diameter of fluted roller shaft 4b on sheave 4.This 4 side gears 6
Heel teeth wheel bore 6a, on the protruding end for the fluted roller shaft 4b for being set on the two rotating disks 1 one of 4 sheaves 4, and therewith
Snugly link together, the side gear 6 of the fluted roller shaft 4b of one of this 4 sheaves 4 outer face with suit thereon
Outer lateral face flushes.
As Figure 1 and Figure 4, the external diameter of one of this 4 transition axises 8 is equal to the internal diameter of transitional pore 1c on the two rotating disks 1.
The inner end of this 4 transition axises 8, insert respectively on the two rotating disks 1 in one of 4 transitional pore 1c, and therewith snugly
Link together.One of this 4 transition axises 8, its inner end flush with the interior lateral face of its rotating disk 1 being connected, its outer end from
The outer of its rotating disk 1 connected laterally faces out stretching.4 transition axises 8 are installed altogether on the two rotating disks 1.
As Figure 1 and Figure 4, one of this 4 transition gears 7, its axial width are equal to the axial width of side gear 6, wherein
The heart has rounded transitional gear hole 7a, and its axis overlaps with transition gear hole 7a axis, transition gear hole 7a internal diameter etc.
In or more than on the two rotating disks 1 transition axis 8 external diameter.The transition gear hole 7a of this 4 transition gears 7, is set in this
On two rotating disks 1 on the protruding end of one of 4 transition axises 8, and fixed thereto link together.This 4 transition axises 8 it
One, its outer face flushes with being set with the outer lateral face of transition gear 7 thereon.One of this 4 transition gears 7 turn where it
Side gear 6 on disk 1 with adjacent same radial direction engages.
As shown in figure 1, the axle bed component 9, two quiet gears 5 containing two axle beds.
As shown in figure 1, the two axle beds 9 are respectively positioned at the outside of one of the two rotating disks 1.One of the two axle beds 9, its
Vertical height is less than the external diameter of rotating disk 1 but nearby has circular shaft bore 9a more than the radius of rotating disk 1, its upper end, axle bed hole 9a
Internal diameter be equal to or more than the rotating shaft 2 external diameter.The axis of axle bed hole 9a axis and the two rotating disks 1 on the two axle beds 9
The lower surface of one of horizontal registration, the two axle beds 9 and the naval vessels deck 15 of relevant position snugly link together.
As Figure 1 and Figure 4, one of the two quiet gears 5, it is annular, and its internal diameter is more than the external diameter of the rotating shaft 2, its
External diameter is equal to the external diameter of side gear 6 on rotating disk 1, and the number of teeth on its external peripheral surface is equal on the external peripheral surface of side gear 6
The number of teeth, its axial width are more than the axial width of the side gear 6.The two quiet gears 5, its axis respectively with the two axle beds 9
One of upper axle bed hole 9a axis overlap, its outer lateral face respectively the interior lateral face with one of the two axle beds 9 with tight fit side
Formula links together.
As Figure 1 and Figure 4, the rotating shaft 2, it inserts the centre bore 1a of the two rotating disks 1 and the two axle beds 9 axle bed
In the 9a of hole, it snugly links together with the two rotating disks 1, and it is fixed together with the two axle beds 9, its
Horizontal axis overlaps with the axis of axle bed hole 9a on the axis or the two axle beds 9 of the two rotating disks 1, and its one end is from Same Name of Ends
The outer of axle bed 9 laterally faces out stretching.The rotating disk 1 of one of the two quiet gears 5, its interior lateral face and relevant position it is outer lateral
Face is opposed but does not contact, and two transition gears 7 on its adjacent rotating disk 1 with surrounding engage.
As shown in figure 1, there is horizontal power output shaft 12 on the motor 11.
As shown in figure 1, the transmission device is made up of big sprocket wheel 10, minor sprocket 13, chain 14.
As shown in figure 1, the big sprocket wheel 10, there is circular big sprocket wheel hole 10a at its center, and its axis is with big sprocket wheel hole 10a's
Axis overlaps, and big sprocket wheel hole 10a internal diameter is equal to the external diameter of the rotating shaft 2.The big sprocket wheel hole 10a of the big sprocket wheel 10 is sleeved on this
Rotating shaft 2 snugly links together therewith from the external part of 9 outer lateral face of axle bed.
As shown in figure 1, the minor sprocket 13, it is located on same perpendicular with the big sprocket wheel 10, and it is big that its external diameter is less than this
The external diameter of sprocket wheel 10, it is snugly on the power output shaft 12 of the motor 11.
As shown in figure 1, the chain 14 is sleeved on the big sprocket wheel 10 and the minor sprocket 13.
As Figure 1 and Figure 4, the motor 11 is powered after rotation, passes through the minor sprocket 13 and the chain 14 drives the big chain
Wheel 10 rotates, rotating shaft 2 and two synchronous rotaries of rotating disk 1 on the big sprocket wheel 10 driving this body, so that on this body
Two pieces of shutdown one of plates 3 Circularly liftables in rotation.At the same time, the two transition teeth rotated with one of the two rotating disks 1
The effect for the quiet gear 5 that wheel 7 is engaged with is forced to rotate, and the two transition gears 7 drive two sides being engaged with respectively
Gear 6 rotates, and the two side gears 6 drive two sheaves 4 being attached thereto to rotate respectively again.4 on the two rotating disks 1
Sheave 4 drives two pieces to shut down plate 3 relative to the rotation of the two opposite directions of rotating disk 1 again, and this two pieces are shut down the two relative turns of one of plate 3
The angle that disk 1 reversely turns over is equal to the two rotating disks 1 with respect to the angle that ground turns over, so as to which this two pieces are shut down one of plates 3 all the time
Keep level state.
The application method that the helicopter parks pivoted frame is such：
First, helicopter is parked：
As shown in figure 1, rotating this body, shutdown plate 3 vacant thereon is gone into extreme higher position, then makes this body
Remains stationary, helicopter are dropped on the shutdown plate 3.
Second, helicopter takes off：
As shown in figure 1, rotating this body, the shutdown plate 3 for parking helicopter thereon is gone into extreme higher position, then made
This body remains stationary, helicopter take off from the shutdown plate 3.
Embodiments of the present invention are explained in detail above in conjunction with accompanying drawing.The present invention is not limited to above-mentioned embodiment party
Formula, can also be before present inventive concept not be departed from art those of ordinary skill's possessed knowledge
Put that various changes can be made, as naval vessels deck man the helo shut down region area it is larger when, increase helicopter parks pivoted frame
Volume, increase component, make it to park more multiple helicopters.The various change made on the premise of present inventive concept is not departed from,
Still fall within the scope of the present invention.
Claims (2)
1. a kind of helicopter parks pivoted frame, it is characterised in that：
The helicopter parks pivoted frame body containing frame, axle bed component, motor (11), transmission device；
The frame body by two rotating disks (1), 1 rotating shaft (2), two pieces shut down plates (3), 4 sheaves (4), 4 side gears (6),
4 transition gears (7), 4 transition axis (8) compositions；
The rotating shaft (2) is elongated cylinder, its axis horizontal, and its axial length is more than the length of helicopter；
In the two rotating disks (1), a rotating disk (1) is located at right side, and another rotating disk (1) is located at left side；The two rotating disks (1),
Its axis horizontal overlaps, and the distance between its interior lateral face is more than the length of helicopter；One of the two rotating disks (1), have thereon
One round center hole (1a), two circles lateral opening (1b), two rounded transitional holes (1c), its axis and the centre bore (1a)
Axis overlap, the internal diameter of the centre bore (1a) is equal to the external diameter of the rotating shaft (2), and the two transitional pores (1c) are located at respectively
One of the centre bore (1a) and the two lateral opening (1b) centre；The axis of one of the two lateral opening (1b) and the center
The distance between the axis in hole (1a) is more than the height of helicopter；Two lateral opening (1b) and position on the rotating disk (1) on right side
In two lateral opening (1b) speculars on the rotating disk (1) in left side；4 lateral opening (1b), 4 mistakes are shared on the two rotating disks (1)
Cross hole (1c)；
One of this 4 sheaves (4), it is made up of coaxial overall sheave disk (4a) and fluted roller shaft (4b)；The sheave disk (4a), its
External diameter is more than the width of helicopter, has radial level race (4c), the lateral length of the race (4c) etc. on its interior lateral face
In the external diameter of the sheave disk (4a)；The fluted roller shaft (4b), its axis horizontal, its axial length are more than the two rotating disks (1)
One of axial width, its external diameter be equal to or less than the two rotating disks (1) on lateral opening (1b) internal diameter；On this 4 sheaves (4)
Fluted roller shaft (4b) inserts in one of 4 lateral opening (1b) on the two rotating disks (1) respectively, the sheave on one of this 4 sheaves (4)
Axle (4b), it is fixed together with the rotating disk (1) where it, rotating disk (1) of its outer end where it is outer laterally towards
Overhang；The outer lateral face of sheave disk (4a) on one of this 4 sheaves (4) and the rotating disk (1) of the relevant position where it
Interior lateral face is opposed；In the two rotating disks (1), there are two sheaves on the rotating disk (1) positioned at right side or the rotating disk (1) positioned at left side
(4) 4 sheaves (4), are installed altogether on the two rotating disks (1)；
This two pieces are shut down plate one of (3), and it be horizontal rectangular plate, its longitudinal length less than the two rotating disk (1) interior lateral faces it
Between distance, its transverse width is equal to the lateral length of race (4c) on sheave (4), and its vertical thickness is equal to the race (4c)
Vertical width；This two pieces are shut down plate (3), and its right-hand member is respectively embedded into the two rotating disks (1) two on the rotating disk (1) on right side
Link together therewith in the race (4c) of one of individual sheave (4) and snugly, its left end is respectively embedded into the two turns
In disk (1) on the rotating disk (1) in left side corresponding to one of two sheaves (4) race (4c) in and therewith snugly
Link together, this two pieces horizontal axis for shutting down one of plate (3) overlap with the axis of its two sheave (4) being connected；
There are circular edges gear hole (6a), its axis and the axle of the heel teeth wheel bore (6a) in one of this 4 side gears (6), its center
Line overlaps, and the internal diameter of the heel teeth wheel bore (6a) is equal to the external diameter of fluted roller shaft (4b) on sheave (4)；The side of this 4 side gears (6)
Gear hole (6a), on the protruding end for the fluted roller shaft (4b) for being set in one of upper 4 sheaves (4) of the two rotating disks (1),
And snugly link together therewith, the outer face of the fluted roller shaft (4b) of one of this 4 sheaves (4) is with being set with thereon
The outer lateral face of side gear (6) flushes；
The external diameter of one of this 4 transition axises (8) is equal to the internal diameter of transitional pore (1c) on the two rotating disks (1)；This 4 transition axises
(8) inner end, insert in one of upper 4 transitional pores (1c) of the two rotating disks (1), and be snugly connected to therewith respectively
Together；One of this 4 transition axises (8), the interior lateral face for the rotating disk (1) that its inner end is connected with it flush, its outer end from its
The outer of the rotating disk (1) connected laterally faces out stretching；4 transition axises (8) are installed altogether on the two rotating disks (1)；
One of this 4 transition gears (7), its axial width are equal to the axial width of side gear (6), and there is rounded transitional tooth at its center
Wheel bore (7a), its axis overlap with the axis of the transition gear hole (7a), the internal diameter of the transition gear hole (7a) be equal to or
More than the external diameter of transition axis (8) on the two rotating disks (1)；The transition gear hole (7a) of this 4 transition gears (7), is set with
On the protruding end of one of upper 4 transition axises (8) of the two rotating disks (1), and fixed thereto link together；This 4 mistakes
One of axle (8) is crossed, its outer face flushes with being set with the outer lateral face of transition gear (7) thereon；This 4 transition gears (7) it
Engaged on one rotating disk (1) where it with the side gear (6) of adjacent same radial direction；
The axle bed component is containing two axle beds (9), two quiet gears (5)；
The two axle beds (9) are respectively positioned at the outside of one of the two rotating disks (1)；One of the two axle beds (9), its vertical height
Nearby there are circular shaft bore (9a), the axle bed hole in external diameter less than rotating disk (1) but the radius more than rotating disk (1), its upper end
The internal diameter of (9a) is equal to or more than the external diameter of the rotating shaft (2)；On the two axle beds (9) axis in axle bed hole (9a) and the two
The axis horizontal of rotating disk (1) overlaps, and the lower surface of one of the two axle beds (9) and the naval vessels deck (15) of relevant position are with close-fitting
Conjunction mode links together；
One of the two quiet gears (5), it is annular, and its internal diameter is more than the external diameter of the rotating shaft (2), and its external diameter is equal to rotating disk
(1) external diameter of side gear (6) on, the number of teeth on its external peripheral surface are equal to the number of teeth on the side gear (6) external peripheral surface,
Its axial width is more than the axial width of the side gear (6)；The two quiet gears (5), its axis respectively with the two axle beds
One of (9) axis of upper axle bed hole (9a) overlaps, its outer lateral face respectively the interior lateral face with one of the two axle beds (9) with tight
Fit system links together；
The rotating shaft (2), it is inserted in the axle bed hole (9a) of the centre bore (1a) of the two rotating disks (1) and the two axle beds (9),
It snugly links together with the two rotating disks (1), and it is fixed together with the two axle beds (9), its water
Flat axis overlaps with the axis in axle bed hole (9a) on the axis or the two axle beds (9) of the two rotating disks (1), and its one end is from of the same name
The outer of the axle bed (9) at end laterally faces out stretching；One of the two quiet gears (5), the rotating disk of its interior lateral face and relevant position
(1) outer lateral face is opposed but does not contact, and two transition gears (7) on its adjacent rotating disk (1) with surrounding are engaged；
There is horizontal power output shaft (12) on the motor (11)；
The transmission device is made up of big sprocket wheel (10), minor sprocket (13), chain (14)；
There are circular big sprocket wheel hole (10a), its axis and the axis of the big sprocket wheel hole (10a) in the big sprocket wheel (10), its center
Overlap, the internal diameter of the big sprocket wheel hole (10a) is equal to the external diameter of the rotating shaft (2)；The big sprocket wheel hole of the big sprocket wheel (10)
(10a) is sleeved on the rotating shaft (2) from the external part of axle bed (9) outer lateral face, and is snugly connected to one therewith
Rise；
The minor sprocket (13), it is located on same perpendicular with the big sprocket wheel (10), and its external diameter is less than the big sprocket wheel
(10) external diameter, it is snugly on the power output shaft (12) of the motor (11)；
The chain (14) is sleeved in the big sprocket wheel (10) and the minor sprocket (13)；
The motor (11) is powered after rotation, passes through the minor sprocket (13) and the chain (14) drives the big sprocket wheel
(10) rotating, the big sprocket wheel (10) drives rotating shaft (2) and two rotating disk (1) synchronous rotaries on the frame body, so that
Two pieces on the frame body are shut down one of plate (3) Circularly liftable in rotation；At the same time, with one of the two rotating disks (1)
The effect for the quiet gear (5) that two transition gears (7) rotated are engaged with is forced to rotate, the two transition gears (7) point
Do not drive two side gears (6) being engaged with to rotate, the two side gears (6) and drive two sheaves being attached thereto respectively
(4) rotate；4 sheaves (4) on the two rotating disks (1) drive two pieces to shut down plate (3) with respect to the two rotating disk (1) opposite directions again
Rotation, shut down the angle that the two relative rotating disks (1) of one of plate (3) reversely turn over for this two pieces and be equal to the two rotating disks (1) relatively
The angle that ground turns over, so as to which one of this two pieces shutdown plates (3) remain horizontality.
2. a kind of usage right requires the method that 1 helicopter parks pivoted frame：
First, helicopter is parked：
The frame body is rotated, shutdown plate (3) vacant thereon is gone into extreme higher position, the frame body is kept quiet
Only, helicopter is dropped on the shutdown plate (3)；
Second, helicopter takes off：
The frame body is rotated, the shutdown plate (3) for parking helicopter thereon is gone into extreme higher position, then makes the frame body
Remains stationary, helicopter take off from the shutdown plate (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711110893.5A CN107826263B (en) | 2017-11-01 | 2017-11-01 | Helicopter parking rotating stand |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711110893.5A CN107826263B (en) | 2017-11-01 | 2017-11-01 | Helicopter parking rotating stand |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107826263A true CN107826263A (en) | 2018-03-23 |
| CN107826263B CN107826263B (en) | 2021-02-05 |
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ID=61655158
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711110893.5A Active CN107826263B (en) | 2017-11-01 | 2017-11-01 | Helicopter parking rotating stand |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107826263B (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS62222909A (en) * | 1986-03-24 | 1987-09-30 | Takashi Suzuki | Solid storing device |
| CN1240865A (en) * | 1998-07-03 | 2000-01-12 | 王元良 | Rotating table type garage for cars |
| US20040256519A1 (en) * | 2003-03-12 | 2004-12-23 | Ellis Stephen C. | System for recovery of aerial vehicles |
| CN102758546A (en) * | 2012-07-09 | 2012-10-31 | 中国轻工建设工程有限公司 | Equipment for storing automobiles |
| CN205422078U (en) * | 2016-03-16 | 2016-08-03 | 广州城建职业学院 | Rotary type three -dimensional garage |
| CN106586019A (en) * | 2016-12-12 | 2017-04-26 | 李新亚 | Long-cylinder parking rack for aircrafts on aircraft carrier |
-
2017
- 2017-11-01 CN CN201711110893.5A patent/CN107826263B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS62222909A (en) * | 1986-03-24 | 1987-09-30 | Takashi Suzuki | Solid storing device |
| CN1240865A (en) * | 1998-07-03 | 2000-01-12 | 王元良 | Rotating table type garage for cars |
| US20040256519A1 (en) * | 2003-03-12 | 2004-12-23 | Ellis Stephen C. | System for recovery of aerial vehicles |
| CN102758546A (en) * | 2012-07-09 | 2012-10-31 | 中国轻工建设工程有限公司 | Equipment for storing automobiles |
| CN205422078U (en) * | 2016-03-16 | 2016-08-03 | 广州城建职业学院 | Rotary type three -dimensional garage |
| CN106586019A (en) * | 2016-12-12 | 2017-04-26 | 李新亚 | Long-cylinder parking rack for aircrafts on aircraft carrier |
Also Published As
| Publication number | Publication date |
|---|---|
| CN107826263B (en) | 2021-02-05 |
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Effective date of registration: 20231115 Address after: 1337, 13th Floor, Building 2, No. 38 Kechuang 5th Street, Beijing Economic and Technological Development Zone, Daxing District, Beijing, 102600 (Yizhuang Cluster, High end Industrial Zone, Beijing Pilot Free Trade Zone) Patentee after: Beifei Blueprint (Beijing) Aeronautical Engineering Technology Research Institute Co.,Ltd. Address before: No.50 Xicheng Road, Yanjiang administrative village, Renmin Town, Zhongshan City, Guangdong Province 528400 Patentee before: Lin Guanghua |
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Effective date of registration: 20240315 Address after: 335400 Fazhan Road, economic development zone, Guixi City, Yingtan City, Jiangxi Province intersects National Highway 320 (in Guixi science and Technology Innovation Center) Patentee after: Beifei blueprints Aviation Technology Co.,Ltd. Guo jiahuodiqu after: Zhong Guo Address before: 1337, 13th Floor, Building 2, No. 38 Kechuang 5th Street, Beijing Economic and Technological Development Zone, Daxing District, Beijing, 102600 (Yizhuang Cluster, High end Industrial Zone, Beijing Pilot Free Trade Zone) Patentee before: Beifei Blueprint (Beijing) Aeronautical Engineering Technology Research Institute Co.,Ltd. Guo jiahuodiqu before: Zhong Guo |