CN108502727A - Play perpendicular device and hoisting machine - Google Patents

Play perpendicular device and hoisting machine Download PDF

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Publication number
CN108502727A
CN108502727A CN201810264152.0A CN201810264152A CN108502727A CN 108502727 A CN108502727 A CN 108502727A CN 201810264152 A CN201810264152 A CN 201810264152A CN 108502727 A CN108502727 A CN 108502727A
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CN
China
Prior art keywords
support portion
oil cylinder
main part
support
perpendicular device
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CN201810264152.0A
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Chinese (zh)
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CN108502727B (en
Inventor
王永刚
吴雪
李永俊
韩召洋
戴政
康永来
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Lanjian Spaceflight Technology Co ltd
Original Assignee
Beijing Blue Arrow Interspace Technology Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Beijing Blue Arrow Interspace Technology Ltd filed Critical Beijing Blue Arrow Interspace Technology Ltd
Priority to CN202010798437.XA priority Critical patent/CN112061980B/en
Priority to CN202010798438.4A priority patent/CN112062061B/en
Priority to CN201810264152.0A priority patent/CN108502727B/en
Publication of CN108502727A publication Critical patent/CN108502727A/en
Application granted granted Critical
Publication of CN108502727B publication Critical patent/CN108502727B/en
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66FHOISTING, LIFTING, HAULING OR PUSHING, NOT OTHERWISE PROVIDED FOR, e.g. DEVICES WHICH APPLY A LIFTING OR PUSHING FORCE DIRECTLY TO THE SURFACE OF A LOAD
    • B66F11/00Lifting devices specially adapted for particular uses not otherwise provided for
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B1/00Installations or systems with accumulators; Supply reservoir or sump assemblies
    • F15B1/02Installations or systems with accumulators
    • F15B1/024Installations or systems with accumulators used as a supplementary power source, e.g. to store energy in idle periods to balance pump load
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B11/00Servomotor systems without provision for follow-up action; Circuits therefor
    • F15B11/16Servomotor systems without provision for follow-up action; Circuits therefor with two or more servomotors
    • F15B11/161Servomotor systems without provision for follow-up action; Circuits therefor with two or more servomotors with sensing of servomotor demand or load
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00Circuits for servomotor systems
    • F15B2211/70Output members, e.g. hydraulic motors or cylinders or control therefor
    • F15B2211/705Output members, e.g. hydraulic motors or cylinders or control therefor characterised by the type of output members or actuators
    • F15B2211/7051Linear output members
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00Circuits for servomotor systems
    • F15B2211/70Output members, e.g. hydraulic motors or cylinders or control therefor
    • F15B2211/71Multiple output members, e.g. multiple hydraulic motors or cylinders
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15BSYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00Circuits for servomotor systems
    • F15B2211/70Output members, e.g. hydraulic motors or cylinders or control therefor
    • F15B2211/78Control of multiple output members
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41FAPPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
    • F41F3/00Rocket or torpedo launchers
    • F41F3/04Rocket or torpedo launchers for rockets

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Engineering & Computer Science (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Geology (AREA)
  • Structural Engineering (AREA)
  • Jib Cranes (AREA)

Abstract

The invention discloses one kind playing perpendicular device and hoisting machine.Playing perpendicular device includes:Main part, the first support portion set on the main part, at least two second support portions, and connect the regulating mechanism of at least two second support portion;Wherein, the main part includes reciprocal first side and the second side in a first direction;First support portion and at least two second support portion are set to first side;Described at least two second support portions are arranged along the second direction of the main part length, and first support portion and at least two second support portion are used to support object to be supported;The variation for the load that the regulating mechanism is used to be applied by object to be supported according to described at least two second support portions dynamically adjusts the load distribution of described at least two second support portions.This props perpendicular device and hoisting machine, can be changed according to supporter stressed skin, dynamically adjust load distribution, to greatly improve the safety of perpendicular process product.

Description

Play perpendicular device and hoisting machine
Technical field
The present invention relates to products to play perpendicular technical field, and in particular to one kind playing perpendicular device and hoisting machine.
Background technology
Since carrier rocket or the product having analogous shape have larger slenderness ratio, during playing perpendicular, axis To pressure change it is larger.It is this have more harsh, i.e. shell is required usually compared with the shell of the product of high-fineness ratio face pressure allowable Body stress is no more than face pressure value allowable.
The carrier rocket of same type integrally plays the perpendicular basic perpendicular pattern using 2 points of main bearings at present, is unsatisfactory for shell Force request.When using 3 points or more of support modes, the pattern of two main supports plus several Auxiliary supports is mostly used.For It prevents during playing perpendicular, rocket envelope is damaged since axially loaded is uneven, usually rigidity by having increased vertical arm It is made up, to increase the quality of vertical arm.
There is an urgent need for designing a kind of new vertical arm, to meet this perpendicular demand with the product compared with high-fineness ratio structure.
Invention content
For above-mentioned technical problem in the related technology, the present invention proposes a kind of perpendicular device and hoisting machine.This props perpendicular Device can change according to supporter stressed skin, dynamically adjust load distribution, to greatly improve perpendicular process production The safety of product.
One aspect of the present invention provides a kind of perpendicular device.The perpendicular device of this includes:Main part is set to the master First support portion in body portion, at least two second support portions, and connect the adjusting machine of at least two second support portion Structure;Wherein, the main part includes reciprocal first side and the second side in a first direction;First support portion and Described at least two second support portions are set to first side;Described at least two second support portions are along the main part length Second direction setting, and first support portion and at least two second support portion are used to support object to be supported;It is described The variation for the load that regulating mechanism is used to be applied by object to be supported according to described at least two second support portions is dynamically adjusted The load distribution of described at least two second support portions.
In one embodiment, the regulating mechanism is hydraulic system or baric systerm.
In one embodiment, the regulating mechanism is hydraulic system;The wherein described hydraulic system includes the first hydraulic oil Cylinder and the second hydraulic cylinder;First hydraulic cylinder one end connects one of them described second support portion, and the other end connects First valve;One end of second hydraulic cylinder connects another second support portion, and other end connection described first Valve;The positive chamber of first oil cylinder and second oil cylinder is by positive chamber pipeline connection, to form positive chamber isobaric system, institute The anti-chamber of the first oil cylinder and second oil cylinder is stated by anti-chamber pipeline connection, to form anti-chamber isobaric system;First valve Oil mass and oil level of the door for adjusting first oil cylinder and second oil cylinder.
In one embodiment, playing perpendicular device includes:Multiple second supports set on first side of the main part Portion, the hydraulic system include multiple multiple oil cylinders for corresponding the multiple second support portion respectively;It is wherein the multiple Second support portion is separately connected one end of corresponding oil cylinder, and the other end of oil cylinder is connected to the first valve;The multiple oil cylinder Positive chamber by positive chamber pipeline connection, to form positive chamber isobaric system, and anti-chamber is by anti-chamber pipeline connection, to form anti-chamber Isobaric system;First valve is used to adjust the oil mass and oil level of first oil cylinder and second oil cylinder.
In one embodiment, in the second direction along the main part length, close to first support portion The second support portion corresponding to oil cylinder cross-sectional area be less than or equal to far from first support portion the second support portion The cross-sectional area of corresponding oil cylinder.
In one embodiment, it in the second direction along the main part length, is supported from close to described first Cross-sectional area from portion to the corresponding oil cylinder of second support portion set gradually far from first support portion according to It is secondary incremental.
In one embodiment, the positive chamber piping connection accumulator, the accumulator is for compensating the hydraulic system Liquid is revealed.
In one embodiment, first valve is three-position four-way valve.
In one embodiment, first support portion can be rotatably set in first side of the main part, and Rotation axis is consistent with the width direction of the main part.
In one embodiment, second support portion is 3-12, and second support portion is set to described first The homonymy of support part in this second direction.
In one embodiment, second support portion is coaxially disposed each other, and coaxial with first support portion Setting.
Another aspect of the present invention provides a kind of hoisting machine, including plays perpendicular device as described above.
The present invention's plays perpendicular device and hoisting machine, by the way that the second support of at least two second support portions and connection is arranged The regulating mechanism in portion, can according to rise it is perpendicular during product casing load change, dynamically adjust played hanging object first The load distribution of support part and the second support portion, to improve the reliability and security that perpendicular device plays the products such as perpendicular rocket.
In reading specific implementation mode and after checking attached drawing, those skilled in the art will recognize that other Feature and advantage.
Description of the drawings
It in order to more clearly explain the embodiment of the invention or the technical proposal in the existing technology, below will be in embodiment Required attached drawing is briefly described, it should be apparent that, the accompanying drawings in the following description is only some realities of the present invention Example is applied, it for those of ordinary skill in the art, without creative efforts, can also be attached according to these Figure obtains other attached drawings.
Fig. 1 is the structural schematic diagram of according to the ... of the embodiment of the present invention perpendicular device.
Fig. 2 is the schematic diagram according to the regulating mechanism of the embodiment of the present invention.
Fig. 3 a and 3b are regulating mechanism schematic diagrames according to the ... of the embodiment of the present invention.
Fig. 4 a are the schematic diagram for playing perpendicular device of the embodiment of the present invention.
The schematic diagram for the hydraulic system for playing perpendicular device that Fig. 4 b are corresponding diagram 4a.
Fig. 5 is the hydraulic schematic that the embodiment of the present invention includes accumulator.
Fig. 6 is the schematic diagram that the embodiment of the present invention includes elevating mechanism and the stent car of support construction.
Fig. 7 is the direction of motion schematic diagram of the embodiment of the present invention risen when perpendicular device plays perpendicular product.
Specific implementation mode
Technical solution to further illustrate the present invention below with reference to the accompanying drawings and specific embodiments.Such as " under Face ", " lower section ", " ... under ", " low ", " top ", " ... on ", the spatial relationship term of "high" etc. for keeping description convenient, To explain positioning of the element relative to second element, indicate in addition to from shown in figure those be orientated different orientations with Outside, these terms are intended to cover the different orientation of device.In addition, for example " element is in another element up/down " can be with table Show that two elements are in direct contact, can also indicate that also there are other elements between two elements.In addition, such as " first ", " the Two " etc. term is also used for describing each element, area, part etc., and should not be regarded as limiting.Similar term is describing Similar element is indicated in the whole text.
As previously mentioned, having using the perpendicular carrier rocket of vertical arm etc. that rises with 3 points and 3 points or more of support portion Compared with high-fineness ratio product when, play a vertical arm and be typically provided with two main bearings plus several aiding supports, to avoid due to using only having Have 2 points of main supports rise vertical arm may caused by damage to such as rocket envelope.For example, hydraulic pressure may be used in aiding support Or form of springs, each Auxiliary support is independent of one another, i.e., the load of rocket body can not carry out shell without control at Auxiliary support Dignity is pressed rationed.That is, during product plays perpendicular, the pattern of this main support cooperation Auxiliary support exists The statically indeterminate problem of load, and this load static indeterminacy situation can be coupled with the stiffness variation for playing vertical arm, so as to cause each Supporting point can not be quantified in the load design stage and be calculated.For example, in products such as rockets during playing perpendicular, it usually can be due to rigid Degree defective coupling causes local overload, and the damage of shell may be caused when serious.
To solve the above-mentioned problems, traditional scheme is typically by having improved the rigid of vertical arm (for example, large span overarm arm) The mode of degree reduces the load deflections during rocket body erects.On the one hand, it is this by way of the rigidity for having improved vertical arm without Method thoroughly eliminates the load deflections of rocket body axial direction;On the other hand usually made the quality of vertical arm excessive, to cause system excessively It is heavy.For example, this method eliminated rocket body by way of having improved vertical arm rigidity and play the load deflections of perpendicular process, it can be with The quality of vertical arm is led to far more than the quality of perpendicular target rocket is played.
One aspect of the present invention provides a kind of perpendicular device.Referring to Fig. 1, the perpendicular device of this includes:Main part 1 is set In the first support portion 2, at least two second support portions 3 of main part 1, and the adjusting of at least two second support portions 3 of connection Mechanism 4.Wherein, main part 1 includes in a first direction reciprocal first side and the second side on S1;First support portion, 2 He At least two second support portions 3 are set to the first side.At least two second support portions 3 are set along the second direction S2 of 1 length of main part It sets, and the first support portion 2 and at least two second support portions 3 are used to support object to be supported.Regulating mechanism 4 is used for according at least The variation for the load that two the second support portions 3 are applied by object to be supported dynamically adjusts at least two second support portions 3 Load distribution.Provided in an embodiment of the present invention perpendicular device, by the way that adjustable floating support point (the second support portion) is arranged, The load distribution of rocket body in axial direction can be dynamically adjusted according to the load bearing variation of rocket body of such as rocket, to Improve the safety that rocket plays perpendicular process.
For example, main part 1 can be string configuration, such as be used to support with compared with high-fineness ratio product (such as Rocket).For example, the length of main part 1 can be roughly equal with the length of product to be supported.
For example, the first support portion 2 is used to rise perpendicular approximately fixed by products such as rockets, avoid the products such as rocket in fire It is moved on the axially and radially direction of arrow.For example, as shown in Figure 1, the first support portion 2 can be to be fixed at main part The annular fixing member of side.For example, annular fixing member can be can opening and closing structure.It is supported playing perpendicular device placement rocket etc. Before object, annular fixing member circumferentially can be opened along it first, in the ring being placed in the supported objects such as rocket after opening After shape fixing piece, can by annular fixing member along its circumferential closure (at this point, the circumferential direction of the inside of annular fixing member and rocket Contact, rocket etc. is blocked from outer circle circumferential direction), to limit rocket along annular fixing member move radially and rocket It is moved axially with respect to main part.In addition, annular fixing member can be diameter adjustable structure, to be beaten rocket to be placed in It, can be by reducing the diameter of annular fixing member, to preferably limit the supported objects such as rocket after annular fixing member after opening It is formed on main part.
For example, as shown in Figure 1, multiple second support portions 3 for example can be curved support structure, these second supports The initial position in portion 3 can be for example coaxially disposed with the first support portion 1.As previously mentioned, the of the first side setting of main part 1 Two support portions 3 after the load change applied by supported object, in a first direction S1 size (the second support portion it is separate Distance of the first side of main part to the first side of main part) it is variable, so as to automatically regulate supported object along main part 1 The load distribution of length direction.Regulating mechanism 4 can for example connect at least two second support portion 3 simultaneously, at two When the load of second support portion 3 changes, by dynamically adjusting height (of second support portion 3 in a first direction on S1 Distance of two support portions far from the first side of main part to the first side of main part), the load that two the second support portions 3 of adjustment are born Lotus is distributed.
For example, on the length direction S2 of main part 1, multiple second support portions 3 can be set to the first support portion 2 Homonymy can also be arranged in the both sides of the first support portion 2, and belong to protection scope of the present invention.Preferably, of the invention Embodiment is explained in such a way that multiple second support portions 3 are arranged in the homonymy of the first support portion 2.
In addition, in the case where the first support portion 2 is annular fixing member, internal diameter can be slightly larger than the outer of supported object Diameter, and felt can be arranged in its internal diameter, when being raised and lowered to perpendicular in rocket etc. and each second support portion 3, the quilts such as rocket Supporter can slightly be swung in annular fixing member, avoided it from being waken up fixing piece and applied load
In one embodiment, the regulating mechanism 4 is hydraulic system or baric systerm.Referring to Fig. 2, for example, adjusting In the case that mechanism 4 is hydraulic system, regulating mechanism 4 can be oil cylinder and piston cylinder operator.For example, multiple oil cylinders 41 can be with It is corresponded with multiple second support portions 3, and these oil cylinders 41 are located at the side of piston 42 and communicate with each other, positioned at piston 42 The other side communicates with each other.The intracavitary pressure of the side to be communicated with each other due to the property of gas, these oil cylinders 41 is equal.Different Load can be carried out when load at second supporting point 3 changes, between the oil cylinder 41 to communicate with each other to adjust again, to reach New equilibrium state.In the case, by precalculating perpendicular load and change in the process in an axial direction is being played such as rocket Change, can realize that such as rocket, load is along axis during playing perpendicular by designing the cross-sectional area of the oil cylinder of corresponding position It is distributed to the dynamic quantitative in direction.
In one embodiment, the regulating mechanism is hydraulic system.Referring to Fig. 3 a and 3b, it includes at least to play perpendicular device Two the second support portions 3.For example, on the length direction S2 of main part 1, two the second support portions 3 are located at the first support portion 2 Homonymy.Hydraulic system includes the first hydraulic cylinder 43 and the second hydraulic cylinder 44.First hydraulic cylinder, 43 one end 45 connects One of them second support portion, and the other end 46 connects the first valve 5.For example, the second support of piston rod connection of the one end 45 Portion 3, so as in the second 3 stress of support portion, the second support portion 3 is moved with movement of the piston rod in oil cylinder.Similarly, One end of second hydraulic cylinder 44 connects another the second support portion 3, and the other end connects the first valve 5.First oil cylinder 43 It is connected to by positive lumen road 48 with the positive chamber (positive chamber refers to the chamber being connect with oil inlet pipe) of the second oil cylinder 44, to form positive chamber The anti-chamber (chamber being connect with oil outlet pipe) of isobaric system, the first oil cylinder 43 and the second oil cylinder 44 is connected to by anti-lumen road 49, To form anti-chamber isobaric system.Oil mass and oil level of first valve 5 for example for adjusting the first oil cylinder 43 and the second oil cylinder 44 Deng.Rising in supported object may be implemented by two oil cylinders of corresponding at least two second support portions in the embodiment of the present invention During perpendicular, the load change according to supported object two the second support portion positions dynamically adjusts two the second support portions Height in a first direction, so as to adjust the load distribution of supported object in an axial direction.
Referring to Fig. 4 a and 4b, in one embodiment, playing perpendicular device includes:Multiple set on the first side of main part Two support portions 3, i.e. the second support portion 31,32,33,34, hydraulic system includes multiple corresponding multiple second support portions respectively 31,32,33,34 multiple oil cylinders 411,412,413,414.Plurality of second support portion 31,32,33,34 is separately connected One end of corresponding oil cylinder 411,412,413,414, and the other end of oil cylinder 411,412,413,414 is connected to the first valve 5.As previously shown, the side of the piston rod of multiple oil cylinders is separately connected corresponding second support portion, when so as to piston rod movement, Corresponding second support portion can be driven to be moved on second direction S2.The multiple oil cylinder 411,412,413,414 is just Chamber is connected to by positive lumen road 48, and to form positive chamber isobaric system, and anti-chamber is connected to by anti-lumen road 49, to form anti-chamber Isobaric system.First valve 5 is used to adjust the oil mass and oil level of oil cylinder 411,412,413,414.The embodiment of the present invention passes through The oil cylinder 411 of the second support portion of multiple correspondences 31,32,33,34 is set, 412,413,414, it can be supported according to multiple second 31,32,33,34 place of portion is loaded, dynamically adjusts load distribution of the object to be supported on shaft body portion length direction, really Perpendicular process safety is protected.
In the above-described embodiments, for example, second support portion 3 is 3-12, and in the second party of 1 length of main part To on S2, the second support portion 3 is set to the homonymy of the first support portion 2.The embodiment of the present invention is by making the second support portion The homonymy of one support portion is arranged, and can simplify the structure of hydraulic system, improves the reliability of system work.
In this embodiment, when the rigidity of main part for playing perpendicular device changes, the liquid of 4 tandem of hydraulic system Press bearing hydraulic oil cylinder 411, hydraulic cylinder 412, hydraulic cylinder 413, hydraulic cylinder 414 on positive lumen road 48, anti-lumen road 49 Under the fluid pressure line equipressure effect ganged up, the altitude compensation system of level pressure random length is formed.Play 1 pressure-bearing of main part of perpendicular device Big 31 position of the second support portion of deformation, 411 elongation of hydraulic cylinder is big, conversely, the second support portion 34 that bearing strain is small Position, the elongation of hydraulic cylinder 414 is small.The stroke difference adaptive equalization that the embodiment of the present invention passes through each oil cylinder The height error that vertical arm stiffness variation is formed is played, and then meets rocket body supporting structure (including the first support portion and second several Support part) arc surface concentricity demand.In addition, the embodiment of the present invention is connected to by fluid path, the positive chamber of each hydraulic cylinder, Anti- cavity pressure difference is equal, and after the geometric parameters such as oil cylinder piston area, rod areas are set, each second support portion (floats Fulcrum) load can controllably distribute.
With continued reference to Fig. 4 b, in this embodiment, in one embodiment, the first valve 5 for example can be 3-position 4-way Valve.For example, before work, the three-position four-way valve 5 of hydraulic system 4 is in left position on-state, and the oil sources being attached thereto starts, from And it is the positive chamber fuel feeding of hydraulic cylinder 411, hydraulic cylinder 412, hydraulic cylinder 413, hydraulic cylinder 414.Hydraulic system is established Operating pressure, oil cylinder are extended to the middle position of total kilometres.By the transhipment of bearing product, perpendicular working condition is played, three-position four-way valve 5 is in Middle position cut-off state, hydraulic oil source do not work, and hydraulic system is closed system.After the completion of work, three-position four-way valve 5 is in the right side Position on-state, oil cylinder reset.For example, when three-position four-way valve 5 is in right position on-state, in-oil cylinder liquid returns to oil Source, to which oil cylinder resets.
It should be noted that the first valve 5 can also be other types of valve.For example, valve should have, there are three works Make position, to by adjusting the position of valve can realize respectively fuel feeding build pressure, system lock and oil cylinder reset (for example, The reset of oil cylinder by in-oil cylinder oil flow back into oil sources realize) operation.It may be noted that the hydraulic pressure of the embodiment of the present invention System can also make it be in closed state always after oil cylinder establishes initial pressure, without playing perpendicular front and back Re-start in-oil cylinder oil level adjustment after perpendicular and reset etc..Such as the hydraulic cylinder of this mode can be only in quilts such as rockets The dynamic tune to supported object load is just realized when supporter is placed on it or plays perpendicular by the variation of the second support portion height Whole, this mode or mode of texturing are all within protection scope of the present invention.
As described in Figure 5, positive lumen road 48 is also connected with accumulator 6, to compensation work state hydraulic system valve member, pipeline A small amount of leakage, to ensure hydraulic system not decompression, it is ensured that be supported the safety of product.
As shown in fig. 6, the second support portion 31,32,33,34 is uniformly arranged on the first side of main part.For example, it is also possible to The load change of perpendicular process is played according to object to be supported, the second support portion 3 is arranged in interval different distance h.For example, from the first support To on the direction S2 of the second support portion 3, the interval h of two neighboring second support portion 3 can gradually increase in portion 2.For example, from On the direction S2 of first the 2 to the second support portion of support portion 3, the interval h between two neighboring second support portion 3 increases 20- every time 40cm, so as to by the second support portion 3 of negligible amounts, realized it is perpendicular during load to supported object in an axial direction Distribution, and realize and the second support portion 3 is targetedly designed according to the axial change regulation of load during playing perpendicular Position, to better safety of protection supported object during playing perpendicular.
In one embodiment, on the second direction S2 along 1 length of the main part, close to described first The cross-sectional area of oil cylinder corresponding to second support portion 3 of support part 2 is less than or equal to the far from first support portion 2 The cross-sectional area of oil cylinder corresponding to two support portions 3.For example, when it includes two the second support portion 3 to play perpendicular device, Cross-sectional area close to the 3 corresponding oil cylinder of the second support portion of the first support portion 2 is less than or equal to far from the first support portion 2 The cross-sectional area of second support portion, 3 corresponding oil cylinder, so as to more effectively offset second far from the first support portion 2 Support portion 3 is when such as rocket plays perpendicular, load change caused by the relatively large deformation being subject to.Due to the far from the first support portion 2 Two support portions, 3 corresponding oil cylinder area is larger, and the anti-chamber of two oil cylinders is by anti-chamber pipeline connection, therefore, two oil cylinders Anti- chamber pressure it is equal.In the cross-sectional area difference of oil cylinder, perpendicular device support is such as rocket far from first when product The position deformation of support part 2 is larger, and the pressure change so as to cause corresponding second support portion 3 is larger, so as to by by position The cross-sectional area of oil cylinder corresponding to the second support portion 3 far from the first support portion 2 designs larger, can be correspondingly The stroke for reducing oil cylinder, so that oil cylinder stroke corresponding with close second support portion 3 of the first support portion 2 is close.
That is, the 3 corresponding oil cylinder of the second support portion far from the first support portion 2 can be become by smaller length Change and realizes larger pressure adjustment.Similarly, when having used perpendicular device to support the products such as rocket, close to the first support portion 2 The load change of second support portion 3 is relatively small, therefore larger length variation can be realized with smaller cross-sectional area, from And realize the height change roughly the same with separate second support portion 3 of the first support portion 2, it improves when rocket etc. is played perpendicular Concentricity has reduced moment of flexure of the perpendicular process load change to applications such as rockets.
In the above-described embodiments, in direction (the i.e. main part from close to the first support portion 2 to far from first support portion 2 Length direction) on S2, the transversal of each oil cylinder 414,413,412,411 of each second support portion 34,33,32,31 is corresponded to respectively Face area is reduced successively.That is, since rocket etc. is during playing perpendicular, from the first support portion 2 to the second support portion 3 On second direction S2, the pressure-bearing variation for playing perpendicular device is sequentially increased, to by making the second support portion 3 on direction S2 The cross-sectional area of corresponding oil cylinder is sequentially increased, and can preferably avoid rocket caused by the stroke difference due to oil cylinder Alignment be deteriorated the case where, to preferably protect erect during rocket safety.
In this embodiment, for example, with spacing distance between adjacent second support portion 3 increase, Rocket mass and length The cross-sectional area increase of the increase of degree, oil cylinder increases.For example, the distance being spaced between adjacent second support portion 3 is identical When, from the first support portion 2, on the second direction S2 of the second support portion 3, the cross-sectional area increase of oil cylinder is with rocket Quality, the elasticity of length and shell increases and increases.Equally, in the quality of rocket, length and identical elasticity, From the direction S2 of first the 2 to the second support portion of support portion 3, the increase of the cross-sectional area of corresponding oil cylinder is with adjacent The increase of spacing distance between two support portions 3 and increase.It should be pointed out that playing perpendicular device based on what the principle designed, all It belongs to the scope of protection of the present invention.
In one embodiment, the first support portion 2 can be rotatably set in the first side of main part 1, pivot center example It is such as consistent with the width direction of main part 1.The embodiment of the present invention is by making the first support portion 2 is rotatable on main part 1 to set It sets, can be in supported objects such as rockets during playing perpendicular, and the height (size in a first direction) of the second support portion 3 When changing so that the supported objects such as rocket can be turned round with the first support portion 2, to avoid object to be supported from bearing to add Moment of flexure further increases rocket and waits for supporter in the safety for playing perpendicular process.
Another aspect of the present invention provides a kind of hoisting machine, including plays perpendicular device as described above.The present invention's rises Therefore crane, has corresponding technique effect as a result of perpendicular device is played.
The present invention's plays perpendicular device and hoisting machine, by the way that the second support of at least two second support portions and connection is arranged The regulating mechanism in portion, can according to rise it is perpendicular during product casing pressure change, dynamically adjust played hanging object first The load distribution of support part and the second support portion, to improve the reliability of perpendicular device.
Referring to Fig. 7, during actual product (for example, rocket) plays perpendicular, if the second support portion 3 of main part 1 is Positioned at the first support portion 2 along the same side of 1 length direction S2 of main part, then the tail portion of rocket can be 2 by the first support portion Support, head are supported by being arranged in the second support portion 3 of 2 side of the first support portion.For example, with shaft rotation mode In the case of playing perpendicular rocket, shaft can be for example arranged close to the first support portion 2, and the direction of shaft can for example be erected with rising The width direction of the main part of device is consistent.When playing perpendicular rocket, for example, can be by making the rocket nose section set on main part 1 Side is rotated around above-mentioned shaft along the directions r1, realizes that rising for rocket is perpendicular.
The above embodiment of the present invention can be combined with each other, and have corresponding technique effect.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention With within principle, any modification, equivalent replacement, improvement and so on should all be included in the protection scope of the present invention god.

Claims (12)

1. one kind playing perpendicular device, which is characterized in that including:
Main part, the first support portion set on the main part, at least two second support portions, and connection described at least two The regulating mechanism of second support portion;
Wherein, the main part includes reciprocal first side and the second side in a first direction;First support portion and Described at least two second support portions are set to first side;Described at least two second support portions are along the main part length Second direction is arranged, and first support portion and at least two second support portion are used to support object to be supported;
The variation for the load that the regulating mechanism is used to be applied by object to be supported according to described at least two second support portions is moved Adjust to state the load distribution of described at least two second support portions.
2. according to claim 1 perpendicular device, which is characterized in that the regulating mechanism is hydraulic system or air pressure system System.
3. according to claim 2 perpendicular device, which is characterized in that the regulating mechanism is hydraulic system;
The wherein described hydraulic system includes the first hydraulic cylinder and the second hydraulic cylinder;First hydraulic cylinder one end connects it In second support portion, and the other end connect the first valve;One end of second hydraulic cylinder connects another institute The second support portion is stated, and the other end connects first valve;
The positive chamber of first oil cylinder and second oil cylinder is described to form positive chamber isobaric system by positive chamber pipeline connection The anti-chamber of first oil cylinder and second oil cylinder is by anti-chamber pipeline connection, to form anti-chamber isobaric system;
First valve is used to adjust the oil mass and oil level of first oil cylinder and second oil cylinder.
4. according to claim 2 perpendicular device, which is characterized in that including:
Multiple second support portions set on first side of the main part, the hydraulic system include that multiple difference one are a pair of Answer multiple oil cylinders of the multiple second support portion;
Wherein the multiple second support portion is separately connected one end of corresponding oil cylinder, and the other end of oil cylinder is connected to the first valve Door;The positive chamber of the multiple oil cylinder is by positive chamber pipeline connection, to form positive chamber isobaric system, and the anti-chamber of the multiple oil cylinder By anti-chamber pipeline connection, to form anti-chamber isobaric system;
First valve is used to adjust the oil mass and oil level of first oil cylinder and second oil cylinder.
5. according to claim 3 or 4 perpendicular device, which is characterized in that along described the second of the main part length On direction, the cross-sectional area of the oil cylinder corresponding to the second support portion close to first support portion is less than or equal to far from institute State the cross-sectional area of the oil cylinder corresponding to the second support portion of the first support portion.
6. according to claim 5 perpendicular device, which is characterized in that in the second direction along the main part length On, it is corresponded to respectively to far from second support portion that first support portion is set gradually from close to first support portion Oil cylinder cross-sectional area it is incremented by successively.
7. according to claim 3 or 4 perpendicular device, which is characterized in that the positive lumen road is also connected with accumulator, the storage It can liquid leakage of the device for compensating the hydraulic system.
8. according to claim 3 or 4 perpendicular device, which is characterized in that first valve is three-position four-way valve.
9. playing perpendicular device according to claim 1-4 any one of them, which is characterized in that first support portion is rotatably set It sets in first side of the main part, and rotation axis is consistent with the width direction of the main part.
10. playing perpendicular device according to claim 1-4 any one of them, which is characterized in that second support portion is 3-12, Second support portion is set to the homonymy of first support portion in this second direction.
11. according to claim 10 perpendicular device, which is characterized in that second support portion is coaxially set each other It sets, and is coaxially disposed with first support portion.
12. a kind of hoisting machine, which is characterized in that play perpendicular device including such as claim 1-11 any one of them.
CN201810264152.0A 2018-03-28 2018-03-28 Lifting device and crane Active CN108502727B (en)

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CN202010798437.XA CN112061980B (en) 2018-03-28 2018-03-28 Erecting device and crane for rocket erecting
CN202010798438.4A CN112062061B (en) 2018-03-28 2018-03-28 Erecting device and crane for erecting carrier rocket
CN201810264152.0A CN108502727B (en) 2018-03-28 2018-03-28 Lifting device and crane

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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110186325A (en) * 2019-05-23 2019-08-30 贵州航天天马机电科技有限公司 A kind of Solid Launch Vehicle multi-point support system
CN110425931A (en) * 2019-07-31 2019-11-08 北京航天发射技术研究所 A kind of twin-tub Erecting System
CN110745056A (en) * 2019-10-10 2020-02-04 北京中科宇航探索技术有限公司 Rocket transfer supporting device and rocket transfer trolley
CN111006546A (en) * 2019-11-05 2020-04-14 蓝箭航天空间科技股份有限公司 Rocket erecting arm
CN111023899A (en) * 2019-11-05 2020-04-17 蓝箭航天空间科技股份有限公司 Rocket transferring and erecting system
WO2021088818A1 (en) * 2019-11-05 2021-05-14 蓝箭航天空间科技股份有限公司 Auxiliary hydraulic supporting device for rocket
CN114084785A (en) * 2021-10-27 2022-02-25 中国运载火箭技术研究院 Overturning lifting appliance with self-adaptive adjusting function and overturning lifting method

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108502727B (en) * 2018-03-28 2023-12-05 蓝箭航天技术有限公司 Lifting device and crane
CN115231008B (en) * 2022-08-18 2024-05-17 北京中科宇航技术有限公司 Uniform load stable adjusting system

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1153871A (en) * 1996-11-13 1997-07-09 中国人民解放军第二炮兵工程学院 Hydraulic system for large erecting equipment
CN103663199A (en) * 2013-12-13 2014-03-26 中联重科股份有限公司 Hoisting machine
KR20170105978A (en) * 2016-03-11 2017-09-20 주식회사수산중공업 Crane with overload prevention system
CN107701545A (en) * 2017-07-04 2018-02-16 贵州航天天马机电科技有限公司 A kind of two-tank method Erecting System
CN208394644U (en) * 2018-03-28 2019-01-18 蓝箭航天技术有限公司 Play perpendicular device and hoisting machine
CN112061980A (en) * 2018-03-28 2020-12-11 蓝箭航天技术有限公司 Erecting device and crane for rocket erecting

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1187797A (en) * 1995-05-02 1998-07-15 克瓦纳尔海运公司 Method for rocket launching
ATE464530T1 (en) * 2007-10-23 2010-04-15 Onuk Tasit Sanayi Ltd Sirketi COLLAPSIBLE ROCKET LAUNCHER RAMP
US7900547B2 (en) * 2008-01-17 2011-03-08 The Boeing Company System and method for preparing a launch device
CN203501906U (en) * 2013-07-26 2014-03-26 北京航天发射技术研究所 Rocket launching pad supporting arm
RU2555056C1 (en) * 2014-02-20 2015-07-10 Акционерное общество "Центральное конструкторское бюро "Титан" (АО "ЦКБ "Титан") Launcher for transportation and mortar start of missile from transporting and starting container
CN104776754B (en) * 2015-04-15 2016-05-18 北京航天发射技术研究所 A kind of 8 fulcrum leveling methods of rocket launch platform
CN106428655B (en) * 2015-08-13 2019-02-12 贵州航天天马机电科技有限公司 A kind of carrier rocket plays vertical frame and adaptively pushes away dress system
RU2620007C2 (en) * 2015-11-16 2017-05-22 Российская Федерация, от имени которой выступает Министерство обороны Российской Федерации Mobile launcher
CN205245898U (en) * 2015-11-24 2016-05-18 四川航天系统工程研究所 There is not quick -witted light -duty high mobility launch vehicle of gyration
CN105910494A (en) * 2016-06-29 2016-08-31 贵州航天天马机电科技有限公司 Stable erection and rapid back-falling electrical control system of rocket erection device
CN107270770B (en) * 2017-07-26 2019-01-25 北京航天发射技术研究所 A kind of guided missile rear support guiding device for firing box
CN107764133B (en) * 2017-09-29 2020-08-07 北京航天发射技术研究所 Truss type vertical missile-launching arm
CN107796266B (en) * 2017-09-29 2020-03-03 北京航天发射技术研究所 Lightweight erecting heat-insulation cabin and preparation method thereof

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1153871A (en) * 1996-11-13 1997-07-09 中国人民解放军第二炮兵工程学院 Hydraulic system for large erecting equipment
CN103663199A (en) * 2013-12-13 2014-03-26 中联重科股份有限公司 Hoisting machine
KR20170105978A (en) * 2016-03-11 2017-09-20 주식회사수산중공업 Crane with overload prevention system
CN107701545A (en) * 2017-07-04 2018-02-16 贵州航天天马机电科技有限公司 A kind of two-tank method Erecting System
CN208394644U (en) * 2018-03-28 2019-01-18 蓝箭航天技术有限公司 Play perpendicular device and hoisting machine
CN112061980A (en) * 2018-03-28 2020-12-11 蓝箭航天技术有限公司 Erecting device and crane for rocket erecting
CN112062061A (en) * 2018-03-28 2020-12-11 蓝箭航天技术有限公司 Erecting device and crane for erecting carrier rocket

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110186325A (en) * 2019-05-23 2019-08-30 贵州航天天马机电科技有限公司 A kind of Solid Launch Vehicle multi-point support system
CN110425931A (en) * 2019-07-31 2019-11-08 北京航天发射技术研究所 A kind of twin-tub Erecting System
CN110745056A (en) * 2019-10-10 2020-02-04 北京中科宇航探索技术有限公司 Rocket transfer supporting device and rocket transfer trolley
CN111006546A (en) * 2019-11-05 2020-04-14 蓝箭航天空间科技股份有限公司 Rocket erecting arm
CN111023899A (en) * 2019-11-05 2020-04-17 蓝箭航天空间科技股份有限公司 Rocket transferring and erecting system
WO2021088818A1 (en) * 2019-11-05 2021-05-14 蓝箭航天空间科技股份有限公司 Auxiliary hydraulic supporting device for rocket
CN114084785A (en) * 2021-10-27 2022-02-25 中国运载火箭技术研究院 Overturning lifting appliance with self-adaptive adjusting function and overturning lifting method
CN114084785B (en) * 2021-10-27 2024-05-14 中国运载火箭技术研究院 Overturning lifting appliance with self-adaptive adjusting function and overturning lifting method

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CN112061980B (en) 2022-05-13
CN112061980A (en) 2020-12-11
CN112062061A (en) 2020-12-11
CN108502727B (en) 2023-12-05

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