CN108482714A - A kind of enhanced Bearing cylinder upper ledge and its strengthen connection structure - Google Patents

A kind of enhanced Bearing cylinder upper ledge and its strengthen connection structure Download PDF

Info

Publication number
CN108482714A
CN108482714A CN201810210098.1A CN201810210098A CN108482714A CN 108482714 A CN108482714 A CN 108482714A CN 201810210098 A CN201810210098 A CN 201810210098A CN 108482714 A CN108482714 A CN 108482714A
Authority
CN
China
Prior art keywords
upper ledge
cylinder
connection structure
carbon cloth
face
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.)
Pending
Application number
CN201810210098.1A
Other languages
Chinese (zh)
Inventor
白刚
张立新
刘国青
阮剑华
肖伟
李竞蔚
余快
王丽俐
易茂斌
李响
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.)
Beijing Institute of Spacecraft System Engineering
Original Assignee
Beijing Institute of Spacecraft System Engineering
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 Institute of Spacecraft System Engineering filed Critical Beijing Institute of Spacecraft System Engineering
Priority to CN201810210098.1A priority Critical patent/CN108482714A/en
Publication of CN108482714A publication Critical patent/CN108482714A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/66Arrangements or adaptations of apparatus or instruments, not otherwise provided for
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/10Artificial satellites; Systems of such satellites; Interplanetary vehicles

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Laminated Bodies (AREA)

Abstract

The invention discloses a kind of enhanced Bearing cylinder upper ledge and its strengthen connection structure, including upper ledge, cylinder and carbon cloth;Upper ledge is annulus, and one end face of upper ledge is respectively equipped with the pin hole that the screw hole that several are used to connect load is used to install positioning pin with several, another end face of upper ledge is equipped with the groove for injecting glue reservoir;Cylinder is hollow cylinder, several through-holes are evenly distributed in the middle part of cylinder side;Upper ledge is coaxially bonded in body end surface, and the piece on the outside of upper ledge between cylinder inside passes through carbon cloth and wraps up splicing.The present invention realizes being reliably connected for interface and being obviously improved for mechanic properties, and interface precision is also effectively improved by the cooperation of upper ledge, cylinder and carbon cloth, compensates for the weaker defect of traditional loaded cylinder upper ledge bearing capacity.

Description

A kind of enhanced Bearing cylinder upper ledge and its strengthen connection structure
Technical field
The present invention relates to a kind of enhanced Bearing cylinder upper ledge and its strengthen connection structure, is particularly suitable for support to list Tie point has the load of big bearing requirements, belongs to high rail remote sensing satellite platform structure technical field.
Background technology
In recent years, telecommunication satellite carrying continues to increase, and the tie point bearing requirements of load and structure are higher and higher, wherein passing through Crossing loaded cylinder upper ledge or the antenna connector near upper ledge can all be connected on upper ledge, and high rail remote sensing satellite platform is mainly used in Remote sensing satellite field, the Main Load of wherein Optical remote satellite are the larger optical cameras of weight, and camera majority is mounted on pair Ground, loaded cylinder upper ledge is frequently as maximum support part or most of payload interface.
With large-scale antenna, the fast development of high-performance camera load, the weight of load is also constantly promoted, therefore also constantly To the bearing capacity of platform interface, more stringent requirements are proposed.
Currently, traditional loaded cylinder upper ledge is a kind of L-type section structure, the upper ledge of this structure makes load effect and knot The state of structure is more complicated, and longitudinal Tensile or Compressive Loading is not only born on the load tie point of upper ledge, also subject to due to supporting rib with plus Loading point position it is eccentric and caused by bending load because traditional upper ledge design is limited by weight and upper ledge per-interface space size, Design process is being continuously improved, utmost carrying ability is had reached, upper ledge interface bearing ability traditional at present is 8000N, is not enough to Meet the requirement of carrying bigger loading device.If performance cannot be broken through, loaded cylinder and platform structure will be restricted Using.Meanwhile to stablize the load smoothly transmitted and born at upper ledge tie point, it is necessary to will be carried out between upper ledge and loaded cylinder Assembly connection, bonding pad must satisfy the needs of high-mechanic.
Invention content
Present invention solves the technical problem that being:Overcome the deficiencies in the prior art, the present invention provides a kind of enhanced centers Loaded cylinder upper ledge and its strengthen connection structure, by the cooperation of upper ledge, cylinder and carbon cloth, realize interface be reliably connected and Mechanic properties are obviously improved, and interface precision is also effectively improved, and are compensated for traditional loaded cylinder upper ledge and are held The weaker defect of loading capability.
Technical solution of the invention is:
A kind of enhanced Bearing cylinder upper ledge and its strengthen connection structure, including upper ledge, cylinder and carbon cloth;Upper ledge is circle Ring, one end face of upper ledge are respectively equipped with the pin hole that the screw hole that several are used to connect load is used to install positioning pin with several, Another end face of upper ledge is equipped with the groove for injecting glue reservoir;Cylinder is hollow cylinder, is evenly distributed in the middle part of cylinder side Several through-holes;Upper ledge is coaxially bonded in body end surface, and the piece on the outside of upper ledge between cylinder inside is wrapped up by carbon cloth It is glued.
In a kind of above-mentioned enhanced Bearing cylinder upper ledge and its in strengthening connection structure, on one end face of the upper ledge It is evenly distributed with the 64 M6 screw holes and 4 M4 pin holes for installing positioning pin for connecting load respectively.
In a kind of above-mentioned enhanced Bearing cylinder upper ledge and its in strengthening connection structure, the depth of 64 M6 screw holes Degree is not less than 20mm, and the depth of 4 M4 pin holes is not less than 28mm;The position degree of 64 M6 screw holes and 4 M4 pin holes is not More than Φ 0.3mm.
In a kind of above-mentioned enhanced Bearing cylinder upper ledge and its in strengthening connection structure, one end face of the upper ledge The groove for loss of weight is equipped between several screw holes, one end face of the upper ledge is additionally provided with 4 M5 for technique processing Screw hole.
In a kind of above-mentioned enhanced Bearing cylinder upper ledge and its in strengthening connection structure, one end face of the upper ledge Flatness is not more than 0.2mm, and the ovality of upper ledge is not more than 0.3mm, and upper ledge end face and the verticality of upper ledge side are not more than 0.3mm。
In a kind of above-mentioned enhanced Bearing cylinder upper ledge and its in strengthening connection structure, the height of the upper ledge is not small In 40mm, upper ledge internal diameter and the difference of upper ledge outer diameter are not less than 12mm.
In a kind of above-mentioned enhanced Bearing cylinder upper ledge and its in strengthening connection structure, the upper ledge uses LD10CS I class GBn223-84 aluminum alloy materials.
In a kind of above-mentioned enhanced Bearing cylinder upper ledge and its in strengthening connection structure, the cylinder uses carbon fiber Polymer matrix composites covering aluminum honeycomb sandwich cylinder.
In a kind of above-mentioned enhanced Bearing cylinder upper ledge and its in strengthening connection structure, the carbon cloth is using multilayer leaching Glue carbon cloth, and be distributed according to gradient transition;The number of plies of carbon cloth is no less than 6 layers, and the thickness of every layer of carbon cloth is identical, the length of each layer carbon cloth It is identical to spend difference.
In a kind of above-mentioned enhanced Bearing cylinder upper ledge and its in strengthening connection structure, room temperature is coated on the carbon cloth Adhesive, and cure under pressure;It is symmetrically wrapped up centered on piece between on the inside of the above outer frame side of carbon cloth and cylinder.
Compared with the prior art, the invention has the advantages that:
【1】This invention removes the eccentric bending moments of interface, improve power transmission efficiency.Traditional upper ledge, bearing point position are deviateed Longitudinal bracing cylinder, in load bearing process, upper ledge inevitably bears additional bending moment, this can cause stress complicated, And the tie point face cylinder wall thickness center of the present invention, load are directly delivered on loaded cylinder, power transmission is direct, and there is no eccentric curved Square.
【2】Upper ledge of the present invention is Nian Jie with body end surface docking, and two equal gluings of binding face, interior outer cylinder wraps up after docking Carbon cloth reinforcement, the result entirely strengthened makes upper ledge single-point interface bearing ability reach 10KN, and Static Test Results show to pass The failure mode of the loaded cylinder upper ledge carrying of system is upper ledge drawing badly or is detached with loaded cylinder, and the failure mode after present invention carrying It is that M6 screws are broken, thus proves that the present invention has been more than traditional loaded cylinder upper ledge bearing capacity.
【3】It is equipped with weight loss groove between each adjacent holes of upper ledge of the present invention, and after reducing Baking soda, wall thickness inside and outside upper ledge It is 2mm, rationally realizes effective distribution of weight.
【4】Upper ledge end face of the present invention provides key interface mounting surface, it is contemplated that deformation caused by machining stress is taken repeatedly Processing combines the process of artificial aging processing, it is ensured that flatness is not more than 0.2mm.In addition, upper ledge is glued with cylinder Butt Assembling After molding, all hickeys of Combined machining, it is ensured that the position degree for being threadedly coupled interface is not more than Φ 0.3mm.
【5】Compact overall structure of the present invention is suitable for various working environments, and service life is relatively long, in complex working condition Under still can good operation, have the characteristics that applied widely, have good market application prospect.
Description of the drawings
Attached drawing is used to provide further understanding of the present invention, and is constituted part of this application, the embodiment of the present invention and It illustrates, for explaining the present invention, not constituting improper limitations of the present invention.In the accompanying drawings:
Fig. 1 is schematic structural view of the invention
Fig. 2 is the structural schematic diagram of upper ledge
Fig. 3 is upper ledge partial sectional view A
Fig. 4 is upper ledge partial sectional view B
Fig. 5 is upper ledge partial sectional view C
Fig. 6 is upper ledge partial sectional view D
Fig. 7 is upper ledge partial sectional view E
Fig. 8 is the partial sectional view of cylinder
Fig. 9 is the structural schematic diagram of carbon cloth
Wherein:1 upper ledge;2 cylinders;3 carbon cloths;
Specific implementation mode
To make the solution of the present invention more be illustrated, explanation and specific embodiment are made the present invention further below in conjunction with the accompanying drawings Description:
As shown in Figure 1, a kind of enhanced Bearing cylinder upper ledge and its reinforcing connection structure, including upper ledge 1,2 and of cylinder Carbon cloth 3;Upper ledge 1 is annulus, and 1 one end faces of upper ledge are respectively equipped with several and are used to pacify with several for connecting the screw hole of load The pin hole of positioning pin is filled, another end face of upper ledge 1 is equipped with the groove for injecting glue reservoir;Cylinder 2 is hollow cylinder, cylinder 2 It is evenly distributed several through-holes in the middle part of side;Upper ledge 1 is coaxially bonded on 2 end face of cylinder, 1 outside of upper ledge and 2 inside of cylinder Between piece pass through carbon cloth 3 package be glued.
As shown in Fig. 2~7, it is preferred that on 1 one end faces of upper ledge respectively be evenly distributed with 64 for connect load M6 screw holes and 4 M4 pin holes for installing positioning pin.
Preferably, the depth of 64 M6 screw holes is not less than 20mm, and the depth of 4 M4 pin holes is not less than 28mm;64 The position degree of M6 screw holes and 4 M4 pin holes is no more than Φ 0.3mm.
Preferably, the groove for loss of weight, the upper ledge 1 one are equipped between several screw holes of 1 one end faces of upper ledge A end face is additionally provided with 4 M5 screw holes for technique processing.
Preferably, the flatness of 1 one end faces of upper ledge is not more than 0.2mm, and the ovality of upper ledge 1 is not more than 0.3mm, upper ledge The verticality of 1 end face and 1 side of upper ledge is not more than 0.3mm.
Preferably, the height of upper ledge 1 is not less than 40mm, and 1 internal diameter of upper ledge and the difference of 1 outer diameter of upper ledge are not less than 12mm.
Preferably, upper ledge 1 uses LD10CS I class GBn223-84 aluminum alloy materials.
As shown in Figure 8, it is preferred that cylinder 2 uses carbon fiber resin matrix composite covering aluminum honeycomb sandwich cylinder.
As shown in Figure 9, it is preferred that carbon cloth 3 uses multilayer impregnation carbon cloth, and is distributed according to gradient transition;The number of plies of carbon cloth 3 No less than 6 layers, the thickness of every layer of carbon cloth 3 is identical, and the length difference of each layer carbon cloth 3 is identical.
Preferably, room temperature adhesive, and cure under pressure are coated on carbon cloth 3;Carbon cloth 3 is with 1 outside of upper ledge and 2 inside of cylinder Between piece centered on symmetrically wrap up.
Preferably, after trench separation, 1 inner wall of upper ledge and the thickness of 1 outer wall of upper ledge are set as 2mm.
Preferably, after upper ledge 1 is Nian Jie with cylinder 2, whole cylinder by rough milling, being heat-treated, finish-milling, assembly Combined machining, protect It is accurate to demonstrate,prove all connecting hole relative positions in upper ledge end, this is because upper ledge 1 is large scale annulus, processing ovality it is difficult to ensure that Very high, the ovality of cylinder 2 is also non-fine, and after the two docking bonding, ovality generally can be worse, therefore, it is necessary to pass through group It closes processing method and ensures interface precision.
The present invention operation principle be:
Upper ledge 1 is Nian Jie with the docking of cylinder 2, and the piece between 2 inside of 1 outside of upper ledge and cylinder is wrapped by carbon cloth 3 Wrap up in splicing, effective supplementing structure intensity;Load is mounted on upper ledge 1 again, you can realize that the stress that load is born directly transmits To cylinder 2, and then significantly increase bearing capacity.
The content not being described in detail in description of the invention is known to the skilled person technology.

Claims (10)

1. a kind of enhanced Bearing cylinder upper ledge and its reinforcing connection structure, it is characterised in that:Including upper ledge (1), cylinder (2) With carbon cloth (3);Upper ledge (1) is annulus, and (1) end face of upper ledge is respectively equipped with several for connecting the screw hole of load and several A pin hole for installing positioning pin, upper ledge (1) another end face are equipped with the groove for injecting glue reservoir;Cylinder (2) is hollow Cylinder, cylinder (2) side middle part are evenly distributed several through-holes;Upper ledge (1) is coaxially bonded on cylinder (2) end face, on Piece between on the outside of frame (1) and on the inside of cylinder (2) is wrapped up by carbon cloth (3) to be glued.
2. a kind of enhanced Bearing cylinder upper ledge according to claim 1 and its reinforcing connection structure, it is characterised in that: The 64 M6 screw holes and 4 M4 for installing positioning pin for connecting load are evenly distributed on (1) end face of the upper ledge respectively Pin hole.
3. a kind of enhanced Bearing cylinder upper ledge according to claim 2 and its reinforcing connection structure, it is characterised in that: The depth of 64 M6 screw holes is not less than 20mm, and the depth of 4 M4 pin holes is not less than 28mm;64 M6 screw holes and 4 The position degree of M4 pin holes is no more than Φ 0.3mm.
4. a kind of enhanced Bearing cylinder upper ledge according to claim 1 and its reinforcing connection structure, it is characterised in that: The groove for loss of weight is equipped between several screw holes of (1) end face of the upper ledge, (1) end face of the upper ledge is also M5 screw holes equipped with 4 for technique processing.
5. a kind of enhanced Bearing cylinder upper ledge according to claim 1 and its reinforcing connection structure, it is characterised in that: The flatness of (1) end face of the upper ledge is not more than 0.2mm, and the ovality of upper ledge (1) is not more than 0.3mm, upper ledge (1) end face It is not more than 0.3mm with the verticality of upper ledge (1) side.
6. a kind of enhanced Bearing cylinder upper ledge according to claim 1 and its reinforcing connection structure, it is characterised in that: The height of the upper ledge (1) is not less than 40mm, and upper ledge (1) internal diameter and the difference of upper ledge (1) outer diameter are not less than 12mm.
7. a kind of enhanced Bearing cylinder upper ledge according to claim 1 and its reinforcing connection structure, it is characterised in that: The upper ledge (1) uses LD10CS I class GBn223-84 aluminum alloy materials.
8. a kind of enhanced Bearing cylinder upper ledge according to claim 1 and its reinforcing connection structure, it is characterised in that: The cylinder (2) uses carbon fiber resin matrix composite covering aluminum honeycomb sandwich cylinder.
9. a kind of enhanced Bearing cylinder upper ledge according to claim 1 and its reinforcing connection structure, it is characterised in that: The carbon cloth (3) uses multilayer impregnation carbon cloth, and is distributed according to gradient transition;The number of plies of carbon cloth (3) is no less than 6 layers, every layer of carbon The thickness of cloth (3) is identical, and the length difference of each layer carbon cloth (3) is identical.
10. a kind of enhanced Bearing cylinder upper ledge according to claim 9 and its reinforcing connection structure, feature exist In:Room temperature adhesive, and cure under pressure are coated on the carbon cloth (3);Carbon cloth (3) is on the outside of upper ledge (1) and cylinder (2) inside Between piece centered on symmetrically wrap up.
CN201810210098.1A 2018-03-14 2018-03-14 A kind of enhanced Bearing cylinder upper ledge and its strengthen connection structure Pending CN108482714A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810210098.1A CN108482714A (en) 2018-03-14 2018-03-14 A kind of enhanced Bearing cylinder upper ledge and its strengthen connection structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810210098.1A CN108482714A (en) 2018-03-14 2018-03-14 A kind of enhanced Bearing cylinder upper ledge and its strengthen connection structure

Publications (1)

Publication Number Publication Date
CN108482714A true CN108482714A (en) 2018-09-04

Family

ID=63339240

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810210098.1A Pending CN108482714A (en) 2018-03-14 2018-03-14 A kind of enhanced Bearing cylinder upper ledge and its strengthen connection structure

Country Status (1)

Country Link
CN (1) CN108482714A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111422377A (en) * 2020-03-10 2020-07-17 上海卫星工程研究所 Structure suitable for satellite and facilitating assembly of double-layer flange type bearing cylinder and laminate

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201136593Y (en) * 2007-12-25 2008-10-22 上海复合材料科技有限公司 Micro-deformation carrier barrel
CN105122965B (en) * 2007-12-25 2012-07-25 上海卫星工程研究所 The connection implementation method of a kind of becket and loaded cylinder
CN105480435A (en) * 2015-12-02 2016-04-13 上海宇航系统工程研究所 Large honeycomb sandwich bearing cylinder

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201136593Y (en) * 2007-12-25 2008-10-22 上海复合材料科技有限公司 Micro-deformation carrier barrel
CN105122965B (en) * 2007-12-25 2012-07-25 上海卫星工程研究所 The connection implementation method of a kind of becket and loaded cylinder
CN105480435A (en) * 2015-12-02 2016-04-13 上海宇航系统工程研究所 Large honeycomb sandwich bearing cylinder

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111422377A (en) * 2020-03-10 2020-07-17 上海卫星工程研究所 Structure suitable for satellite and facilitating assembly of double-layer flange type bearing cylinder and laminate
CN111422377B (en) * 2020-03-10 2021-10-15 上海卫星工程研究所 Structure suitable for satellite and facilitating assembly of double-layer flange type bearing cylinder and laminate

Similar Documents

Publication Publication Date Title
CN112571825B (en) Composite material joint and preparation method thereof
CN101189118A (en) Method for manufacturing a reinforced shell for forming component parts for aircraft and shell for component parts for aircraft
JP2010508203A (en) Aircraft or spacecraft hardened enclosure with highly rigid laminated longitudinal members and corresponding laminated longitudinal members
CN105128785A (en) Combined type automobile energy-absorbing box
EP2900456A1 (en) A method of forming a structural connection between a spar cap and a fairing for a wind turbine blade
CN113771388B (en) Forming method of special-shaped composite material reinforced grid rib and special-shaped skin cabin section thereof
CN113911393A (en) Cone-prism transition type honeycomb interlayer bearing cylinder structure
CN108482714A (en) A kind of enhanced Bearing cylinder upper ledge and its strengthen connection structure
CN111070725A (en) Preparation method of mortise-tenon-connected carbon fiber composite material laminated plate
KR20110130636A (en) Insert, sandwich panel having the same and method for manufacturing the sandwich panel
CN102009481B (en) Method for manufacturing carbon fiber arm support for concrete pump truck
CN108000968A (en) A kind of new Terahertz carbon fiber composite panel structure
CN102297207A (en) Glued jointing and screw connection method between transmission shaft and metal flanges
US20140251076A1 (en) Concrete pumping equipment and bending connecting rod device thereof, and manufacturing method for the device
CN107748102A (en) It is a kind of to apply the balanced method for drawing load to radome
CN103241391A (en) Heat insulation component for heat control of a Mars landing machine, and manufacturing method thereof
CN211852482U (en) Connecting structure of composite material rod piece and metal joint
CN102837453B (en) Tension member and preparation method and engineering machinery thereof
EP1442873A3 (en) A repair method
CN110984578A (en) Arm support, engineering machinery and manufacturing method of arm support
CN109969432B (en) Detachable heat-proof structure and preparation method and application thereof
CN111059137A (en) Connecting structure of composite material rod piece and metal joint and forming method
CN203297186U (en) Hydraulic oil cylinder
CN202706334U (en) Anchor device for FRP (Fiber Reinforced Plastic) pipe and metal bar
CN101973124A (en) Method for manufacturing carbon fiber arm support for concrete pump truck

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20180904

RJ01 Rejection of invention patent application after publication