CN105460337A - Blade basket for cleaning and fluorescent inspection of aero-engine rotor blades - Google Patents

Blade basket for cleaning and fluorescent inspection of aero-engine rotor blades Download PDF

Info

Publication number
CN105460337A
CN105460337A CN201510778122.8A CN201510778122A CN105460337A CN 105460337 A CN105460337 A CN 105460337A CN 201510778122 A CN201510778122 A CN 201510778122A CN 105460337 A CN105460337 A CN 105460337A
Authority
CN
China
Prior art keywords
blade
basket
blades
tenon
lateral strut
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
CN201510778122.8A
Other languages
Chinese (zh)
Inventor
王超
杨天南
赵四洋
唐雅伶
王威
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.)
Shenyang Liming Aero Engine Group Co Ltd
Original Assignee
Shenyang Liming Aero Engine Group Co 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 Shenyang Liming Aero Engine Group Co Ltd filed Critical Shenyang Liming Aero Engine Group Co Ltd
Priority to CN201510778122.8A priority Critical patent/CN105460337A/en
Publication of CN105460337A publication Critical patent/CN105460337A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65DCONTAINERS FOR STORAGE OR TRANSPORT OF ARTICLES OR MATERIALS, e.g. BAGS, BARRELS, BOTTLES, BOXES, CANS, CARTONS, CRATES, DRUMS, JARS, TANKS, HOPPERS, FORWARDING CONTAINERS; ACCESSORIES, CLOSURES, OR FITTINGS THEREFOR; PACKAGING ELEMENTS; PACKAGES
    • B65D7/00Containers having bodies formed by interconnecting or uniting two or more rigid, or substantially rigid, components made wholly or mainly of metal
    • B65D7/12Containers having bodies formed by interconnecting or uniting two or more rigid, or substantially rigid, components made wholly or mainly of metal characterised by wall construction or by connections between walls
    • B65D7/14Containers having bodies formed by interconnecting or uniting two or more rigid, or substantially rigid, components made wholly or mainly of metal characterised by wall construction or by connections between walls of skeleton or like apertured construction, e.g. baskets or carriers formed of wire mesh, of interconnected bands, bars, or rods, or of perforated sheet metal
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B08CLEANING
    • B08BCLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
    • B08B13/00Accessories or details of general applicability for machines or apparatus for cleaning

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Adornments (AREA)

Abstract

The invention discloses a blade basket for cleaning and fluorescent inspection of aero-engine rotor blades. Angular brackets mutually spaced in the longitudinal direction and aligned in the transverse direction are arranged on bottom steel bars of a basket body, transverse stop rods for locating the lower ends of blade tenons are arranged at the bottom ends of the angular brackets, transverse supporting rods A are fixed to the middle parts of the angular brackets, transverse supporting rods B are fixed to the upper ends of the angular brackets, and tenon clamping claws capable of clamping the blade tenons are fixed to the transverse supporting rods A and the transverse supporting rods B. When the blade basket is used for containing the blades, the transverse stop rods and the tenon clamping claws locate the blades in a six-point mode, collision does not occur easily in the cleaning, fluorescent inspection, circulating and lifting process of the blades, and therefore scrapping caused by collision is reduced; the blades are vertically placed in the basket, and therefore the loading capacity of the basket is greater than that of a flat basket of the same size by one third; the contact area between the blades and clamps is small, the surfaces of the blades are not shielded and can be cleaned completely, fluorescent agents can be sprayed to the whole surfaces of the blades in the fluorescent inspection process, and therefore the cleaning quality and the fluorescent inspection quality of the blades can be guaranteed.

Description

A kind of aeroengine rotor leaf cleaning and fluorescence blade basket
Technical field
The present invention relates to the utensil of splendid attire component of machine, a kind of blade basket used in particularly aeroengine rotor blade washing, fluorescence process.
Background technology
Aeroengine rotor blade (as shown in Figure 1) surface quality requirements is very strict, in washing, fluorescence process, usual use is put down basket (being namely simple plane at the bottom of basket) and is carried out splendid attire blade, at the bottom of blade lies in basket, not only splendid attire limited amount, and at washing, fluorescence, turnover and the easy play of hoisting process Leaf with mutually collide with, more colliding with can cause blade rejection, brings unnecessary economic loss to enterprise.
Summary of the invention
For the defect with flat basket splendid attire blade, the object of this invention is to provide a kind of blade and locate aeroengine rotor leaf cleaning that is firm, that not easily collide with and fluorescence blade basket.
For realizing this purpose, aeroengine rotor leaf cleaning provided by the invention and fluorescence blade basket, comprise the square basket be welded into by reinforcing bar, the bottom surface reinforcing bar of basket is fixed with the angular support frame of longitudinally spaced, lateral alignment, the horizontal pin for location, blade tenon lower end is had in the bottom of angular support frame, lateral strut A is fixed with at the middle part of angular support frame, angular support frame upper end be fixed with lateral strut B, lateral strut A and lateral strut B are fixed with the tenon claw that can clamp blade tenon respectively.
Described angular support frame and bottom surface reinforcing bar are 30 ° of angles.
Two that described tenon claw is welded on the both sides of described lateral strut A and lateral strut B by lower end, upper end links together have certain elastomeric curved wire net and form.
During with blade basket splendid attire blade of the present invention, blade lean is put, blade tenon lower end is stuck on horizontal pin, with the tenon claw on lateral strut A, the middle part of blade tenon is clamped, with the tenon claw on lateral strut B, the upper end of blade tenon is clamped.Blade by the tenon claw on horizontal pin and lateral strut A and lateral strut B by six point locations.
With compared with flat basket splendid attire blade, advantage of the present invention is:
1, blade is located firm in basket, and in washing, fluorescence, turnover and hoisting process, blade not easily play occurs, and can avoid mutually colliding with, thus greatly reduce that blade causes because mutually colliding with scrap phenomenon.
2, blade erects and puts in basket, can fill 1/3rd blades than the flat basket identical with size dimension more, and the space availability ratio of blade basket improves.
3, blade and its fixture minimally area of contact, its surface is not blocked, and in washing and fluorescence process, blade surface can be washed, and during fluoroscopy, fluorescer can spray attachment blade all surfaces, and blade washs and fluorescent substance measures to ensure.
Accompanying drawing explanation
Fig. 1 is the structural representation of aeroengine rotor blade, wherein Fig. 1 (a) be blade front view, left view that Fig. 1 (b) is Fig. 1 (a);
Fig. 2 is the block diagram of blade basket of the present invention;
Fig. 3 is the birds-eye view of Fig. 2;
Fig. 4 is the lateral plan of single support portions in Fig. 2
Fig. 5 is C portion enlarged drawing in Fig. 3;
Fig. 6 is blades installation schematic diagram (lateral plan).
Nomenclature in figure: 1-blade, 2-blade tenon, 3-basket, 4-bottom surface reinforcing bar, 5-angular support frame, the horizontal pin of 6-, 7-lateral strut A, 8-lateral strut B, 9-tenon claw.
Detailed description of the invention
Below in conjunction with drawings and Examples, the present invention will be further described.
As shown in Figure 1, blade 1 bottom of aeroengine rotor is blade tenon 2, and blade tenon length is 120mm, and blade tenon bottom width is 20mm, and blade tenon top (neck) width is 10mm.
Fig. 2,3,4,5 is the structural representation of the blade basket of this blade of splendid attire.This blade basket comprises the square basket 3 be welded into by reinforcing bar, and basket is horizontal and vertical is of a size of 1m, is highly 0.5m.Be made up of bottom surface reinforcing bar 4 longitudinal arrangement of four (comprising edge) diameter 10mm at the bottom of the basket of basket, reinforcing bar horizontal mutual spacing in bottom surface is 330mm, before and after on the reinforcing bar of bottom surface, spaced 225mm welds four angular support frames 5, angular support frame is made up of angle bar or steel plate, its both sides are mutually vertical, be formed as 30 ° of slopes with bottom surface reinforcing bar 4, slope length is 100mm.After the bottom of angular support frame is superimposed up and down by two reinforcing bars together horizontal welding on the reinforcing bar of bottom surface, form the horizontal pin 6 that blade tenon lower edge is located, at angular support frame apart from horizontal pin 20mm place welding lateral strut A7, at angular support frame apart from 5mm place, its upper end welding lateral strut B8, lateral strut A and lateral strut B laterally weld a pair tenon claw 9 as shown in Figure 5 every 140mm, each tenon claw is welded on lateral strut A and lateral strut B both sides respectively by two lower ends, the curved wire net (the reinforcing bar braiding of wire sets diameter 3mm is made) that upper end links together is formed, overall in swallowtail shape, often pair of tenon claw tilts to the other side mutually, its tip spacing is than blade tenon upper width slightly large (have more than tenon upper width and be no more than 0.06mm), formation can clamp the clip of blade tenon.A pair tenon claw on lateral strut B is for clamping the upper end of blade tenon, and a pair tenon claw on lateral strut A is for clamping the middle part of blade tenon, and two pairs of tenon claws are one group, for locating a slice blade.Arrange by above-mentioned size, altogether can arrange 28 groups (as shown in Figures 2 and 3) in basket.
For preventing misoperation generation blade to drop phenomenon, finer wire is adopted to be woven into net (not shown) in the outside of whole blade basket.
As shown in Figure 6, during with the present embodiment splendid attire engine rotor blade, 28 blades are tilted to put with 28 groups of tenon claw one_to_one corresponding respectively, be stuck on horizontal pin by the blade tenon lower end of every sheet blade, in the middle part of blade tenon and upper end is respectively by tenon claw clamping (tenon claw and blade tenon side play are no more than 0.03mm) on lateral strut A and lateral strut B.
This blade basket is than putting down basket many splendid attires 1/3rd blade with same specification.Blade is by six point locations in basket, and not easily play in washing, fluorescence, turnover and hoisting process, can not collide with, and what blade caused because colliding with scrap phenomenon greatly reduces, for enterprise avoids unnecessary economic loss.Simultaneously, blade and fixture (horizontal lever, lateral strut A, lateral strut B and tenon claw) minimally area of contact, surface is not blocked, can be washed in washing and fluorescence process Leaf surface, during fluoroscopy, fluorescer can spray attachment blade all surfaces, and the quality of blade washing and fluorescence is ensured.

Claims (3)

1. an aeroengine rotor leaf cleaning and fluorescence blade basket, comprise the square basket (3) be welded into by reinforcing bar, it is characterized in that: be fixed with longitudinally spaced on the bottom surface reinforcing bar (4) of basket, the angular support frame (5) of lateral alignment, the horizontal pin (6) for location, blade tenon lower end is had in the bottom of angular support frame, lateral strut A (7) is fixed with at the middle part of angular support frame, angular support frame upper end be fixed with lateral strut B (8), lateral strut A (7) and lateral strut B (8) are fixed with the tenon claw (9) that can clamp blade tenon respectively.
2. aeroengine rotor leaf cleaning according to claim 1 and fluorescence blade basket, is characterized in that: described angular support frame (5) and bottom surface reinforcing bar (4) are in 30 ° of angles.
3. aeroengine rotor leaf cleaning according to claim 1 and fluorescence blade basket, is characterized in that: two that described tenon claw (9) is welded on the both sides of described lateral strut A (7) and lateral strut B (8) by lower end, upper end links together have certain elastomeric curved wire net and form.
CN201510778122.8A 2015-11-13 2015-11-13 Blade basket for cleaning and fluorescent inspection of aero-engine rotor blades Pending CN105460337A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510778122.8A CN105460337A (en) 2015-11-13 2015-11-13 Blade basket for cleaning and fluorescent inspection of aero-engine rotor blades

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510778122.8A CN105460337A (en) 2015-11-13 2015-11-13 Blade basket for cleaning and fluorescent inspection of aero-engine rotor blades

Publications (1)

Publication Number Publication Date
CN105460337A true CN105460337A (en) 2016-04-06

Family

ID=55598589

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510778122.8A Pending CN105460337A (en) 2015-11-13 2015-11-13 Blade basket for cleaning and fluorescent inspection of aero-engine rotor blades

Country Status (1)

Country Link
CN (1) CN105460337A (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20100009674A (en) * 2008-07-21 2010-01-29 김상돈 A washig machine for a test-apparatus
CN202321129U (en) * 2011-09-30 2012-07-11 东风(十堰)车身部件有限责任公司 Folding bumper carrying protective mechanism
CN202752266U (en) * 2012-08-08 2013-02-27 湖南电子信息产业集团有限公司 Washing clamp
CN203470439U (en) * 2013-08-16 2014-03-12 陈彩央 Cleaning frame for tongue depressors
CN104976489A (en) * 2014-04-11 2015-10-14 上海启发电子科技有限公司 Support used for hanging guide wheel

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20100009674A (en) * 2008-07-21 2010-01-29 김상돈 A washig machine for a test-apparatus
CN202321129U (en) * 2011-09-30 2012-07-11 东风(十堰)车身部件有限责任公司 Folding bumper carrying protective mechanism
CN202752266U (en) * 2012-08-08 2013-02-27 湖南电子信息产业集团有限公司 Washing clamp
CN203470439U (en) * 2013-08-16 2014-03-12 陈彩央 Cleaning frame for tongue depressors
CN104976489A (en) * 2014-04-11 2015-10-14 上海启发电子科技有限公司 Support used for hanging guide wheel

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PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20160406

WD01 Invention patent application deemed withdrawn after publication