CN104712625B - Instrument metal hemming edge being fixed on composite material blade - Google Patents

Instrument metal hemming edge being fixed on composite material blade Download PDF

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Publication number
CN104712625B
CN104712625B CN201310670457.9A CN201310670457A CN104712625B CN 104712625 B CN104712625 B CN 104712625B CN 201310670457 A CN201310670457 A CN 201310670457A CN 104712625 B CN104712625 B CN 104712625B
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China
Prior art keywords
fixed
hemming edge
metal hemming
upper cover
cover plate
Prior art date
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Active
Application number
CN201310670457.9A
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Chinese (zh)
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CN104712625A (en
Inventor
马新伟
鲁金华
郝春鹏
李志忠
徐立国
鲁召朋
郭影
侯段敏
姚希双
王广平
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.)
AVIC Huiyang Aviation Propeller Co Ltd
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AVIC Huiyang Aviation Propeller Co Ltd
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Publication date
Application filed by AVIC Huiyang Aviation Propeller Co Ltd filed Critical AVIC Huiyang Aviation Propeller Co Ltd
Priority to CN201310670457.9A priority Critical patent/CN104712625B/en
Publication of CN104712625A publication Critical patent/CN104712625A/en
Application granted granted Critical
Publication of CN104712625B publication Critical patent/CN104712625B/en
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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16BDEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B11/00Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding
    • F16B11/006Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding by gluing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/16Blades

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Road Paving Structures (AREA)
  • Automobile Manufacture Line, Endless Track Vehicle, Trailer (AREA)

Abstract

The invention discloses a kind of instrument being glued to metal hemming edge on composite material blade, front apron is fixed on the front end of bottom plate, rear baffle is fixed on the rear portion of bottom plate, and the one end of upper cover plate away from paddle shaft is supported on front apron side wall, its other end is supported on rear baffle side wall;More than two pieces of lower supporting block is fixed between front apron and rear baffle, the holding tank that one end opposite position that had in lower supporting block does not have metal hemming edge with blade matches, both ends are respectively fixed with screw rod;Accommodate and be fixed with rubber protection pad in groove bottom;Upper cover plate is leaning out otic placode with each lower corresponding position of supporting block, and otic placode is being provided with hole with the corresponding position of screw rod, and screw rod is placed in hole, is fixed by locking nut;The rubber pad for being wrapped in heating component is fixed with upper cover plate inner wall.Metal hemming edge is glued on composite material blade using the present invention, its adhesive effect is good, without imaginary point;Its heat-transfer effect is good, saves energy;And will not damaged blade.

Description

Instrument metal hemming edge being fixed on composite material blade
Technical field
The present invention relates to a kind of instrument being glued to metal hemming edge on composite material blade.
Background technology
In recent years, composite material is continued to develop with its high specific strength with aeronautical technology, specific stiffness and good anti- Fatigability and corrosion resistance are widely applied aboard, are also made extensively using the helicopter of composite material blade With.It is very big by foreign object impact power because composite material blade blade tip has very high linear velocity, so blade tip part generally requires to glue The impact resistance of metal hemming edge enhancing blade is connect, and existing instrument metal hemming edge being bonded on blade is that metal hemming edge is recessed Mould.The metal hemming edge for scribbling glue and blade are placed in metal hemming edge cavity plate and carry out rigid pressurized, existing metal hemming edge cavity plate with The position of metal hemming edge contact is metal, using very stiff and demanding crimping, so since metal hemming edge cavity plate and metal hemming edge be not all for Regular shape, it is easy to since the position that error causes to have cannot contact or contact unreal, cause to crimp not in place, metal hemming edge It is unreal with blade bonding, there is imaginary point, easily come off, influence performance and the service life of blade.Also heating unit is enclosed in gold Belong to the outside of bound edge cavity plate, by metal heat transfer to metal hemming edge, its heat-transfer effect is poor, and a part of heat of peripheral heating unit It is scattered in air, wastes thermal energy.
The content of the invention
The purpose of the present invention is exactly to solve the above-mentioned problems in the prior art, there is provided metal hemming edge is glued to by one kind Metal hemming edge, is glued on composite material blade, its adhesive effect is good, does not have by the instrument on composite material blade using the instrument There is imaginary point;Its heat-transfer effect is good, saves energy;And will not damaged blade.
To achieve the above object, technical solution of the invention is:Metal hemming edge is glued to composite material paddle by one kind Instrument on leaf, it includes bottom plate, front apron, rear baffle, more than two pieces of lower supporting block, paddle shaft support plate and metal hemming edge Upper cover plate that inner wall shape matches, rubber pad, rubber protection pad, the heating component being wrapped in rubber pad, crimping screw rod and Nut;Front apron is fixed on the front end of bottom plate, and the one end of upper cover plate away from paddle shaft is supported on its side wall;Rear baffle is fixed on bottom The rear portion of plate, the upper cover plate other end are supported on its side wall;The rear end of bottom plate is fixed with paddle shaft support plate;In front apron and rear gear More than two pieces of lower supporting block is fixed between plate, is had in lower supporting block opposite with one end that blade does not have metal hemming edge The holding tank that position matches is answered, both ends are respectively fixed with screw rod;Accommodate and be fixed with rubber protection pad in groove bottom;Upper cover plate exists Otic placode is leant out with each lower corresponding position of supporting block, otic placode is being provided with hole with the corresponding position of screw rod, and screw rod is placed in hole, It is fixed by locking nut;The rubber pad for being enclosed with heating component is fixed with upper cover plate inner wall.
Heating component described above is heating tube or heater strip.
Bottom plate described above is mounted below traveling wheel.
In use, glued blade is placed in the holding tank of lower supporting block, front end and back support front apron and after In baffle sidewall, paddle shaft is supported in paddle shaft support plate, and metal hemming edge is placed in the upper end of blade, and upper cover plate is by locking nut and spiral shell Bar is crimped on metal hemming edge.The present invention has installed rubber pad additional in the contact position of upper cover plate and metal hemming edge, in this way, upper cover plate With metal hemming edge by rubber pad soft contact, it compensate for the gap caused by very stiff and demanding between metal, after it is crimped There is no gap, its adhesive effect is good, without imaginary point;The heating component of the present invention is located in rubber sheet gasket, it is directly metal bag Side is heated, and without transmission, heating is direct, and heat transfer effect is good, it be located in upper cover plate, without it is direct it is exposed outside, its to Outer heat-transfer effect is poor, saves energy.Rubber pad and rubber protection pad protect blade to be damaged during crimping.In short, using Metal hemming edge is glued on composite material blade by the present invention, its adhesive effect is good, without imaginary point;Its heat-transfer effect is good, saves Energy;And will not damaged blade.
Brief description of the drawings
Fig. 1 is the front sectional view of the present invention;
Fig. 2 is the top view of the present invention;
Fig. 3 is the AA sectional views of Fig. 1.
Embodiment
The present invention will be further described with specific embodiment below in conjunction with the accompanying drawings.
As shown in Figure 1, Figure 2 and Figure 3, the present embodiment includes the lower branch of bottom plate 13, front apron 1, more than 9, two pieces of rear baffle Bracer 6, paddle shaft support plate 16, the upper cover plate 2 to match with 4 inner wall shape of metal hemming edge, rubber pad 3, rubber protection pad 12, bag Heating component, crimping screw rod 11 and the nut 10 being rolled in rubber pad 3.Front apron 1 is fixed on the front end of bottom plate 13, upper cover plate 2 One end away from paddle shaft is supported on its side wall.Rear baffle 9 is fixed on the rear portion of bottom plate 13, and 2 other end of upper cover plate is supported on it On side wall.The rear end of bottom plate 13 is fixed with paddle shaft support plate 16.It is fixed with three pieces and supports between front apron 1 and rear baffle 9 Block 6, has the holding tank 14 that one end opposite position of metal hemming edge 4 no with blade 7 matches in lower supporting block 6, Both ends are respectively fixed with screw rod 11.Holding tank is fixed with rubber protection pad 12 on 14 bottom surface.Upper cover plate 2 with each lower supporting block 6 Corresponding position leans out otic placode 15, and otic placode 15 is being provided with hole with 11 corresponding position of screw rod, and screw rod 11 is placed in hole, by locking Tight nut 10 is fixed.The rubber pad 3 for being wrapped in heating tube or heater strip is fixed with 2 inner wall of upper cover plate.Under bottom plate 13 Face is provided with traveling wheel 8.5 be the electric anti-icing equipment on blade.
Above-described embodiment is only preferable and exemplary, and those skilled in the art can do according to the spirit of this patent Same technological improvement, these are all covered by the protection domain of this patent.

Claims (3)

1. a kind of instrument being glued to metal hemming edge on composite material blade, it include bottom plate, front apron, rear baffle, two pieces More than lower supporting block, paddle shaft support plate, the upper cover plate to match with metal hemming edge inner wall shape, crimp screw rod and nut;Its It is characterized in that:It further includes rubber pad, rubber protection pad, the heating component being wrapped in rubber pad;Front apron is fixed on bottom plate Front end, the one end of upper cover plate away from paddle shaft is supported on its side wall;Rear baffle is fixed on the rear portion of bottom plate, the upper cover plate other end It is supported on its side wall;The rear end of bottom plate is fixed with paddle shaft support plate;More than two pieces are fixed between front apron and rear baffle Lower supporting block, have the receiving that one end opposite position for not having metal hemming edge with blade matches in lower supporting block Groove, both ends are respectively fixed with screw rod;Accommodate and be fixed with rubber protection pad in groove bottom;Upper cover plate is corresponding with each lower supporting block Position lean out otic placode, otic placode is being provided with hole with the corresponding position of screw rod, and screw rod is placed in hole, is compressed by locking nut solid It is fixed;The rubber pad for being wrapped in heating component is fixed with upper cover plate inner wall.
2. the instrument according to claim 1 being glued to metal hemming edge on composite material blade, it is characterised in that:It is described Heating component be heating tube or heater strip.
3. the instrument according to claim 1 or 2 being glued to metal hemming edge on composite material blade, it is characterised in that: The bottom plate is mounted below traveling wheel.
CN201310670457.9A 2013-12-11 2013-12-11 Instrument metal hemming edge being fixed on composite material blade Active CN104712625B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201310670457.9A CN104712625B (en) 2013-12-11 2013-12-11 Instrument metal hemming edge being fixed on composite material blade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201310670457.9A CN104712625B (en) 2013-12-11 2013-12-11 Instrument metal hemming edge being fixed on composite material blade

Publications (2)

Publication Number Publication Date
CN104712625A CN104712625A (en) 2015-06-17
CN104712625B true CN104712625B (en) 2018-05-08

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Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105667830A (en) * 2016-03-08 2016-06-15 哈尔滨飞机工业集团有限责任公司 Pressurizing tool for bonding helicopter main blade front edge wrapping sheet
CN112373052B (en) * 2020-10-21 2022-11-29 武汉理工大学 Gluing method and device for metal wrapping edges of composite material blades
CN113107940B (en) * 2021-04-07 2024-03-19 江苏航运职业技术学院 Multifunctional on-shaft strain gauge pasting tool

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE20013117U1 (en) * 2000-05-18 2001-09-27 Hymer Ag Flap and door attachment on motorhomes
DE102010063076A1 (en) * 2010-12-14 2012-06-14 Airbus Operations Gmbh Fastening arrangement and fastening fitting for attaching a component to a structural component of an aircraft or spacecraft
CN203702781U (en) * 2013-12-11 2014-07-09 惠阳航空螺旋桨有限责任公司 Tool for fixing metal covered edge on composite paddle

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