CN105909557A - Fan rotor blade mounting structure - Google Patents

Fan rotor blade mounting structure Download PDF

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Publication number
CN105909557A
CN105909557A CN201610457598.6A CN201610457598A CN105909557A CN 105909557 A CN105909557 A CN 105909557A CN 201610457598 A CN201610457598 A CN 201610457598A CN 105909557 A CN105909557 A CN 105909557A
Authority
CN
China
Prior art keywords
mounting structure
rotor blade
blade
fan
wheel disc
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
CN201610457598.6A
Other languages
Chinese (zh)
Inventor
张岩
印雪梅
马晓健
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.)
AECC Shenyang Engine Research Institute
AVIC Shenyang Engine Design and Research Institute
Original Assignee
AVIC Shenyang Engine Design and Research Institute
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 AVIC Shenyang Engine Design and Research Institute filed Critical AVIC Shenyang Engine Design and Research Institute
Priority to CN201610457598.6A priority Critical patent/CN105909557A/en
Publication of CN105909557A publication Critical patent/CN105909557A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/30Vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/08Sealings
    • F04D29/083Sealings especially adapted for elastic fluid pumps
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/668Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps damping or preventing mechanical vibrations

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The invention discloses a fan rotor blade mounting structure, and relates to the technical field of turbine fan engines. According to the fan rotor blade mounting structure, a rotor blade is mounted on a fan wheel disc (4). The fan rotor blade mounting structure is characterized by comprising a specially-shaped flow path plate (1) and blades (2), wherein the specially-shaped flow path plate (1) is fixedly connected with the fan wheel disc (4), and is used for limiting the blades (2) from vibrating in a circumferential direction of the fan wheel disc (4); the blades (2) are fixedly connected with fan wheel disc (4) through tenons; and the specially-shaped flow path plate (1) and the blades (2) are alternatively arranged in the circumferential direction of the fan wheel disc (4). The fan rotor blade mounting structure has the beneficial effects that: the blades are not provided with edge plates, the specially-shaped flow path plate is arranged between the two adjacent blades, and the specially-shaped flow path plate replaces edge plates on the current blades to position the blades, so that the blades are prevented from vibrating in the circumferential direction of the fan wheel disc, and stress at roots of the blades is reduced.

Description

A kind of fan rotor blade mounting structure
Technical field
The present invention relates to turbofan technical field, be specifically related to a kind of fan rotor blade and knot is installed Structure.
Background technology
Fan blade is one of the most representational strength member of turbofan, directly affects turbine wind The performance of fan engine.In the modern times civilian turbofan of big bypass ratio, it is desired to fan blade is born To a certain degree still keep blade construction integrity after foreign object strike, and meet the requirement in service life, respectively Plant and keep high-caliber performance etc. under working condition.
The end of the eighties, Rolls-Royce company of Britain, GE company of the U.S. and Pu Hui company, SNECMA company of France In succession put into a large amount of human and material resources, financial resources are devoted to the research work of Novel fan vane, low aspect ratio without Convex shoulder fan blade design theory is arisen at the historic moment, and has following irreplaceable advantage: 1. improve fan part Efficiency;2. reduce engine noise;3. improve fan part surge margin 4. and increase anti-foreign object damage ability Deng.
Considering the impact of airload and centrifugal load, low aspect ratio is without convex shoulder fan blade tenon position The problem such as margin of safety deficiency and contact stress height easily occurs.Therefore, how to reduce tenon position load, become For solving the key of problem.
Summary of the invention
It is an object of the invention to provide a kind of fan rotor blade mounting structure, to solve or at least to alleviate background The problem at least one place in the presence of technology.
The technical solution used in the present invention is: provide a kind of fan rotor blade mounting structure, and rotor blade is pacified Being contained on fan wheel disc, described fan rotor blade mounting structure comprises special-shaped stream plate, blade;Described different Type stream plate is fixing with described fan wheel disc to be connected, for limiting described blade in described fan wheel disc circumference Vibration;Described blade is connected by tenon and described fan wheel disc are fixing;Described special-shaped stream plate and described leaf Sheet is alternately arranged in the circumference of described fan wheel disc.
Preferably, described special-shaped stream plate comprises limiting section and connecting portion;Described limiting section and described connecting portion One-body molded, described connecting portion is removably fixing with described fan wheel disc to be connected, described limiting section Both sides are for limiting the vibration of described blade.
Preferably, described special-shaped stream plate also comprises reinforcement;Described limiting section has the interior table being oppositely arranged Face and outer surface, described reinforcement is fixing with the inner surface of described limiting section to be connected, and described reinforcement is provided with Two, two described reinforcements are arranged in the lateral symmetry of described limiting section respectively, the both sides of described limiting section Refer to the side near described special-shaped stream plate both sides blade.
Preferably, described fan rotor blade mounting structure also comprises sealing member;Described reinforcement and described limit Position portion formed holding tank, described sealing member is arranged in described holding tank, and with described blade contact.
Preferably, described sealing member is rubber strip, and described rubber strip comprises the first sealing and the second sealing, Described first sealing is one-body molded with described second sealing, and described first sealing seals with described second Portion's shape has angle, and the summit of described angle is positioned at described holding tank.
Preferably, the limiting section of described special-shaped stream plate is set to arc plate;Described special-shaped stream plate is with described After blade is installed on described fan wheel disc, the side circular arc of described arc plate and described blade opposite flank The circular arc center of circle overlaps.
Preferably, it is provided with gap between side and the side of described blade of described limiting section.
Preferably, described special-shaped stream plate uses aluminium alloy manufacture.
Preferably, the outer surface of described limiting section is arc surface.
The beneficial effects of the present invention is:
In the fan rotor blade mounting structure of the present invention, blade is without listrium, between two adjacent blades Being provided with special-shaped stream plate, special-shaped stream plate replaces the listrium on existing blade to position blade, prevents Blade is in the vibration of fan wheel disc circumference.
Sealing member can reduce main flow area air leakage rate, improves the efficiency of electromotor.Blade can the most more Change.Further, since blade does not exist listrium, reducing the Root Stress of blade, sealing member selects rubber strip, The vibration of blade can also be played cushioning effect.
Accompanying drawing explanation
Fig. 1 is the schematic diagram of the fan rotor blade mounting structure of one embodiment of the invention.
Fig. 2 is the schematic diagram of the special-shaped stream plate in the fan rotor blade mounting structure shown in Fig. 1.
Fig. 3 is special-shaped stream plate and the mounting structure figure of fan wheel disc in embodiment illustrated in fig. 1.
Fig. 4 is special-shaped stream plate and the top view of blade in embodiment illustrated in fig. 1.
Wherein, 1-abnormal shape stream plate, 2-blade, 3-sealing member, 4-fan wheel disc, 11-limiting section, 12- Connecting portion, 13-reinforcement, 14-inner surface, 15-outer surface, 16-side, 31-the first sealing, 32- Second sealing.
Detailed description of the invention
Clearer for the purpose making the present invention implement, technical scheme and advantage, real below in conjunction with the present invention Execute the accompanying drawing in example, the technical scheme in the embodiment of the present invention is further described in more detail.In the accompanying drawings, The most same or similar label represents same or similar element or has same or like function Element.Described embodiment is a part of embodiment of the present invention rather than whole embodiments.Lead to below It is exemplary for crossing the embodiment being described with reference to the drawings, it is intended to be used for explaining the present invention, and it is not intended that right The restriction of the present invention.Based on the embodiment in the present invention, those of ordinary skill in the art are not making creation The every other embodiment obtained under property work premise, broadly falls into the scope of protection of the invention.Below in conjunction with Embodiments of the invention are described in detail by accompanying drawing.
In describing the invention, it is to be understood that term " " center ", " longitudinally ", " laterally ", "front", "rear", "left", "right", " vertically ", " level ", " top ", " end " " interior ", Orientation or the position relationship of the instruction such as " outward " they are based on orientation shown in the drawings or position relationship, merely to It is easy to describe the present invention and simplification description rather than instruction or the device of hint indication or element must have spy Fixed orientation, with specific azimuth configuration and operation, therefore it is not intended that limit to scope System.
As shown in Figures 1 to 4, a kind of fan rotor blade mounting structure, rotor blade is arranged on fan wheel On dish 4, fan rotor blade mounting structure comprises special-shaped stream plate 1, blade 2;Special-shaped stream plate 1 with Fan wheel disc 4 is fixing to be connected, for limiting the blade 2 vibration in fan wheel disc 4 circumference;Blade 2 passes through Tenon is fixing with fan wheel disc 4 to be connected;Special-shaped stream plate 1 replaces in the circumference of fan wheel disc 4 with blade 2 Arrange.
In the fan rotor blade mounting structure of the present invention, blade 2 without listrium, two adjacent blades 2 Between be provided with special-shaped stream plate 1, special-shaped stream plate 1 replaces the listrium on existing blade to carry out blade 2 Location, prevents blade 2 in the vibration of fan wheel disc 4 circumference.Owing to blade 2 does not exist listrium, reduce The Root Stress of blade 2.
In the present embodiment, special-shaped stream plate 1 comprises limiting section 11 and connecting portion 12;Limiting section (11) One-body molded with connecting portion 12, connecting portion 12 is removably fixing with fan wheel disc 4 to be connected, spacing The both sides in portion 11 are for limiting the vibration of blade 2.
In the present embodiment, special-shaped stream plate 1 also comprises reinforcement 13;Limiting section 11 has and is oppositely arranged Inner surface 14 and outer surface 15, the inner surface 14 of reinforcement 13 and limiting section 11 is fixing to be connected, and adds Strong muscle 13 is provided with two, and two reinforcements 13 are arranged in the lateral symmetry of limiting section 11 respectively, spacing The both sides in portion 11 refer to the side 16 near special-shaped stream plate 1 both sides blade 2.Reinforcement 13 is set Advantage is, it is possible to alleviate the thickness of limiting section 11, utilizes reinforcement 13 to ensure special-shaped stream plate 1 simultaneously Intensity, be conducive to alleviating the weight of special-shaped stream plate 1.
In the present embodiment, reinforcement 13 is one-body molded with limiting section 11, and reinforcement 13 and limiting section The junction of 11 is provided with fillet, has an advantage in that, reduces the stress of junction.It is understood that The fillet of the junction of reinforcement 13 and limiting section 11 should be greater than the thickness of reinforcement 13, it is possible to preferably Solid line alleviates the purpose of stress.
In the present embodiment, connecting portion 12 is arranged on inner surface 14, and to the side away from inner surface 14 Being provided with connecting hole in extension, connecting portion 12, connecting portion is by bolt, self-locking nut and fan wheel disc 4 fixing connections.Can stand and be understood by, the connecting portion 12 on a special-shaped stream plate 1 should at least set It is equipped with two, has an advantage in that, it is possible to be completely fixed special-shaped stream plate 1.In the present embodiment, special-shaped stream 3 connecting portions 12 it are provided with on road plate 1.
In the present embodiment, fan rotor blade mounting structure also comprises sealing member 3;Reinforcement 13 and limit Position portion 11 forms holding tank, and sealing member 3 is arranged in holding tank, and contacts with blade 2.
In the present embodiment, sealing member 3 is rubber strip, and it is close that rubber strip comprises the first sealing 31 and second Envelope portion 32, the first sealing 31 is one-body molded with the second sealing 32, and the first sealing 31 is close with second Envelope portion 32 shape has angle, and the summit of described angle is positioned at described holding tank.Have an advantage in that, rubber Bar has certain elasticity, is possible not only to play the effect of sealing, it is also possible to play the effect of bumper and absorbing shock. When blade 2 vibrates, first blade 2 extrudes rubber strip, and rubber strip is by compression, when due to blade 2 Oscillation Amplitude relatively big, when rubber strip is compressed to a certain degree, the side of blade 2 and special-shaped stream plate 1 On the side 16 of limiting section 11 contact, limit the vibration of blade 2.Due to the cushioning effect of rubber strip, Impact force when blade 2 contacts with the side 16 of the limiting section 11 on special-shaped stream plate 1 is less, can keep away Exempt from blade 2 is caused damage.
In the present embodiment, the advantage that the first sealing 31 of rubber strip and the second sealing 32 arrange angle It is, it is possible to the compression for rubber strip leaves certain deformation space, plays more preferable cushioning effect.
In the present embodiment, special-shaped stream plate 1 and blade 2 form the stream of electromotor, and special-shaped stream It is provided with sealing member 3 between plate 1 and blade 2, the leakage of air-flow can be alleviated, improve the efficiency of electromotor.
Because fan rotor blade 2 bending is violent, root is particularly evident, and the structure of special-shaped stream plate 1 needs therewith Adapting, by special-shaped stream plate 1 and blade 2 matching part analysis, fan rotor blade 2 circular arc enters Row Fitting Analysis, determines that two sides are and the circular arc of fan rotor blade matching part approximation iso-curvature change Type structure, both sides are reserved certain gap respectively, are met engine assembly and fan blade is independent the most more with blade The requirement changed.
In the present embodiment, the limiting section 11 of special-shaped stream plate 1 is set to arc plate;Special-shaped stream plate 1 After installing on fan wheel disc 4 with blade 2, the side circular arc of described arc plate and blade 2 opposite flank The circular arc center of circle overlaps (as shown in Figure 4).
In the present embodiment, it is provided with gap between side 16 and the side of blade 2 of limiting section 11.Its Advantage is, first disclosure satisfy that the demand that blade 2 is individually replaced, furthermore it is possible to be the vibration of blade 2 Leave certain cushion space, under the effect of sealing member, realize the buffering of blade vibration, prevent blade 2 Directly collide with limiting section 11.
In the present embodiment, the outer surface 15 of limiting section 11 is arc surface.Have an advantage in that, the most permissible Increase the intensity of special-shaped stream plate 1, furthermore it is possible to alleviate the resistance of air-flow in stream.
In the present embodiment, special-shaped stream plate 1 uses aluminium alloy manufacture.Have an advantage in that, it is possible, firstly, to Reducing the weight of special-shaped stream plate 1, further, since special-shaped stream plate 1 is irregular structure, aluminium alloy adds Work is convenient, is more suitable for the processing and manufacturing to special-shaped stream plate 1.
Last it is noted that above example is only in order to illustrate technical scheme, rather than to it Limit.Although the present invention being described in detail with reference to previous embodiment, the ordinary skill people of this area Member is it is understood that the technical scheme described in foregoing embodiments still can be modified by it or right Wherein portion of techniques feature carries out equivalent;And these amendments or replacement, do not make appropriate technical solution Essence depart from various embodiments of the present invention technical scheme spirit and scope.

Claims (9)

1. a fan rotor blade mounting structure, rotor blade is arranged on fan wheel disc (4), and it is special Levy and be: described fan rotor blade mounting structure comprises special-shaped stream plate (1), blade (2);Described Special-shaped stream plate (1) is fixing with described fan wheel disc (4) to be connected, and is used for limiting described blade (2) and exists The vibration of described fan wheel disc (4) circumference;
Described blade (2) is connected by tenon and described fan wheel disc (4) are fixing;
Described special-shaped stream plate (1) replaces in the circumference of described fan wheel disc (4) with described blade (2) Arrange.
2. fan rotor blade mounting structure as claimed in claim 1, it is characterised in that: described abnormal shape Stream plate (1) comprises limiting section (11) and connecting portion (12);Described limiting section (11) and described company Meeting portion (12) one-body molded, described connecting portion (12) is with described fan wheel disc (4) removably Fixing connection, the both sides of described limiting section (11) are used for limiting the vibration of described blade (2).
3. fan rotor blade mounting structure as claimed in claim 2, it is characterised in that: described abnormal shape Stream plate (1) also comprises reinforcement (13);Described limiting section (11) has the inner surface being oppositely arranged (14) and outer surface (15), the inner surface (14) of described reinforcement (13) and described limiting section (11) Fixing connection, described reinforcement (13) is provided with two, and two described reinforcements (13) are respectively described The lateral symmetry of limiting section (11) is arranged, the both sides of described limiting section (11) refer near described special-shaped stream The side (16) on road plate (1) both sides blade (2).
4. fan rotor blade mounting structure as claimed in claim 3, it is characterised in that: described fan Rotor blade mounting structure also comprises sealing member (3);Described reinforcement (13) and described limiting section (11) Forming holding tank, described sealing member (3) is arranged in described holding tank, and contacts with described blade (2).
5. fan rotor blade mounting structure as claimed in claim 4, it is characterised in that: described sealing Part (3) is rubber strip, and described rubber strip comprises the first sealing (31) and the second sealing (32), Described first sealing (31) is one-body molded with described second sealing (32), described first sealing (31) Having angle with described second sealing (32) shape, the summit of described angle is positioned at described holding tank.
6. fan rotor blade mounting structure as claimed in claim 4, it is characterised in that: described abnormal shape The limiting section (11) of stream plate (1) is set to arc plate;Described special-shaped stream plate (1) and described blade (2) after the upper installation of described fan wheel disc (4), the side circular arc of described arc plate and described blade (2) The circular arc center of circle of opposite flank overlaps.
7. fan rotor blade mounting structure as claimed in claim 4, it is characterised in that: described spacing It is provided with gap between side (16) and the side of described blade (2) in portion (11).
8. fan rotor blade mounting structure as claimed in claim 2, it is characterised in that: described spacing The outer surface (15) in portion (11) is arc surface.
9. the fan rotor blade mounting structure as described in any one of claim 1 to 8, it is characterised in that: Described special-shaped stream plate (1) uses aluminium alloy manufacture.
CN201610457598.6A 2016-06-21 2016-06-21 Fan rotor blade mounting structure Pending CN105909557A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610457598.6A CN105909557A (en) 2016-06-21 2016-06-21 Fan rotor blade mounting structure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610457598.6A CN105909557A (en) 2016-06-21 2016-06-21 Fan rotor blade mounting structure

Publications (1)

Publication Number Publication Date
CN105909557A true CN105909557A (en) 2016-08-31

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ID=56758254

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610457598.6A Pending CN105909557A (en) 2016-06-21 2016-06-21 Fan rotor blade mounting structure

Country Status (1)

Country Link
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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110285093A (en) * 2018-02-19 2019-09-27 通用电气公司 For promoting the platform device of rotor
CN112943381A (en) * 2021-03-17 2021-06-11 中国航发动力股份有限公司 Protection device for be used for taking assembly of convex shoulder rotor blade
CN114321006A (en) * 2020-09-29 2022-04-12 中国航发商用航空发动机有限责任公司 Fan runner plate, deformation control method thereof and fan

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3712757A (en) * 1969-10-28 1973-01-23 Secr Defence Bladed rotors for fluid flow machines
US6217283B1 (en) * 1999-04-20 2001-04-17 General Electric Company Composite fan platform
CN1398322A (en) * 2000-02-09 2003-02-19 西门子公司 Turbine blade arrangement
US6634863B1 (en) * 2000-11-27 2003-10-21 General Electric Company Circular arc multi-bore fan disk assembly
CN1651746A (en) * 2004-01-21 2005-08-10 通用电气公司 Methods and apparatus for assembling gas turbine engines
EP1881160A2 (en) * 2006-07-22 2008-01-23 Rolls-Royce plc Seal for an annulus filler between fan blades
WO2014140449A1 (en) * 2013-03-15 2014-09-18 Snecma Multiflow turbojet engine fan and turbojet engine fitted with such a fan

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3712757A (en) * 1969-10-28 1973-01-23 Secr Defence Bladed rotors for fluid flow machines
US6217283B1 (en) * 1999-04-20 2001-04-17 General Electric Company Composite fan platform
CN1398322A (en) * 2000-02-09 2003-02-19 西门子公司 Turbine blade arrangement
US6634863B1 (en) * 2000-11-27 2003-10-21 General Electric Company Circular arc multi-bore fan disk assembly
CN1651746A (en) * 2004-01-21 2005-08-10 通用电气公司 Methods and apparatus for assembling gas turbine engines
EP1881160A2 (en) * 2006-07-22 2008-01-23 Rolls-Royce plc Seal for an annulus filler between fan blades
WO2014140449A1 (en) * 2013-03-15 2014-09-18 Snecma Multiflow turbojet engine fan and turbojet engine fitted with such a fan

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110285093A (en) * 2018-02-19 2019-09-27 通用电气公司 For promoting the platform device of rotor
US10738630B2 (en) 2018-02-19 2020-08-11 General Electric Company Platform apparatus for propulsion rotor
CN114321006A (en) * 2020-09-29 2022-04-12 中国航发商用航空发动机有限责任公司 Fan runner plate, deformation control method thereof and fan
CN112943381A (en) * 2021-03-17 2021-06-11 中国航发动力股份有限公司 Protection device for be used for taking assembly of convex shoulder rotor blade

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Application publication date: 20160831