CN204716303U - Combined type blade root - Google Patents

Combined type blade root Download PDF

Info

Publication number
CN204716303U
CN204716303U CN201520201755.8U CN201520201755U CN204716303U CN 204716303 U CN204716303 U CN 204716303U CN 201520201755 U CN201520201755 U CN 201520201755U CN 204716303 U CN204716303 U CN 204716303U
Authority
CN
China
Prior art keywords
movable block
combined type
blade root
fixed block
blade
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.)
Active
Application number
CN201520201755.8U
Other languages
Chinese (zh)
Inventor
陈海燕
刘丙权
崔娟
袁善虎
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 Huatsing Gas Turbine and IGCC Technology Co Ltd
Original Assignee
Beijing Huatsing Gas Turbine and IGCC Technology 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 Beijing Huatsing Gas Turbine and IGCC Technology Co Ltd filed Critical Beijing Huatsing Gas Turbine and IGCC Technology Co Ltd
Priority to CN201520201755.8U priority Critical patent/CN204716303U/en
Application granted granted Critical
Publication of CN204716303U publication Critical patent/CN204716303U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Abstract

The utility model relates to the antivibration area of blade or cantilever type rotational structure, provides a kind of combined type blade root.This combined type blade root comprises fixed block and movable block, and the top of described fixed block is used for being connected with blade, and bottom is provided with the first assembly department and is opened in the slot on described first assembly department; The bottom of described movable block is provided with the second assembly department, and described movable block activity is inserted in described slot, and and leave gap between the inwall of described slot; Described first assembly department and the second assembly department are all for being connected with wheel disc.When blade by vibration passing to blade root body and fixed block time, owing to there is gap between fixed block and movable block,, there is not resonance between movable block and fixed block, avoid blade and produce excessive amplitude in the absorbing vibrational energy by the friction between movable block and fixed block.

Description

Combined type blade root
Technical field
The utility model relates to the antivibration area of blade or cantilever type rotational structure, provides a kind of combined type blade root especially.
Background technique
The damage accident of rotating machinery blade (crackle, fracture), the overwhelming majority causes due to vibration.Rotor blade receives powerful centrifugal force load, adds the alternate load that Airflow Exciting-Vibration Force causes, and after work certain hour, easily causes vibrating fatigue, produces fatigue crack.
Vibration frequency is the important parameter of blade design, usually requires that the integral multiple of Natural Frequency of Blade and working speed has and certain avoids rate, avoid resonance.Relative integers choosing doubly is relevant with the factor such as irregular, the air cylinder structure form of the number of blade adjacent structure, air inlet runner.
In order to ensure Security, according to calculating and the measurement of frequency, estimate and judge the situation of vibration.But affect by the factor such as fit up gap, material behavior dispersiveness, machining error of leaf temperature field, blade root and wheel disc, theory calculate is difficult to the actual frequency calculating blade accurately.And to be tested processes monitoring blade frequencies of doing experiment, once find that blade can not meet frequency and avoid rate demand, in order to not affect aeroperformance, substantially can not adjust vane thickness, revising movable vane forward and backward level stator blade number simultaneously and also not too realizing.Best feasible method is the frequency changing blade self, namely needs to design the whole blade of a kind of frequency-adjustable, can conveniently tune to open the blade natural frequency of vibration, avoids resonance when making it run.
Integral shroud linear leaf is usually through arranging vibration damping boss, and utilize shroud (integral shroud), lacing wire etc. to increase damping, change shroud and lacing wire size are adjusted frequency.But for not shrouded blade, except changing vane thickness and blade integral material, available adjustment vibration frequency means are few.And change material and also need whole blade again manufacturing.
Model utility content
(1) technical problem that will solve
The purpose of this utility model is to provide a kind of combined type blade root and blade, under the prerequisite not affecting aeroperformance, realizes the adjustment of himself frequency and vibration damping fast.
(2) technological scheme
For achieving the above object, the utility model provides a kind of combined type blade root, it is characterized in that, comprising:
Fixed block, the top of described fixed block is used for being connected with blade, and bottom is provided with the first assembly department and is opened in the slot on described first assembly department; With
Movable block, the bottom of described movable block is provided with the second assembly department, and described movable block activity is inserted in described slot, and and leave gap between the inwall of described slot;
Described first assembly department and the second assembly department are all for being connected with wheel disc.
Preferably, the inwall of described slot offers draw-in groove; The outer wall of described movable block is provided with inserted part, described inserted part and described draw-in groove snap-fit engagement.
Preferably, the outer wall of described second assembly department is provided with the moat face of inner concavity, fills out and be provided with damping material in described moat face.
Preferably, described damping material is damping glue.
Preferably, described slot and movable block are all from top to bottom in gradually closing formula structure.
Preferably, described slot and movable block are swallow-tail form.
Preferably, described fixed block and/or described movable block offer packing groove vertically, in described packing groove, is filled with damping material.
Preferably, the material of described movable block is different from the material of described fixed block.
Preferably, the outer wall of described second assembly department is provided with wearing layer.
Preferably, described wearing layer is shot-peening layer.
(3) beneficial effect
The utility model provides a kind of combined type blade root, comprises fixed block and movable block, and the top of fixed block is for connecting blade, bottom is used for being connected with wheel disc, the bottom of fixed block is also provided with slot, and movable block activity is inserted in this slot, and has gap between movable block and slot.When blade by vibration passing to blade root body and fixed block time, owing to there is gap between fixed block and movable block, thus by the friction between movable block and fixed block absorbing vibrational energy, there is not resonance between movable block and fixed block, thus avoid blade and produce excessive amplitude.The utility model adds the flexibility that blade design manufactures.Without the need to redesigning blade profile or changing contiguous structure form, the adjustment of the blade natural frequency of vibration is realized quickly and easily by adjustment movable block material, movable block and the fit form of fixed block, the damping glue thickness of movable block, reduce the difficulty of blade design, improve the Security of blade vibration.
Accompanying drawing explanation
Fig. 1 is the blade of the utility model embodiment one and the schematic diagram of fixed block;
Fig. 2 is the schematic diagram of the movable block of the utility model embodiment one;
Fig. 3 is a kind of combined type blade root of the utility model embodiment one and the schematic diagram of blade;
Fig. 4 is the blade of the utility model embodiment two and the schematic diagram of fixed block;
Fig. 5 is the schematic diagram of the movable block of the utility model embodiment two;
Fig. 6 is a kind of combined type blade root of the utility model embodiment two and the schematic diagram of blade;
Fig. 7 is the blade of the utility model embodiment three and the schematic diagram of fixed block;
Fig. 8 is the schematic diagram of the movable block of the utility model embodiment three;
Fig. 9 is a kind of combined type blade root of the utility model embodiment three and the schematic diagram of blade.
Reference character:
1, blade; 2, slot; 3, movable block; 4, fixed block; 21, the first working surface; 22, the second working surface; 23, inserted part; 24, draw-in groove; 25, damping material.
Embodiment
Below in conjunction with drawings and Examples, embodiment of the present utility model is described in further detail.Following examples for illustration of the utility model, but are not used for limiting scope of the present utility model.
In description of the present utility model, except as otherwise noted, term " on ", D score, " top ", " bottom ", the orientation of the instruction such as " longitudinal direction " or state relation be based on orientation shown in the drawings or state relation, only the utility model and simplified characterization for convenience of description, instead of the device of instruction or hint indication or element must have specific orientation, with specific azimuth configuration and operation, therefore can not be interpreted as restriction of the present utility model.
In description of the present utility model, it should be noted that, unless otherwise clearly defined and limited, term " connection " should be interpreted broadly, and such as, can be fixedly connected with, also can be removably connect, or connect integratedly; Can be directly be connected, also indirectly can be connected by intermediary.For the ordinary skill in the art, concrete condition the concrete meaning of above-mentioned term in the utility model can be understood.
Embodiment one
Shown in composition graphs 1 to Fig. 3, a kind of combined type blade root that the utility model embodiment one provides, comprises fixed block 4 and movable block 3, and the top of fixed block 4 is used for fixing blade; The bottom of described fixed block 4 has the first assembly department to two radial side projections and the slot 2 that is opened on described first assembly department, and described first assembly department is used for the first working surface 21 by its two radial side and wheel disc clamping; The activity of described movable block 3 is inserted in described slot 2, and movable block 3 can be the multiple of dual extension-compression modulus, selects the movable block 3 of suitable Young's modulus according to frequency reducing or raising frequency demand; Between the axial both sides of described fixed block 4 and the inwall of slot 2, there is gap, the bottom of described movable block 3 has the second assembly department to two radial side projections, described second assembly department is used for the second working surface 22 and described wheel disc clamping by its two radial side, wherein, the second working surface 22 is concordant with the normal direction of the first working surface 21.
When blade 1 by vibration passing to fixed block 4 time, because movable block 3 and fixed block 4 are not integral structure, and between fixed block 4 and movable block 3, there is gap, thus by friction between movable block 3 and fixed block 4 absorbing vibrational energy, movable block 3 is not vibrated with fixed block 4 same frequency, namely there is not resonance between movable block 3 and fixed block 4, thus avoid blade 1 and produce excessive amplitude.
Can realize diametrically spacing between movable block 3 and fixed block 4 by means of only the connection with wheel disc, but preferably all offer draw-in groove 24 on the top of slot 2, the inserted part 23 of evagination is all set in the axial both sides of described movable block 3, described inserted part 23 and described draw-in groove 24 snap-fit engagement, thus realize movable block 3 and fixed block 4 relative limit in the vertical.Thus, when mounted, first movable block 3 can be installed in slot 2, then be connected with wheel disc again, therefore facilitate installation.
By testing or calculate the frequency determining the not combined blade 1 identical with blade material, and record this value; According to the size of vibrating source frequency, the movable block 3 of processing different materials (Young's modulus or density difference) coordinates with fixed block 4.The system of selection of movable block 3 material: in order to improve the frequency of blade 1, can make movable block 3 select the material that Young's modulus is comparatively large or density is less; Otherwise, in order to reduce the frequency of blade 1, movable block 3 can be made to select the material that Young's modulus is less or density is larger.
Wherein, the material of described movable block 3 is different from the material of described fixed block 4, and namely the movable block 3 and fixed block 4 of unlike material itself have different vibration frequency characteristics, can promote with this effect absorbing vibration frequency.
Wherein, movable block 3 because of vibration can the axial changing of the relative positions, thus and produce between wheel disc and rub more frequently, therefore wearing layer can be set at the second working surface 22, to reduce wearing and tearing, the shot-peening layer that described wearing layer is formed preferably by shot blast; Certainly, the first working surface 21 of fixed block 4 also can arrange wearing layer.
Embodiment two
Shown in composition graphs 4 to Fig. 6, a kind of combined type blade root that the present embodiment two provides, substantially identical with the structure of embodiment one, something in common repeats no more, and difference is:
Described second working surface 22 is provided with the moat face compared with the first working surface 21 indent, fill out in described moat face and be provided with damping material 25, this damping material 25 can be damping glue, and this damping material 25 also can absorbing vibrational energy to a certain extent, realizes the adjustment of vibration frequency further.
Embodiment three
Shown in composition graphs 7 to Fig. 9, a kind of combined type blade root that the present embodiment three provides, substantially identical with the structure of embodiment two, something in common repeats no more, and difference is:
The axial both sides of the both sides that slot 2 is relative and described movable block 3 are from top to bottom all in gradually closing formula structure, namely the both sides that fixed block 4 is relative and the axial both sides of described movable block 3 are all in inverted dovetail shaped, movable block 3 by its axial both sides top-down gradually closing formula structure installment in the overall slot 2 formed in inverted trapezoidal structure equally from top to bottom, by changing the movable block 3 with the second assembly department of different relative position height, regulate the height of movable block 3 in slot 2, and then realize the adjustment in gap between the both sides of movable block 3 and fixed block 4, realize the adjustment of vibration frequency thus.
In addition, also on described fixed block 4 and/or movable block 3, packing groove can be offered vertically, in described packing groove, be filled with damping material, play the effect regulating vibration frequency further.
Combination blade root constructional of the present utility model, by the design that movable block 3 coordinates with fixed block 4, damping, contact stiffness and mass distribution can be adjusted easily, friction Absorbable rod vibrational energy simultaneously between movable block 3, blade 1 frequency modulation can be realized fast, add the vibration safety of blade 1, reduce design risk, do not need repeatedly to design blade 1 profile and thickness, improve design efficiency.
The above is only preferred implementation of the present utility model; should be understood that; for those skilled in the art; under the prerequisite not departing from the utility model know-why; can also make some improvement and replacement, these improve and replace and also should be considered as protection domain of the present utility model.

Claims (10)

1. a combined type blade root, is characterized in that, comprising:
Fixed block (4), the top of described fixed block (4) is used for being connected with blade (1), and bottom is provided with the first assembly department and is opened in the slot (2) on described first assembly department; With
Movable block (3), the bottom of described movable block (3) is provided with the second assembly department, and described movable block (3) activity is inserted in described slot (2), and and leave gap between the inwall of described slot (2);
Described first assembly department and the second assembly department are all for being connected with wheel disc.
2. combined type blade root according to claim 1, is characterized in that, the inwall of described slot (2) offers draw-in groove (24); The outer wall of described movable block (3) is provided with inserted part (23), described inserted part (23) and described draw-in groove (24) snap-fit engagement.
3. combined type blade root according to claim 2, is characterized in that, the outer wall of described second assembly department is provided with the moat face of inner concavity, fills out and be provided with damping material (25) in described moat face.
4. combined type blade root according to claim 3, is characterized in that, described damping material (25) is damping glue.
5. combined type blade root according to claim 1, is characterized in that, described slot (2) and movable block (3) are all from top to bottom all in gradually closing formula structure.
6. combined type blade root according to claim 5, is characterized in that, described slot (2) and movable block (3) are swallowtail-shaped structure.
7. combined type blade root according to claim 5, is characterized in that, described fixed block (4) and/or described movable block (3) offers packing groove vertically, is filled with damping material in described packing groove.
8. the combined type blade root according to any one of claim 1 to 7, is characterized in that, the material of described movable block (3) is different from the material of described fixed block (4).
9. the combined type blade root according to any one of claim 1 to 7, is characterized in that, the outer wall of described second assembly department is provided with wearing layer.
10. combined type blade root according to claim 9, is characterized in that, described wearing layer is shot-peening layer.
CN201520201755.8U 2015-04-03 2015-04-03 Combined type blade root Active CN204716303U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201520201755.8U CN204716303U (en) 2015-04-03 2015-04-03 Combined type blade root

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201520201755.8U CN204716303U (en) 2015-04-03 2015-04-03 Combined type blade root

Publications (1)

Publication Number Publication Date
CN204716303U true CN204716303U (en) 2015-10-21

Family

ID=54315306

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201520201755.8U Active CN204716303U (en) 2015-04-03 2015-04-03 Combined type blade root

Country Status (1)

Country Link
CN (1) CN204716303U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104912603A (en) * 2015-04-03 2015-09-16 北京华清燃气轮机与煤气化联合循环工程技术有限公司 Combined blade root

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104912603A (en) * 2015-04-03 2015-09-16 北京华清燃气轮机与煤气化联合循环工程技术有限公司 Combined blade root

Similar Documents

Publication Publication Date Title
Williams Simulation of blade casing interaction phenomena in gas turbines resulting from heavy tip rubs using an implicit time marching method
US8186057B2 (en) Bladed rotor balancing
AU2013354038B2 (en) Rotor blade trailing edge
CN104568351B (en) Damping-structure-optimized blade testing experiment table and experimental method thereof
CN102132047B (en) Turbine blade and gas turbine
ATE550520T1 (en) VIBRATION DAMPERS FOR TURBO MACHINE BLADES, ASSOCIATED TURBO MACHINE AND ASSOCIATED MOTORS
RU2580447C2 (en) Blades system and appropriate gas turbine
US20140161617A1 (en) Bladed rotor wheel for a turbine engine
US20140348657A1 (en) Turbomachine blade
US9869621B2 (en) Test bench combining high-frequency tribological stress and oligocyclic fatigue, on a blade disk of turboshaft engine of an aircraft including a test piece having a portion with a shape of a blade root of a rotor and is engaged in a groove shape complementary to another test piece
RU2013105207A (en) TURBINE UNIT (OPTIONS) AND METHOD FOR CHANGING THE FREQUENCY OF OWN OSCILLATIONS OF A TURBINE UNIT
CN204716303U (en) Combined type blade root
EP3138999B1 (en) Damper pin for damping adjacent turbine blades and turbine engine
CN104912603A (en) Combined blade root
CN110909433A (en) Gas turbine compressor rotor fir-shaped tenon-mortise connection structure optimization method
JP6278447B2 (en) Liquid damper and rotary machine blade provided with the same
CN113605993A (en) High-pressure turbine moving blade set with damping vibration attenuation blocks
JP2015148287A (en) Liquid damper and rotary machine blade including the same
CN109522592A (en) A kind of blade of aviation engine FOD, which permits, to be repaired the limit and determines method
JP6151932B2 (en) Damping member for rotating machinery
JP6280769B2 (en) Rotor blade and rotating machine
CN109614739A (en) A kind of novel nonlinear contact processing method for shrouded blade
CN203856517U (en) Steam turbine internal cylinder capable of measuring dynamic and static clearance
JP2019528401A (en) Operation load setting method, tower structure design method, tower structure and wind turbine
EP1890006A1 (en) Rotor with a vibrational damper for a turbomachine

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
PE01 Entry into force of the registration of the contract for pledge of patent right

Denomination of utility model: Combined blade root

Effective date of registration: 20161104

Granted publication date: 20151021

Pledgee: Tsinghua Holdings Co., Ltd.

Pledgor: Beijing Huatsing Gas Turbine & IGCC Technology Co., Ltd.

Registration number: 2016990000853

PLDC Enforcement, change and cancellation of contracts on pledge of patent right or utility model
PC01 Cancellation of the registration of the contract for pledge of patent right

Date of cancellation: 20191211

Granted publication date: 20151021

Pledgee: Tsinghua Holdings Co., Ltd.

Pledgor: Beijing Huatsing Gas Turbine & IGCC Technology Co., Ltd.

Registration number: 2016990000853

PC01 Cancellation of the registration of the contract for pledge of patent right