CN204851336U - Reconditioner casket blade angle's device - Google Patents
Reconditioner casket blade angle's device Download PDFInfo
- Publication number
- CN204851336U CN204851336U CN201520488861.9U CN201520488861U CN204851336U CN 204851336 U CN204851336 U CN 204851336U CN 201520488861 U CN201520488861 U CN 201520488861U CN 204851336 U CN204851336 U CN 204851336U
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- CN
- China
- Prior art keywords
- spheroid
- plectrum
- bolt
- interlock ring
- blade angle
- 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.)
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Abstract
The utility model relates to an aviation field especially relates to a reconditioner casket blade angle's device. The utility model discloses include self -locking nut (4), bolt (5), spheroid (9), bolt (10), plectrum (11) and interlock ring (8), plectrum (11) are fixed on interlock ring (8) through bolt (10), and it is tangent with the external diameter of spheroid (9), spheroid (9) are fixed on quick -witted casket adjustable vane through bolt (5), drive plectrum (11) motion when the motion of interlock ring (8) circumference, plectrum (11) drive spheroid (9), spheroid (9) drive adjustable vane through bolt (5) and rotate, thereby realize the adjustment of adjustable vane angle. The utility model discloses simple structure, the installation is swift, has increased adjustable vane's control range, has avoided the axial motion of the relative gas turbine of interlock ring machine casket, has reduced blade adjusting device's space.
Description
Technical field
The utility model relates to aviation field, particularly relates to a kind of device adjusting casing blade angle.
Background technique
At present, the blade angle-adjustable controlling device of gas turbine mainly contains simple rocking bar regulative mode, this device is the adjustment being carried out blade angle by rocking bar band moving vane, for the structure of simple rocking bar regulative mode, interlock ring not only will carry out circumferential movement, there is the axial motion of relative casing simultaneously, when therefore completing adjustment of blade angle, need larger space; This its complex structure of mode by rocking bar adjusting vane angle, the difficulty adding gas turbine installation and keep in repair, during interlock ring circumferential movement, mechanical wear is very fast, in addition, due to the drawback that adjusting vane angular range is little, then the situation of the adjustment of blade angle scope can not satisfying the demand larger.
Summary of the invention
The purpose of this utility model is to provide a kind of device adjusting casing blade angle, the problem that original controlling device complex structure, required adjustment movement space are comparatively large to solve, gas turbine I&M difficulty is comparatively large, regulating blade angle scope is less.
The technological scheme that the utility model adopts is: provide a kind of device adjusting casing blade angle, includes casing 1, self-locking nut 4, adjustable vane 3, bolt 5, interlock ring 8, spheroid 9, bolt 10 and plectrum 11.Described plectrum 11 one end is provided with ears structure, plectrum 11 is fixed on interlock ring 8 through the through hole on plectrum 11 by bolt 10, described spheroid 9 is connected with adjustable vane 3 by bolt 5, and spheroid 9 is arranged between the ears of plectrum 11, and the ears of the external diameter of spheroid 9 and plectrum 11 are tangent.When needs adjusting vane angle, interlock ring 8 only needs to do circumferential movement, and interlock ring 8 drives plectrum 11 to move, and plectrum 11 is stirred adjustable vane 3 by spheroid 9 and rotated, thus realizes the angular adjustment of adjustable vane 3.In adjustment process, interlock ring 8 only needs to do circumferential movement, saves adjustment space.
Alternatively, described interlock ring 8 is set to " U " type structure, interlock ring 8 connects the position of plectrum 11, is provided with roller bearing core 13 between two side, " U " type structure can alleviate the weight of interlock ring 8, and the effect of support is played in the two side of roller bearing core 13 pairs of interlock rings 8.
Alternatively, on the external diameter of described roller bearing core 13, cover has roller 12, and roller 12 external diameter two ends are provided with boss structure, the groove that two ends boss is formed is stuck on casing 1, when interlock ring 8 does circumferential movement, roller 12 rolls around roller bearing core 13, decreases the mechanical wear of interlock ring 8 and casing 1.
Alternatively, on casing 1 for adjustable vane 3 is installed through hole in can be provided with lining 14, lining 14 one end is provided with boss structure, and the two ends of lining 14 are also provided with pad 6, and lining 14 can reduce mechanical wear when adjustable vane 3 rotates and between casing 1.
Alternatively; lining 7 is provided with between described spheroid 9 and adjustable vane 3; the large external diameter of lining 7 is less than the sphere diameter of spheroid 9; lining 7 can prevent in blade adjustments process; interfere between plectrum 11 and adjustable vane 3; be provided with square washer 2 between self-locking nut 4 and adjustable vane 3, namely square washer 2 can protect adjustable vane 3 from wearing and tearing, again can retaining washer 6.
The beneficial effects of the utility model are, just can realize the regulatory function of blade angle by means of only the circumferential movement of interlock ring; Secondly, the utility model structure is simple, easy for installation, makes the regulation range of blade angle under same space condition, increases more than 1.5 times than original simple rocking bar regulative mode; The utility model also can be applicable in the machinery relevant to turbine structure adjustable vane such as space industry.In addition, the roller in the middle of interlock ring and roller bearing core coordinate cleverly makes the mechanical wear in movement process obtain obvious improvement.
Accompanying drawing explanation
Fig. 1 is the utility model casing adjustment of blade angle device schematic diagram;
Fig. 2 is the utility model casing adjustment of blade angle device sectional view.
Embodiment
Be described in detail of the present utility model below in conjunction with accompanying drawing 1, accompanying drawing 2 and specific embodiment:
Adjust a device for casing blade angle, include casing 1, square washer 2, adjustable vane 3, self-locking nut 4, bolt 5, pad 6, lining 7, interlock ring 8, spheroid 9, bolt 10, plectrum 11, roller 12, roller bearing core 13 and lining 14.Described interlock ring 8 is set to " U " type structure, for connecting the position of plectrum 11 on interlock ring 8, two side is provided with equal-sized coaxial through-hole, be provided with roller bearing core 13 between two side, roller bearing core 13 external diameter cover has roller 12, and roller 12 external diameter two ends are provided with boss structure, two ends boss shape concavity draw-in groove is stuck on casing 1, plectrum 11 is provided with ears structure and screw hole, and bolt 10 is through plectrum 11, roller bearing core 13, interlock ring 8, and the other end is locked by self-locking nut 4.Described spheroid 9 is connected with adjustable vane 3 by screw 5, and spheroid 9 is arranged between the ears of plectrum 11, and the ears of the external diameter of spheroid 9 and plectrum 11 are tangent.Described spheroid 9 is provided with two equal-sized parallel planes, in the central position of plane, line centered by plane normal is processed with through hole, the outer surface of described spheroid 9 is spherical, lining 7 is provided with between spheroid 9 and adjustable vane 3, the large external diameter of lining 7 is less than the sphere diameter of spheroid 9, locked by self-locking nut 4 between bolt 5 and adjustable vane 3, between self-locking nut 4 and adjustable vane 3, be provided with square washer 2; On described casing 1 for adjustable vane 3 is installed hole in lining 14 is installed, described lining 14 one end is provided with boss structure, and the two ends of lining 14 are provided with pad 6.When needs adjusting vane angle, interlock ring 8 only needs to do circumferential movement, and interlock ring 8 drives plectrum 11 to move, and plectrum 11 drives spheroid 9, and spheroid 9 is stirred adjustable vane 3 by bolt 5 and rotated, thus realizes the angular adjustment of adjustable vane 3.In adjustment process, interlock ring 6 only needs to do circumferential movement, saves adjustment space.During interlock ring 6 circumferential movement, roller 12 rolls around roller bearing core 13, and the motion decreased between interlock ring 6 and casing 1 is worn and torn.
The above; be only embodiment of the present utility model; but protection domain of the present utility model is not limited thereto; anyly be familiar with those skilled in the art in the technical scope that the utility model discloses; the change that can expect easily or replacement, all should be encompassed within protection domain of the present utility model.Therefore, protection domain of the present utility model should be as the criterion with the protection domain of described claim.
Claims (6)
1. one kind adjusts the device of casing blade angle, include casing (1), self-locking nut (4), adjustable vane (3), bolt (5), interlock ring (8), spheroid (9), bolt (10) and plectrum (11), it is characterized in that: described plectrum (11) one end is provided with ears structure, plectrum (11) is fixed on interlock ring (8) through the through hole on plectrum (11) by bolt (10), described spheroid (9) is connected with adjustable vane (3) by bolt (5), spheroid (9) is arranged between the ears of plectrum (11), and the ears of the external diameter of spheroid (9) and plectrum (11) are tangent.
2. a kind of device adjusting casing blade angle according to claim 1, it is characterized in that: described spheroid (9) is provided with two equal-sized parallel planes, in the central position of plane, line centered by plane normal is processed with through hole, and the outer surface of described spheroid (9) is spherical.
3. a kind of device adjusting casing blade angle according to claim 1, is characterized in that: described interlock ring (8) is set to " U " type structure.
4. a kind of device adjusting casing blade angle according to claim 1, is characterized in that: the position described interlock ring (8) connecting plectrum (11), is provided with roller bearing core (13) between two side.
5. a kind of device adjusting casing blade angle according to claim 4, is characterized in that: described roller bearing core (13) arranged outside has roller (12), and roller (12) two ends outer radius is provided with boss.
6. a kind of device adjusting casing blade angle according to claim 1, it is characterized in that: between described spheroid (9) and described adjustable vane (3), be provided with lining (7), and the large external diameter of lining (7) is less than the sphere diameter of spheroid (9).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201520488861.9U CN204851336U (en) | 2015-07-08 | 2015-07-08 | Reconditioner casket blade angle's device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201520488861.9U CN204851336U (en) | 2015-07-08 | 2015-07-08 | Reconditioner casket blade angle's device |
Publications (1)
Publication Number | Publication Date |
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CN204851336U true CN204851336U (en) | 2015-12-09 |
Family
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Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN201520488861.9U Active CN204851336U (en) | 2015-07-08 | 2015-07-08 | Reconditioner casket blade angle's device |
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CN (1) | CN204851336U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111103129A (en) * | 2019-12-10 | 2020-05-05 | 西安交通大学 | Turbine cooling rotary table structure with adjustable channel position |
-
2015
- 2015-07-08 CN CN201520488861.9U patent/CN204851336U/en active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111103129A (en) * | 2019-12-10 | 2020-05-05 | 西安交通大学 | Turbine cooling rotary table structure with adjustable channel position |
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