CN109292039B - A kind of installation method of distance-adjustable oar hub - Google Patents
A kind of installation method of distance-adjustable oar hub Download PDFInfo
- Publication number
- CN109292039B CN109292039B CN201810802864.3A CN201810802864A CN109292039B CN 109292039 B CN109292039 B CN 109292039B CN 201810802864 A CN201810802864 A CN 201810802864A CN 109292039 B CN109292039 B CN 109292039B
- Authority
- CN
- China
- Prior art keywords
- blade
- blade root
- crank disc
- root bolt
- bolt
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B71/00—Designing vessels; Predicting their performance
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H3/00—Propeller-blade pitch changing
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The invention discloses a kind of installation methods of distance-adjustable oar hub, belong to tuning for Controllable Pitch Propeller technical field.By before blade and crank disc are assembled in paddle shell, first crank disc is fixed on a platform, one positioning ring is set on crank disc, blade and crank disc are bolted by blade root again, wherein positioning ring is substituted for bearer ring, to simulate blade and crank disc after being assembled in paddle shell, since the screw-down torque of blade root bolt is larger, the case where rear blade can be deformed is tightened.Then blade axial direction gap width h at this time is measured, and according to the axial length of blade axial direction gap width h, positioning ring be t and blade axial gap setting value H, the axis axial length D of bearer ring is calculated, and the axis axial length of the intracorporal bearer ring of paddle shell is processed to D, finally blade and crank disc are assembled in paddle shell, make bearer ring between blade and crank disc.Blade axial direction gap width is within the scope of setting value H after the installation method can guarantee installation.
Description
Technical field
The present invention relates to tuning for Controllable Pitch Propeller technical field, in particular to a kind of installation method of distance-adjustable oar hub.
Background technique
The working principle of adjustable pitch propeller (abbreviation tuning for Controllable Pitch Propeller) is to drive propeller hub oil cylinder, Jin Ertong by hydraulic system
Crossing the crank-slide block mechanism being arranged in propeller hub mechanism makes blade around the axis rotation perpendicular to paddle shaft, thus change screw pitch,
Realize speed change, positive vehicle and the reversing of ship.
In tuning for Controllable Pitch Propeller, crank disc is mounted in the inner cavity of paddle shell, and blade is connected as by blade root bolt with crank disc
One, the inner wall of paddle shell are equipped with a circle bearer ring, and bearer ring is between blade and the connector of crank disc, and bearer ring
Separate crank disc end face and blade close crank disc end face between have a gap, this gap is called blade axial direction
Gap.
In the implementation of the present invention, the inventor finds that the existing technology has at least the following problems:
The size of blade axial gap is related with blade, crank disc, the relative dimensions of three parts of paddle shell, in practical peace
During dress, since the screw-down torque of blade root bolt is larger, tightening rear blade can be deformed, this will lead to actual paddle shaft
It is less than to gap width and resulting blade axial direction gap width is calculated according to the size of part.And blade shafting gap width is too small, can lead
Cause the failure of tuning for Controllable Pitch Propeller displacement.If by the excessive of blade axial direction gap width setting, and will lead to and let out between blade and bearer ring
Leakage, seriously affects the propulsive performance of ship.
Summary of the invention
The embodiment of the invention provides a kind of installation methods of distance-adjustable oar hub, it is ensured that distance-adjustable oar hub is being installed
Afterwards, blade axial direction gap width is in range of set value.The technical solution is as follows:
The embodiment of the invention provides a kind of installation method of distance-adjustable oar hub, the distance-adjustable oar hub include paddle shell,
Crank disc and blade, the paddle shell are equipped with mounting hole, and the inner wall of the mounting hole is equipped with bearer ring, the bearer ring
Axis is overlapped with the axis of the mounting hole, and an end face of the crank disc is equipped with the first rotary table, first rotary table and institute
Crank disc coaxial arrangement is stated, an end face of the blade is equipped with the second rotary table, and second rotary table is coaxially set with the blade
It sets, the internal diameter of the bearer ring matches with the outer diameter of first rotary table and the outer diameter of second rotary table, the installation side
Method includes:
The crank disc is fixed on platform;
Positioning ring is set on the crank disc, and the positioning ring is set in outside first rotary table, the positioning ring
The outer diameter of internal diameter and first rotary table matches;
The blade is bolted with the crank disc by blade root, the positioning ring is made to be set in second rotary table
Outside, the internal diameter of the positioning ring and the outer diameter of second rotary table match, and the positioning ring is arranged in the blade and institute
It states between crank disc, the axial length of the positioning ring is t;
Blade axial direction gap width h is measured, the blade axial direction gap width is the positioning ring far from the crank disc
End face to the distance between the end face close to the crank disc of the blade;
The bearer ring is processed, making the axial length D, D=t+h-H, H of the bearer ring is the blade axial gap
Setting value;
The blade, the positioning ring and the crank disc are successively dismantled;
The blade is bolted with the crank disc by blade root in the paddle shell, is arranged the bearer ring
Outside first rotary table and second rotary table, and the bearer ring is between the blade and the crank disc.
It is further, described that the crank disc is fixed on platform, comprising:
Positioning plate is fixed on the platform, and the positioning plate is equipped with a circle seam allowance, the outer diameter of the seam allowance and institute
The outer diameter for stating crank disc matches, and the crank-pin to match with the crank-pin on the crank disc is additionally provided on the positioning plate and is pacified
Fill hole;
The crank disc is arranged in the seam allowance, is located at the crank-pin in the crank-pin mounting hole.
Further, multiple tapped through holes are additionally provided on the positioning plate, the platform is equipped with multiple T-type thread grooves,
The multiple tapped through hole is arranged in a one-to-one correspondence with the multiple T-type thread groove, described that positioning plate is fixed on the platform,
Include:
It is by multiple T-bolts that the positioning plate is fixed on the platform.
Further, the positioning ring is equipped with multiple lifting threaded holes, described that positioning ring is arranged on the crank disc,
Include:
Lifting bolt is installed in the multiple lifting threaded hole;
The lifting bolt is connected using suspender, the positioning ring is lifted to the crank disc.
Further, described to be bolted the blade by blade root with the crank disc, it is arranged the positioning ring
Outside second rotary table, comprising:
The blade is connect with the crank disc using 8 blade root bolts, 8 blade root bolts are along the blade
It is provided at circumferentially spaced.
Further, described to be bolted the blade by blade root with the crank disc in the paddle shell, packet
It includes:
The blade is connect with the crank disc using 8 blade root bolts, 8 blade root bolts are along the blade
It is provided at circumferentially spaced.
Further, the erection sequence of 8 blade root bolts is as follows:
First blade root bolt and the second blade root bolt, the first blade root bolt and the second blade root bolt spacings are installed
180°;
Third blade root bolt and the 4th blade root bolt, the third blade root bolt and the first blade root bolt spacings are installed
2 θ of angle, the 4th blade root bolt with described 180 ° of third blade root bolt spacings;
5th blade root bolt and the 6th blade root bolt, the 5th blade root bolt and the first blade root bolt spacings are installed
3 θ of angle, the third blade root bolt is between the 5th blade root bolt and the first blade root bolt, the 5th leaf
Root bolt and 180 ° of 6th blade root bolt spacings described;
7th blade root bolt and the 8th blade root bolt, the 7th blade root bolt and the first blade root bolt spacings are installed
Angle, θ, the 7th blade root bolt is between the third blade root bolt and the first blade root bolt, the 7th blade root
Bolt and 180 ° of 8th blade root bolt spacings described, 0 45 ° of < θ <.
Further, the measurement blade axial direction gap width h, comprising:
The clearance gauge of different-thickness is arranged in blade axial gap, blade axial direction gap width h is measured.
Further, the processing bearer ring, comprising:
The paddle shell is mounted on milling machine, the intracorporal bearer ring of paddle shell is processed using face and side cutter.
It is further, described successively to dismantle the blade, the positioning ring and the crank disc, comprising:
By the blade root Bolt dismantling, separate the blade with the crank disc;
The positioning ring is dismantled from the crank disc;
The crank disc is dismantled from the platform.
Technical solution provided in an embodiment of the present invention has the benefit that
Pass through the platform before blade and crank disc are assembled in paddle shell, first crank disc being fixed on outside paddle shell
On, a positioning ring is set on crank disc, then blade and crank disc are bolted by blade root, wherein positioning ring can be used
In replacing bearer ring, to simulate blade and crank disc after being assembled in paddle shell, since the screw-down torque of blade root bolt is larger,
Tighten the case where rear blade can be deformed.Then measure blade axial direction gap width h at this time, and according to blade axial direction gap width h,
The axial length of positioning ring is the setting value H of t and blade axial gap, the axis axial length D of bearer ring is calculated, and process
The intracorporal bearer ring of paddle shell, so that the axial length of bearer ring is D.Finally blade and crank disc are assembled in paddle shell, made
Bearer ring is between blade and crank disc.Since this installation method considers blade deformation to blade axial direction gap width in advance
It influences, therefore can guarantee blade and crank disc after being assembled in paddle shell, blade axial direction gap width is in setting value H range
It is interior.The installation method can be widely applied to tuning for Controllable Pitch Propeller manufacturing industry, be with a wide range of applications.
Detailed description of the invention
To describe the technical solutions in the embodiments of the present invention more clearly, make required in being described below to embodiment
Attached drawing is briefly described, it should be apparent that, drawings in the following description are only some embodiments of the invention, for
For those of ordinary skill in the art, without creative efforts, it can also be obtained according to these attached drawings other
Attached drawing.
Fig. 1 is a kind of cross-sectional view of the part-structure of distance-adjustable oar hub provided in an embodiment of the present invention;
Fig. 2 is a kind of method flow diagram of the installation method of distance-adjustable oar hub provided in an embodiment of the present invention;
Fig. 3 is a kind of cross-sectional view of positioning plate provided in an embodiment of the present invention;
Fig. 4 is a kind of top view of positioning plate provided in an embodiment of the present invention;
Fig. 5 is a kind of cross-sectional view of the mounting structure of blade and crank disc provided in an embodiment of the present invention;
Fig. 6 is a kind of cross-sectional view of positioning ring provided in an embodiment of the present invention;
Fig. 7 is a kind of top view of positioning ring provided in an embodiment of the present invention;
Fig. 8 is a kind of top view of the mounting structure of blade and crank disc provided in an embodiment of the present invention.
Specific embodiment
To make the object, technical solutions and advantages of the present invention clearer, below in conjunction with attached drawing to embodiment party of the present invention
Formula is described in further detail.
In order to better understand the present invention, the part-structure of distance-adjustable oar hub is briefly described below:
Fig. 1 is a kind of cross-sectional view of the part-structure of distance-adjustable oar hub provided in an embodiment of the present invention, as shown in Figure 1, adjusting
It include paddle shell 1, crank disc 2 and blade 3 away from paddle propeller hub.Wherein, paddle shell 1 is equipped with mounting hole 1a, the inner wall of mounting hole 1a
It is equipped with bearer ring 4, the axis of bearer ring 4 is overlapped with the axis of mounting hole 1a.Crank disc 2 and blade 3 are connected by blade root bolt 5
It connects, bearer ring 4 is between crank disc 2 and blade 3.One end face of crank disc 2 is equipped with the first rotary table 21, the first rotary table 21 with
Crank disc 2 is coaxially disposed.One end face of blade 3 is equipped with the second rotary table 31, and the second rotary table 31 is coaxially disposed with blade 3.Bearing
Ring 4 is set in outside the first rotary table 21 and the second rotary table 31, the outer diameter of the internal diameter of bearer ring 4 and the first rotary table 21 and the second rotary table 31
Match.
Fig. 2 is a kind of method flow diagram of the installation method of distance-adjustable oar hub provided in an embodiment of the present invention, such as Fig. 2 institute
Show, which includes:
Crank disc is fixed on platform by step 101.
Specifically, crank disc can be fixed on platform by positioning plate.
Fig. 3 is a kind of cross-sectional view of positioning plate provided in an embodiment of the present invention, and Fig. 4 is one kind provided in an embodiment of the present invention
The top view of positioning plate, as shown in Figure 3 and Figure 4, positioning plate 6 are equipped with a circle seam allowance 61, the outer diameter of seam allowance 61 and crank disc
Outer diameter matches, and the crank-pin mounting hole 62 and multiple screw threads to match with the crank-pin on crank disc is additionally provided on positioning plate 6
Through-hole 63.
By the way that positioning plate 6 is arranged, crank disc can be positioned, prevent crank disc play in the horizontal direction.
Fig. 5 is a kind of cross-sectional view of the mounting structure of blade and crank disc provided in an embodiment of the present invention, as shown in figure 5,
In conjunction with Fig. 4, step 101 may include:
Positioning plate 6 is fixed on platform 200;
Crank disc 2 is arranged in seam allowance 61, is located at crank-pin 2a in crank-pin mounting hole 62.
Further, platform 200 is equipped with multiple T-type thread grooves 210, multiple tapped through holes 63 on positioning plate 6 and more
A T-type thread groove 210 is arranged in a one-to-one correspondence.In the present embodiment, positioning plate 6 is logical equipped with 4 tapped through holes, 63,4 screw threads
Hole 63 is spaced apart along the circumferentially equidistant of positioning plate 6, and the axis of 4 tapped through holes 63 is parallel with the axis of positioning plate 6, to protect
The fixation for demonstrate,proving positioning plate 6 is more stable.By being arranged crank disc 2 on platform 200, in order to subsequent measurement.
Specifically, step 101 further include:
Positioning plate 6 is fixed on platform 200 by multiple T-bolts 300.
After executing the step 101, the end face equipped with the first rotary table 21 of crank disc 2 is upward (i.e. far from platform 200), to hold
Row step 102.
Positioning ring is arranged in step 102 on crank disc.
Specifically, as shown in figure 5, an end face of the separate platform 200 of crank disc 2 is equipped with first rotary table 21 of circle, the
One rotary table 21 is coaxially disposed with crank disc 2, and positioning ring 7 is set in outside the first rotary table 21, the internal diameter of positioning ring 7 and the first rotary table 21
Outer diameter match.
Fig. 6 is a kind of cross-sectional view of positioning ring provided in an embodiment of the present invention, and Fig. 7 is one kind provided in an embodiment of the present invention
The top view of positioning ring, as shown in Figure 6 and Figure 7, positioning ring 7 are equipped with multiple lifting threaded hole 7a, lift screw thread by setting
Hole positioning ring 7 easy to remove.
Specifically, in conjunction with Fig. 6, step 102 can also include:
Lifting bolt (not shown) is installed in multiple lifting threaded hole 7a;
Lifting bolt is connected using suspender, it will be in the lifting to crank disc 2 of positioning ring 7.
In the present embodiment, as shown in fig. 6, lifting threaded hole 7a, two lifting threaded hole 7a there are two setting on positioning ring 7
Circumferentially-spaced 180 ° along positioning ring are arranged, and axis being arranged radially along positioning ring 7 of two lifting threaded hole 7a.
Blade and crank disc are bolted by step 103 by blade root.
Specifically, as shown in figure 5, an end face of blade 3 is equipped with second rotary table 31 of circle, the second rotary table 31 and blade 3
Coaxial arrangement, the internal diameter of positioning ring 7 and the outer diameter of the second rotary table 31 match, the setting of positioning ring 7 blade 3 and crank disc 2 it
Between, the axial length of positioning ring 7 is t.Positioning ring 7 is set in outside the first rotary table 21 and the second rotary table 31.
Preferably, in the present embodiment, the axial length of positioning ring 7 is that t can be configured according to the following formula:
T=T-0.1mm;
Wherein, T is the theoretical axial length of bearer ring.By being that the ratio T that t is arranged is smaller by the axial length of positioning ring 7,
After preventing blade to be deformed, the value of blade axial direction gap width h is caused to become smaller, it is subsequent to be unable to measure blade axial direction gap width
The case where h, occurs.
It should be noted that the theoretical axial length T of bearer ring and the setting value H of blade axial gap are this field skill
Art personnel are according to the preset theoretical value of relative dimensions of blade, three crank disc, paddle shell parts.
Fig. 8 is a kind of top view of the mounting structure of blade and crank disc provided in an embodiment of the present invention, as shown in figure 8,
Step 103 can also include:
Blade is connect with crank disc using 8 blade root bolts, 8 blade root bolt being provided at circumferentially spaced along blade.
Preferably, in conjunction with Fig. 8, the erection sequence of 8 blade root bolts be can be such that
First blade root spiral shell 51 and the second blade root bolt 52, the first blade root bolt 51 and the second blade root bolt 52 interval are installed
180°;
Third blade root bolt 53 and the 4th blade root bolt 54 are installed, third blade root bolt 53 and the first blade root bolt 51 are spaced
2 θ of angle, the 4th blade root bolt 54 are spaced 180 ° with third blade root bolt 53;
5th blade root bolt 55 and the 6th blade root bolt 56 are installed, the 5th blade root bolt 56 and the first blade root bolt 51 are spaced
3 θ of angle, third blade root bolt 53 is between the 5th blade root bolt 55 and the first blade root bolt 51,55 He of the 5th blade root bolt
6th blade root bolt 56 is spaced 180 °;
7th blade root bolt 57 and the 8th blade root bolt 58 are installed, the 7th blade root bolt 57 and the first blade root bolt 51 are spaced
Angle, θ, the 7th blade root bolt 57 are located between third blade root bolt 53 and the first blade root bolt 51, the 7th blade root bolt 57 and
Eight blade root bolts 58 are spaced 180 °, 0 45 ° of < θ <.
In the present embodiment, θ=30 °.
It should be noted that the embodiment of the present invention the first blade root bolt 51 and the second blade root bolt 52 are installed it is successive suitable
Sequencing, the 5th blade root bolt 55 and the 6th blade root bolt of sequence, third blade root bolt 53 and the installation of the 4th blade root bolt 54
The sequencing that the sequencing and the 7th blade root bolt 57 of 56 installations and the 8th blade root bolt 58 are installed is with no restrictions.
Using above-mentioned mounting means install 8 blade root bolts, it is ensured that the stress of 8 blade root bolts more evenly, to subtract
The deformation that few blade 3 occurs.
Step 104, measurement blade axial direction gap width h.
Wherein, as shown in figure 5, blade axial direction gap width h is end face the leaning on to blade 3 of the separate crank disc 2 of positioning ring 7
The distance between the end face of nearly crank disc 2.
Specifically, step 104 may include:
It is arranged in blade axial gap using the clearance gauge of different-thickness, measures blade axial direction gap width h.It is surveyed by clearance gauge
Amount is the distance between two end faces, compared with directly measuring the distance between two o'clock in two end faces using gage, is surveyed
The blade axial direction gap width h measured is more acurrate.
Step 105, processing bearer ring.
Specifically, bearer ring is processed, making the axial length D, D=t+h-H, H of bearer ring is setting for blade axial gap
Definite value.
Paddle shell can be mounted on milling machine in step 105, the intracorporal bearing of paddle shell is processed using face and side cutter
Ring, to guarantee the machining accuracy of bearer ring.
Step 106 successively dismantles blade, positioning ring and crank disc.
Specifically, in conjunction with Fig. 5, step 106 includes:
Blade root bolt 5 is dismantled, separates blade 3 with crank disc 2, positioning ring 7 is dismantled from crank disc, by crank disc
2 dismantle from platform 200.
Specifically, in the present embodiment, since crank disc 2 is to be fixedly connected by positioning plate 6 with platform 200, only need by
Crank disc 2 takes out from the seam allowance of positioning plate 6, and positioning plate 6 can continue to be fixed on platform 200, convenient for next time to crank
Disk 2 is positioned.
Blade and crank disc are bolted by step 107 in paddle shell by blade root.
Specifically, step 107 includes:
Blade is connect with crank disc using 8 blade root bolts, 8 blade root bolt being provided at circumferentially spaced along blade.
Preferably, 8 blade root bolts can be installed according to the erection sequence in step 103, and the present invention is no longer superfluous herein
It states.As shown in Figure 1, at this time bearer ring 4 with a thickness of D, bearer ring 4 is set in outside the first rotary table 21 and the second rotary table 31, and axis
Carrier ring 4 is between blade 3 and crank disc 2.
The embodiment of the present invention is by being first fixed on paddle for crank disc before blade and crank disc are assembled in paddle shell
On platform outside shell, a positioning ring is set on crank disc, then blade and crank disc are bolted by blade root, wherein
Positioning ring is substituted for bearer ring, to simulate blade and crank disc after being assembled in paddle shell, due to blade root bolt
Screw-down torque is larger, tightens the case where rear blade can be deformed.Then blade axial direction gap width h at this time is measured, and according to paddle
Rachis is the setting value H of t and blade axial gap to the axial length of gap width h, positioning ring, and the theory of bearer ring is calculated
Axis axial length D, and the intracorporal bearer ring of paddle shell is processed, so that the axial length of bearer ring is D.Finally by blade and crank disc
It is assembled in paddle shell, makes bearer ring between blade and crank disc.Since this installation method considers blade deformation in advance
Influence to blade axial direction gap width, therefore can guarantee blade and crank disc after being assembled in paddle shell, between blade axial direction
Gap value is within the scope of setting value H.The installation method can be widely applied to tuning for Controllable Pitch Propeller manufacturing industry, be with a wide range of applications.
The foregoing is merely presently preferred embodiments of the present invention, is not intended to limit the invention, it is all in spirit of the invention and
Within principle, any modification, equivalent replacement, improvement and so on be should all be included in the protection scope of the present invention.
Claims (10)
1. a kind of installation method of distance-adjustable oar hub, the distance-adjustable oar hub includes paddle shell, crank disc and blade, the paddle shell
Body is equipped with mounting hole, and the inner wall of the mounting hole is equipped with bearer ring, the axis of the axis of the bearer ring and the mounting hole
Line is overlapped, and an end face of the crank disc is equipped with the first rotary table, and first rotary table and the crank disc are coaxially disposed, described
One end face of blade is equipped with the second rotary table, and second rotary table and the blade are coaxially disposed, the internal diameter of the bearer ring with
The outer diameter of the outer diameter of first rotary table and second rotary table matches, which is characterized in that the installation method includes:
The crank disc is fixed on platform;
Positioning ring is set on the crank disc, and the positioning ring is set in outside first rotary table, the internal diameter of the positioning ring
Match with the outer diameter of first rotary table;
The blade is bolted with the crank disc by blade root, is set in the positioning ring outside second rotary table,
The internal diameter of the positioning ring and the outer diameter of second rotary table match, and the positioning ring is arranged in the blade and the song
Between handle disk, the axial length of the positioning ring is t;
Blade axial direction gap width h is measured, the blade axial direction gap width is the end face far from the crank disc of the positioning ring
To the distance between the end face close to the crank disc of the blade;
The bearer ring is processed, making the axial length D, D=t+h-H, H of the bearer ring is setting for the blade axial gap
Definite value;
The blade, the positioning ring and the crank disc are successively dismantled;
The blade is bolted with the crank disc by blade root in the paddle shell, the bearer ring is made to be set in institute
It states outside the first rotary table and second rotary table, and the bearer ring is between the blade and the crank disc.
2. installation method according to claim 1, which is characterized in that described that the crank disc is fixed on platform, packet
It includes:
Positioning plate is fixed on the platform, and the positioning plate is equipped with a circle seam allowance, the outer diameter of the seam allowance and the song
The outer diameter of handle disk matches, and the crank-pin to match with the crank-pin on the crank disc is additionally provided on the positioning plate and is installed
Hole;
The crank disc is arranged in the seam allowance, is located at the crank-pin in the crank-pin mounting hole.
3. installation method according to claim 2, which is characterized in that multiple tapped through holes are additionally provided on the positioning plate,
The platform is equipped with multiple T-type thread grooves, and the multiple tapped through hole is arranged in a one-to-one correspondence with the multiple T-type thread groove,
It is described that positioning plate is fixed on the platform, comprising:
It is by multiple T-bolts that the positioning plate is fixed on the platform.
4. installation method according to claim 1, which is characterized in that the positioning ring is equipped with multiple lifting threaded holes,
It is described that positioning ring is set on the crank disc, comprising:
Lifting bolt is installed in the multiple lifting threaded hole;
The lifting bolt is connected using suspender, the positioning ring is lifted to the crank disc.
5. installation method according to claim 1, which is characterized in that described that the blade and the crank disc are passed through leaf
Root is bolted, and is set in the positioning ring outside second rotary table, comprising:
The blade is connect with the crank disc using 8 blade root bolts, circumferential direction of the 8 blade root bolts along the blade
Interval setting.
6. installation method according to claim 1, which is characterized in that it is described in the paddle shell by the blade and institute
Crank disc is stated to be bolted by blade root, comprising:
The blade is connect with the crank disc using 8 blade root bolts, circumferential direction of the 8 blade root bolts along the blade
Interval setting.
7. installation method according to claim 5 or 6, which is characterized in that the erection sequence of 8 blade root bolts is such as
Under:
First blade root bolt and the second blade root bolt, the first blade root bolt and the second blade root bolt spacings are installed
180°;
Third blade root bolt and the 4th blade root bolt, the third blade root bolt and the first blade root bolt spacings angle are installed
2 θ, the 4th blade root bolt with described 180 ° of third blade root bolt spacings;
5th blade root bolt and the 6th blade root bolt, the 5th blade root bolt and the first blade root bolt spacings angle are installed
3 θ, the third blade root bolt is between the 5th blade root bolt and the first blade root bolt, the 5th blade root spiral shell
Bolt and 180 ° of 6th blade root bolt spacings described;
7th blade root bolt and the 8th blade root bolt, the 7th blade root bolt and the first blade root bolt spacings angle are installed
θ, the 7th blade root bolt is between the third blade root bolt and the first blade root bolt, the 7th blade root bolt
With described 180 ° of 8th blade root bolt spacings, 0 45 ° of < θ <.
8. installation method according to claim 1, which is characterized in that the measurement blade axial direction gap width h, comprising:
The clearance gauge of different-thickness is arranged in blade axial gap, blade axial direction gap width h is measured.
9. installation method according to claim 1, which is characterized in that the processing bearer ring, comprising:
The paddle shell is mounted on milling machine, the intracorporal bearer ring of paddle shell is processed using face and side cutter.
10. installation method according to claim 1, which is characterized in that described by the blade, the positioning ring and described
Crank disc is successively dismantled, comprising:
By the blade root Bolt dismantling, separate the blade with the crank disc;
The positioning ring is dismantled from the crank disc;
The crank disc is dismantled from the platform.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201810802864.3A CN109292039B (en) | 2018-07-20 | 2018-07-20 | A kind of installation method of distance-adjustable oar hub |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201810802864.3A CN109292039B (en) | 2018-07-20 | 2018-07-20 | A kind of installation method of distance-adjustable oar hub |
Publications (2)
Publication Number | Publication Date |
---|---|
CN109292039A CN109292039A (en) | 2019-02-01 |
CN109292039B true CN109292039B (en) | 2019-11-08 |
Family
ID=65172279
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201810802864.3A Active CN109292039B (en) | 2018-07-20 | 2018-07-20 | A kind of installation method of distance-adjustable oar hub |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN109292039B (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114789270B (en) * | 2021-06-18 | 2024-04-12 | 江南重工有限公司 | Method for machining shell of controllable pitch propeller |
CN113859496B (en) * | 2021-09-30 | 2024-06-04 | 中国船舶重工集团公司第七0四研究所 | Large-scale high load adjustable pitch propeller hub based on rigidity optimization |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0477145A1 (en) * | 1990-09-19 | 1992-03-25 | SANTA CATERINA DI BRENA ADA & C. S.a.S. | A variable-pitch propeller having feathering blades |
CN101602399A (en) * | 2009-07-17 | 2009-12-16 | 南京高精船用设备有限公司 | Propeller hub |
CN101706349A (en) * | 2009-11-10 | 2010-05-12 | 武汉船用机械有限责任公司 | Static balancing method of whole propeller combination of adjustable pitch propellers |
CN102530216A (en) * | 2012-02-14 | 2012-07-04 | 武汉船用机械有限责任公司 | High-power rudder propeller with guide pipe and detaching method for blades of propeller |
CN102554556A (en) * | 2010-12-14 | 2012-07-11 | 上海船厂船舶有限公司 | Machining method for eliminating wear of propeller hub and blades of adjustable propeller device |
CN105108527A (en) * | 2015-09-01 | 2015-12-02 | 武汉船用机械有限责任公司 | Horizontal boring and milling tool for crank pin disc and using method thereof |
CN205147901U (en) * | 2015-11-09 | 2016-04-13 | 中船钢构工程股份有限公司 | Roll adjustment oar base turning off -centre anchor clamps for boss |
CN107128439A (en) * | 2017-03-01 | 2017-09-05 | 武汉船用机械有限责任公司 | A kind of distance-adjustable oar hub assembly tooling |
-
2018
- 2018-07-20 CN CN201810802864.3A patent/CN109292039B/en active Active
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0477145A1 (en) * | 1990-09-19 | 1992-03-25 | SANTA CATERINA DI BRENA ADA & C. S.a.S. | A variable-pitch propeller having feathering blades |
CN101602399A (en) * | 2009-07-17 | 2009-12-16 | 南京高精船用设备有限公司 | Propeller hub |
CN101706349A (en) * | 2009-11-10 | 2010-05-12 | 武汉船用机械有限责任公司 | Static balancing method of whole propeller combination of adjustable pitch propellers |
CN102554556A (en) * | 2010-12-14 | 2012-07-11 | 上海船厂船舶有限公司 | Machining method for eliminating wear of propeller hub and blades of adjustable propeller device |
CN102530216A (en) * | 2012-02-14 | 2012-07-04 | 武汉船用机械有限责任公司 | High-power rudder propeller with guide pipe and detaching method for blades of propeller |
CN105108527A (en) * | 2015-09-01 | 2015-12-02 | 武汉船用机械有限责任公司 | Horizontal boring and milling tool for crank pin disc and using method thereof |
CN205147901U (en) * | 2015-11-09 | 2016-04-13 | 中船钢构工程股份有限公司 | Roll adjustment oar base turning off -centre anchor clamps for boss |
CN107128439A (en) * | 2017-03-01 | 2017-09-05 | 武汉船用机械有限责任公司 | A kind of distance-adjustable oar hub assembly tooling |
Also Published As
Publication number | Publication date |
---|---|
CN109292039A (en) | 2019-02-01 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN109292039B (en) | A kind of installation method of distance-adjustable oar hub | |
US9879656B2 (en) | Roller bearing arrangement for mounting parts of a wind power plant and a wind power plant having a blade bearing designed in such a manner | |
RU2654796C2 (en) | Turbomachine, which contains the means of speed measurement and torque of the turbomachine shaft, and the method of monitoring the mentioned shaft | |
WO2016181729A1 (en) | Drive device for wind turbines, drive device unit for wind turbines, and wind turbine | |
JP2013002445A (en) | Retention device for rotating blade | |
CN107902075B (en) | Static variable pitch propeller | |
CN109516362B (en) | The suspender and its application method of a kind of while hoisting rotor and stator component | |
CN107289030A (en) | A kind of roller bearing pretension adjustment structure and method | |
CN106640995B (en) | Clamp system and equipment with the clamp system | |
WO2017063489A1 (en) | Full-engagement transmission method and device | |
CN113237599A (en) | Clamp suitable for dynamic balance compensation of asymmetric transmission shaft with radial structure | |
CN107084051A (en) | A kind of direct acting type fuel-metering device and its metering method | |
CN110848273A (en) | Precision coupling device for roller way transmission shaft of glass annealing kiln | |
SE541732C2 (en) | Game adjustment mechanism for a gear transmission, in an internal combustion engine and method for adjusting the flank play of such a gear transmission | |
CN104864055A (en) | Drive system adopting polar radius and polar angle | |
CN108858047A (en) | A kind of device connecting water pump vane for removing interference | |
CN109505847B (en) | Aeroengine bearing nut locking structure | |
EP3015654A1 (en) | Turbine assembly | |
CN210317403U (en) | Steam seal structure convenient to measure and adjust turbine radial clearance | |
CN205534083U (en) | Full -tooth meshes transmission | |
CN207795801U (en) | A kind of combined type determines torque nut | |
CN206957967U (en) | A kind of removable axle sleeve for motor connection impeller | |
CN109466730B (en) | Pitch adjusting device for pitch-adjusting propeller model and using method thereof | |
CN113199237A (en) | Method for assembling low-pressure turbine guider of aircraft engine and coaxiality auxiliary control device | |
CN102501956B (en) | Integral propeller hub body of marine propeller |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |