CN109108850A - The supporting system of novel axial exhaust turbine rotor - Google Patents
The supporting system of novel axial exhaust turbine rotor Download PDFInfo
- Publication number
- CN109108850A CN109108850A CN201810927783.6A CN201810927783A CN109108850A CN 109108850 A CN109108850 A CN 109108850A CN 201810927783 A CN201810927783 A CN 201810927783A CN 109108850 A CN109108850 A CN 109108850A
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- CN
- China
- Prior art keywords
- cavity
- sliding
- shaft
- fixedly installed
- bevel gear
- 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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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
- B25B11/00—Work holders not covered by any preceding group in the subclass, e.g. magnetic work holders, vacuum work holders
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M15/00—Testing of engines
- G01M15/02—Details or accessories of testing apparatus
Abstract
The invention discloses the supporting systems of novel axial exhaust turbine rotor, including fuselage, the first cavity being arranged in the fuselage and the second cavity being arranged in the fuselage, third cavity is provided with and communicated between first cavity and second cavity, the 4th cavity of opening to the left is provided on the right side of second cavity in end wall, driving chamber is provided in the third cavity bottom wall, symmetrical sliding rack is slidably provided in first cavity, the through-hole for being provided with the 5th cavity in the sliding rack and being penetrated through below the 5th cavity or so；Device structure of the invention is simple, it is easy to operate, the movement of equipment and the clamping of rotor are driven by using the same power source, realize that rotor distance is adjusted in handoff procedure again, this equipment conveniently moving adjusts automation, automatic aligning axle center, measuring accuracy and testing efficiency are improved, cooperates and does not influence between each process, improve device practical performance.
Description
Technical field
The present invention relates to steam turbine field, the supporting system of specifically novel axial exhaust turbine rotor.
Background technique
With the development of science and technology, social progress, country promotes always high-tech development, in steam turbine field, one
Directly there is a relatively difficult technical problem, inconvenience when being exactly the bulky test of part turbine rotor, and steamer
Machine rotor clamping not of uniform size is constant, and using axial power after existing equipment clamping, rotor main shaft exists same with power source main shaft
Axis degree error, causes measuring accuracy to decline, therefore a kind of device of urgent need solves problems.
Summary of the invention
Technical problem to be solved by the invention is to provide the supporting system of novel axial exhaust turbine rotor, energy
Enough solve the problems in above-mentioned present technology.
The present invention is achieved through the following technical solutions: the branch of novel axial exhaust turbine rotor of the invention
System is held, it is described including fuselage, the first cavity being arranged in the fuselage and the second cavity being arranged in the fuselage
It is provided with and communicated with third cavity between first cavity and second cavity, is provided with opening in end wall on the right side of second cavity
The 4th cavity to the left is provided with driving chamber in the third cavity bottom wall, is slidably provided with a left side in first cavity
Right symmetrical sliding rack, be provided in the sliding rack the 5th cavity and below the 5th cavity left and right perforation it is logical
Hole is rotatably provided with spline housing in the 5th cavity, and the spline housing outer surface is fixedly installed with first bevel gear, institute
The splined hole that left and right perforation is provided in spline housing is stated, the splined hole internal spline is connected with the splined shaft that left and right extends,
It is rotatably dispose in the first cavity left hand end wall at left and right sides of the splined shaft, it is symmetrical in end wall before and after first cavity
It is provided be open opposite the first sliding cavity and the second sliding cavity below first sliding cavity, first sliding
The 6th cavity is provided with and communicated between chamber and second sliding cavity, can horizontally slip in first sliding cavity be provided with
The first rack gear that the sliding rack on right side is fixedly connected, what can be horizontally slipped in second sliding cavity is provided with and left side
The second rack gear for being fixedly connected of Soviet Union's Sohu's sliding rack is rotatably provided with through first cavity in the 6th cavity
First rotating shaft, first rotating shaft front and rear sides end are rotatably dispose in the end wall of the 6th cavity front and back, and described first turn
Axis rear side end is fixedly connected with the first motor being fixedly installed in the 6th cavity rear side end wall, in the 6th cavity
The first rotating shaft outer surface is fixedly installed with and first rack gear and the second rack gear meshed gears, first cavity
The interior first rotating shaft outer surface is fixedly installed with first pulley, is provided with the 7th cavity, institute in the 5th cavity roof
It states to can slide up and down in the 7th cavity and is provided with the first sliding shoe, be symmetrically arranged with up and down before and after first sliding shoe
The second sliding eye, be slidably connected with the first slide guide bar extended up and down, first slide guide in second sliding eye
Two sides are fixedly installed in the 7th cavity or more end wall bar up and down, are connected between the 5th cavity and the 7th cavity
It is provided with the 8th cavity, thread bush is rotatably provided in the 8th cavity, is provided with opening upwards in the thread bush
Thread cavity, the thread cavity screw-internal thread fit is connected with the threaded rod upwardly extended, the threaded rod top end with it is described
First sliding shoe is fixedly connected, and the thread bush bottom end protrudes into the 5th cavity and end is fixedly installed with and described
The second bevel gear of one bevel gear engagement, is provided with lighting device on the fuselage, the lighting device include headlamp and
Lamp holder.
Preferably technical solution, the splined shaft left distal end protrude into second cavity, second cavity
Third hand tap gear is fixedly mounted in the interior splined shaft outer surface, and can slide up and down in the third cavity, it is sliding to be provided with second
Motion block is provided with the 9th external cavity of connection in the second sliding shoe, and rotation is arranged between end wall before and after the third cavity
The second shaft for having front and back to extend, second shaft outer surface are fixedly installed with the second belt wheel and are located at second belt wheel
The cam of front side is driven by the belt through the through-hole between second belt wheel and the first pulley and is cooperatively connected, institute
It states and is fixedly installed with the second motor in end wall on the left of the second sliding shoe, the second motor output shaft left distal end is fixedly installed with
The 4th bevel gear engaged with the third hand tap gear.
Preferably technical solution, rotation is provided with third shaft between the 4th cavity and the driving chamber, institute
It states the third shaft end in the 4th cavity and is fixedly installed with the 5th bevel gear cooperated with the 4th bevel gear, it is described
The third shaft end in driving chamber is fixedly installed with the 6th bevel gear, and front and back is rotatably provided in the driving chamber
The 4th shaft extended, the 4th shaft front and rear sides end end wall before and after the driving chamber protrude into exterior space and end
End is fixedly installed with the first idler wheel, and the 4th shaft outer surface in the driving chamber is fixedly installed with and the 6th cone tooth
The 7th bevel gear of engagement is taken turns, is symmetrically arranged with rotatable second idler wheel on end wall before and after the fuselage.
Preferably technical solution, the interior rotation of the sliding rack bottom wall symmetrical and symmetrical third before and after being provided with
Idler wheel.
Preferably technical solution, elasticity is provided with press bullet between the second sliding shoe and the third cavity
Spring.
Preferably technical solution, front and back is symmetrically set in the 7th cavity roof, with the first sliding shoe roof
Opening is equipped with to the tenth opposite cavity, the interior rotation of the tenth cavity is provided with the 5th shaft that left and right extends, the institute of front side
It states the 5th shaft and is connect with the third motor power being fixedly installed in the end wall of the tenth cavity left side, outside the 5th shaft
Surface is fixedly installed with the 4th idler wheel.
Preferably technical solution is fixedly installed with lamp holder, fixed peace on the lamp holder roof on the fuselage roof
Equipped with headlamp.
The beneficial effects of the present invention are: starting second motor, second electricity when being worked with equipment of the invention
Machine rotation drives the 4th bevel gear rotation, and the 4th bevel gear rotation drives the 5th bevel gear rotation, and described the
The rotation of five bevel gears drives the 6th bevel gear rotation, and the 6th bevel gear rotation drives the 7th bevel gear rotation,
The 7th bevel gear rotation drives the first idler wheel rotation, moves the equipment at this time to suitable location, rotates institute at this time
First motor is stated, the first motor rotation drives the first rotating shaft rotation, and the first rotating shaft rotation drives described first
Belt wheel rotation, the first pulley rotation drive the second belt wheel rotation, and the second belt wheel rotation drives the cam
Rotation, when the cam rotates described in the second slide switch moved up under top pressure spring effect, the triconodont at this time
Wheel is engaged with the 4th bevel gear, and the 4th bevel gear and the 5th bevel gear are detached from the gear at the same time and rotate
Drive first rack gear and second rack gear backwards to mobile, first rack gear and second rack gear movement backwards
Drive two sliding racks in left and right separate, when the sliding rack distance is greater than rotor axial length when left and right two, by the rotor
It is placed between two sliding racks in left and right, inverts the first motor at this time, the first motor reversion drives the left and right
Two sliding racks move towards, and the rotor shaft protrudes into the 7th cavity, start second motor at this time, and described
The rotation of two motors drives the 4th bevel gear rotation, and the 4th bevel gear rotation drives the third hand tap gear rotation, institute
It states third hand tap gear rotation and drives the splined shaft rotation, the splined shaft rotation drives the spline housing rotation, the spline
Set rotation drives first bevel gear rotation, and the first bevel gear rotation drives the second bevel gear rotation, and described the
The rotation of two bevel gears drives the thread bush rotation, and the thread bush rotation drives the threaded rod to move up, on the threaded rod
Shipper pole moves first sliding shoe and moves up the clamping rotor shaft, rotates the third motor at this time, and the third motor turns
Dynamic to drive the 4th idler wheel rotation, the 4th idler wheel rotation drives the rotor rotation, convenient for test.
Device structure of the invention is simple, easy to operate, drives the movement of equipment by using the same power source and turns
The clamping of son, and realize that rotor distance is adjusted in handoff procedure, this equipment conveniently moving adjusts automation, automatic aligning axis
The heart improves measuring accuracy and testing efficiency, cooperates and do not influence between each process, improve device practicability
Energy.
Detailed description of the invention
The present invention is described in detail by following specific embodiments and drawings for ease of explanation,.
Fig. 1 is the supporting system overall structure diagram of novel axial exhaust turbine rotor of the invention；
Fig. 2 is A-A structural schematic diagram in Fig. 1.
Specific embodiment
As Figure 1-Figure 2, the supporting system of novel axial exhaust turbine rotor of the invention, including fuselage 100,
The first cavity 131 being arranged in the fuselage 100 and the second cavity 101 being arranged in the fuselage 100, described first
It is provided with and communicated with third cavity 111 between cavity 131 and second cavity 101, is set in the 101 right side end wall of the second cavity
It is equipped with the 4th cavity 113 of opening to the left, is provided with driving chamber 119, first cavity in 111 bottom wall of third cavity
It is slidably provided with symmetrical sliding rack 138 in 131, is provided with the 5th cavity 137 and position in the sliding rack 138
The through-hole 122 of perforation is controlled below the 5th cavity 137, is rotatably provided with spline housing in the 5th cavity 137
134,134 outer surface of spline housing is fixedly installed with first bevel gear 135, and left and right perforation is provided in the spline housing 134
Splined hole 133,133 internal spline of splined hole is connected with the splined shaft 103 that left and right extends, and the splined shaft 103 is left
Right two sides are rotatably dispose in 131 left hand end wall of the first cavity, are symmetrically arranged in the 131 front and back end wall of the first cavity
The first sliding cavity 128 for being open opposite and the second sliding cavity 130 positioned at 128 lower section of the first sliding cavity, described first
The 6th cavity 127 is provided with and communicated between sliding cavity 128 and second sliding cavity 130, it can be left in first sliding cavity 128
Right sliding is provided with the first rack gear 129 being fixedly connected with the sliding rack 138 on right side, in second sliding cavity 130
What can be horizontally slipped is provided with the second rack gear 123 being fixedly connected with Sohu of the Soviet Union sliding rack 138 in left side, the 6th cavity
The first rotating shaft 124 through first cavity 131,124 front and rear sides of first rotating shaft end are rotatably provided in 127
End is rotatably dispose in the 127 front and back end wall of the 6th cavity, 124 rear side end of first rotating shaft and is fixedly installed on described the
First motor in six cavitys, 127 rear side end wall is fixedly connected, 124 appearance of the first rotating shaft in the 6th cavity 127
Face be fixedly installed with 123 meshed gears 126 of first rack gear 129 and the second rack gear, in first cavity 131
124 outer surface of first rotating shaft is fixedly installed with first pulley 125, and the 7th sky is provided in 137 roof of the 5th cavity
Chamber 139 can slide up and down in the 7th cavity 139 and be provided with the first sliding shoe 141,141 front and back of the first sliding shoe
It is symmetrically arranged with the second sliding eye 150 up and down, is slidably connected in second sliding eye 150 and extends up and down
First slide guide bar 140, about 140 two sides of the first slide guide bar are fixedly installed in about 139 end wall of the 7th cavity, institute
It states and is provided with and communicated with the 8th cavity 142 between the 5th cavity 137 and the 7th cavity 139, can turn in the 8th cavity 142
Dynamic is provided with thread bush 143, is provided with the thread cavity 144 of opening upwards in the thread bush 143, in the thread cavity 144
It is threadedly engaged the threaded rod 145 for being connected with and upwardly extending, 145 top end of threaded rod and first sliding shoe 141 are solid
Fixed connection, 143 bottom end of thread bush protrudes into the 5th cavity 137 and end is fixedly installed with and the first cone tooth
The second bevel gear 136 of 135 engagements is taken turns, is provided with lighting device on the fuselage 100, the lighting device includes headlamp
201 and lamp holder 200.
Valuably, 103 left distal end of splined shaft protrudes into second cavity 101, in second cavity 101
Third hand tap gear 102 is fixedly mounted in 103 outer surface of splined shaft, can slide up and down and is provided in the third cavity 111
The second sliding shoe 105, the 9th cavity 110 being provided in the second sliding shoe 105 outside connection, the third cavity 111
Rotation is provided with the second shaft 109 that front and back extends between the end wall of front and back, and 109 outer surface of the second shaft is fixedly installed with second
Belt wheel 107 and the cam 108 on front side of second belt wheel 107, second belt wheel 107 and the first pulley 125
Between be driven and be cooperatively connected by the belt 146 through the through-hole 122, fixed peace in the 105 left side end wall of the second sliding shoe
Equipped with the second motor 106, the 106 output shaft left distal end of the second motor is fixedly installed with nibbles with the third hand tap gear 102
The 4th bevel gear 104 closed.
Valuably, rotation is provided with third shaft 114 between the 4th cavity 113 and the driving chamber 119, and described the
114 end of third shaft in four cavitys 113 is fixedly installed with the 5th bevel gear with the 4th bevel gear 104 cooperation
112,114 end of third shaft in the driving chamber 119 is fixedly installed with the 6th bevel gear 115, the driving chamber 119
Interior the 4th shaft 117 for being rotatably provided with front and back and extending, the driving is run through in the 117 front and rear sides end of the 4th shaft
119 front and back end wall of chamber protrudes into exterior space and end is fixedly installed with the first idler wheel 120, and described in the driving chamber 119
Four shafts, 117 outer surface is fixedly installed with the 7th bevel gear 116 engaged with the 6th bevel gear 115, before the fuselage 100
Rotatable second idler wheel is symmetrically arranged on aft bulkhead.
Valuably, symmetrical and symmetrical third idler wheel 132 before and after being provided with is rotated in 138 bottom wall of sliding rack.
Valuably, elasticity is provided with top pressure spring 121 between the second sliding shoe 105 and the third cavity 111.
Valuably, in 139 roof of the 7th cavity, with the first sliding shoe roof front and back be symmetrically arranged with opening to
The tenth opposite cavity 148, rotation is provided with the 5th shaft 147 that left and right extends in the tenth cavity 148, front side it is described
5th shaft 147 is connect with the third motor power being fixedly installed in the 148 left side end wall of the tenth cavity, and described 5th turn
147 outer surface of axis is fixedly installed with the 4th idler wheel 149.
Valuably, it is fixedly installed with lamp holder 200 in 100 roof of fuselage, is fixedly installed on 200 roof of lamp holder
Headlamp 201 works convenient for the equipment in no light.
When equipment of the invention is in original state, the first motor, the second motor 106 and third motor are located
In stationary state, two sliding racks 138 in left and right are in fit-state, and the cam 108 squeezes the second sliding shoe 105
Positioned at 111 bottom of third cavity, the third hand tap gear 102 is detached from the 4th bevel gear 104, the 4th cone tooth
Wheel 104 is engaged with the 5th bevel gear 112.
When being worked with equipment of the invention, start second motor 106, the rotation of the second motor 106 drives institute
The rotation of the 4th bevel gear 104 is stated, the 4th bevel gear 104 rotation drives the 5th bevel gear 112 rotation, the 5th cone
The rotation of gear 112 drives the 6th bevel gear 115 rotation, and the 6th bevel gear 115 rotation drives the 7th bevel gear
116 rotations, the 7th bevel gear 116 rotation drive first idler wheel 120 to rotate, move the equipment at this time to suitable position
It sets, rotates the first motor at this time, the first motor rotation drives the first rotating shaft 124 to rotate, the first rotating shaft
124 rotations drive the first pulley 125 to rotate, and the rotation of first pulley 125 drives second belt wheel 107 to rotate,
Second belt wheel 107 rotation drives the cam 108 to rotate, when the cam 108 rotates described in the second slide switch 105 exist
The top pressure spring 121 moves up under acting on, and the third hand tap gear 102 is engaged with the 4th bevel gear 104 at this time, and described the
Four bevel gears 104 are detached from the rotation of gear 126 at the same time with the 5th bevel gear 112 and drive first rack gear 129
And second rack gear 123 is left backwards to mobile drive backwards to movement, first rack gear 129 and second rack gear 123
Right two sliding racks 138 are separate, when two sliding racks 138 in left and right are apart from greater than rotor axial length, by the rotor
It is placed between two sliding racks 138 in left and right, inverts the first motor at this time, the first motor reversion drives the left side
Right two sliding racks 138 move towards, and the rotor shaft protrudes into the 7th cavity 139, start second electricity at this time
Machine 106, the rotation of the second motor 106 drive the 4th bevel gear 104 rotation, and the 4th bevel gear 104 rotation drives
The third hand tap gear 102 rotates, and the rotation of third hand tap gear 102 drives the splined shaft 103 to rotate, the splined shaft
103 rotations drive the spline housing 134 to rotate, and the rotation of spline housing 134 drives the first bevel gear 135 to rotate, described
The rotation of first bevel gear 135 drives the second bevel gear 136 to rotate, and the rotation of second bevel gear 136 drives the screw thread
143 rotation of set, the thread bush 143 rotation drive the threaded rod 145 to move up, and the threaded rod 145, which moves up, drives described the
One sliding shoe 141, which moves up, clamps the rotor shaft, rotates the third motor at this time, and the third motor rotates described in drive
The rotation of 4th idler wheel 149, the 4th idler wheel 149 rotation drives the rotor rotation, convenient for test.
The beneficial effects of the present invention are: starting second motor, second electricity when being worked with equipment of the invention
Machine rotation drives the 4th bevel gear rotation, and the 4th bevel gear rotation drives the 5th bevel gear rotation, and described the
The rotation of five bevel gears drives the 6th bevel gear rotation, and the 6th bevel gear rotation drives the 7th bevel gear rotation,
The 7th bevel gear rotation drives the first idler wheel rotation, moves the equipment at this time to suitable location, rotates institute at this time
First motor is stated, the first motor rotation drives the first rotating shaft rotation, and the first rotating shaft rotation drives described first
Belt wheel rotation, the first pulley rotation drive the second belt wheel rotation, and the second belt wheel rotation drives the cam
Rotation, when the cam rotates described in the second slide switch moved up under top pressure spring effect, the triconodont at this time
Wheel is engaged with the 4th bevel gear, and the 4th bevel gear and the 5th bevel gear are detached from the gear at the same time and rotate
Drive first rack gear and second rack gear backwards to mobile, first rack gear and second rack gear movement backwards
Drive two sliding racks in left and right separate, when the sliding rack distance is greater than rotor axial length when left and right two, by the rotor
It is placed between two sliding racks in left and right, inverts the first motor at this time, the first motor reversion drives the left and right
Two sliding racks move towards, and the rotor shaft protrudes into the 7th cavity, start second motor at this time, and described
The rotation of two motors drives the 4th bevel gear rotation, and the 4th bevel gear rotation drives the third hand tap gear rotation, institute
It states third hand tap gear rotation and drives the splined shaft rotation, the splined shaft rotation drives the spline housing rotation, the spline
Set rotation drives first bevel gear rotation, and the first bevel gear rotation drives the second bevel gear rotation, and described the
The rotation of two bevel gears drives the thread bush rotation, and the thread bush rotation drives the threaded rod to move up, on the threaded rod
Shipper pole moves first sliding shoe and moves up the clamping rotor shaft, rotates the third motor at this time, and the third motor turns
Dynamic to drive the 4th idler wheel rotation, the 4th idler wheel rotation drives the rotor rotation, convenient for test.
Device structure of the invention is simple, easy to operate, drives the movement of equipment by using the same power source and turns
The clamping of son, and realize that rotor distance is adjusted in handoff procedure, this equipment conveniently moving adjusts automation, automatic aligning axis
The heart improves measuring accuracy and testing efficiency, cooperates and do not influence between each process, improve device practicability
Energy.
The above description is merely a specific embodiment, but scope of protection of the present invention is not limited thereto, any
The change or replacement expected without creative work, should be covered by the protection scope of the present invention.Therefore, of the invention
Protection scope should be determined by the scope of protection defined in the claims.
Claims (7)
1. the supporting system of novel axial exhaust turbine rotor of the invention, including fuselage, is arranged in the fuselage
First cavity and the second cavity being arranged in the fuselage, it is characterised in that: first cavity and second cavity
Between be provided with and communicated with third cavity, be provided with the 4th cavity of opening to the left on the right side of second cavity in end wall, described the
It is provided with driving chamber in three cavity bottom walls, symmetrical sliding rack, the cunning are slidably provided in first cavity
It is provided with the 5th cavity and the through-hole positioned at the 5th cavity lower section left and right perforation in moving frame, can turn in the 5th cavity
Dynamic is provided with spline housing, and the spline housing outer surface is fixedly installed with first bevel gear, and left and right is provided in the spline housing
The splined hole of perforation, the splined hole internal spline are connected with the splined shaft that left and right extends, turn at left and right sides of the splined shaft
It is dynamic to be set in the first cavity left hand end wall, opposite first that be open is symmetrically arranged with before and after first cavity in end wall
Sliding cavity and the second sliding cavity below first sliding cavity, first sliding cavity and second sliding cavity it
Between be provided with and communicated with the 6th cavity, being provided with for can horizontally slipping in first sliding cavity is fixed with the sliding rack on right side
First rack gear of connection, being provided with for can horizontally slipping in second sliding cavity are fixedly connected with Sohu of the Soviet Union sliding rack in left side
The second rack gear, be rotatably provided with the first rotating shaft through first cavity in the 6th cavity, described first turn
Axis front and rear sides end is rotatably dispose in front of and after the 6th cavity in end wall, the first rotating shaft rear side end be fixedly installed on
First motor on rear side of 6th cavity in end wall is fixedly connected, and the first rotating shaft outer surface in the 6th cavity is solid
Dingan County is equipped with first rack gear and the second rack gear meshed gears, the first rotating shaft appearance in first cavity
Face is fixedly installed with first pulley, and the 7th cavity is provided in the 5th cavity roof, can go up downslide in the 7th cavity
It is dynamic to be provided with the first sliding shoe, it is symmetrically arranged with the second sliding eye up and down before and after first sliding shoe, described the
The the first slide guide bar extended up and down is slidably connected in two sliding eyes, the first slide guide bar is fixedly installed on two sides up and down
7th cavity in end wall, is provided with and communicated with the 8th cavity between the 5th cavity and the 7th cavity up and down, described
It is rotatably provided with thread bush in 8th cavity, the thread cavity of opening upwards, the thread cavity are provided in the thread bush
Screw-internal thread fit is connected with the threaded rod upwardly extended, and the threaded rod top end is fixedly connected with first sliding shoe,
The thread bush bottom end protrudes into the 5th cavity and end is fixedly installed with second engaged with the first bevel gear
Bevel gear is provided with lighting device on the fuselage, and the lighting device includes headlamp and lamp holder.
2. the supporting system of novel axial exhaust turbine rotor according to claim 1, it is characterised in that: the flower
Key axis left distal end protrudes into second cavity, and third cone is fixedly mounted in the splined shaft outer surface in second cavity
Gear can slide up and down in the third cavity and be provided with the second sliding shoe, and it is outer that connection is provided in the second sliding shoe
9th cavity in portion, rotation is provided with the second shaft that front and back extends, second shaft between end wall before and after the third cavity
Outer surface is fixedly installed with the second belt wheel and the cam on front side of second belt wheel, second belt wheel and described first
It is driven and is cooperatively connected by the belt through the through-hole between belt wheel, be fixedly installed with the on the left of the second sliding shoe in end wall
Two motors, the second motor output shaft left distal end are fixedly installed with the 4th bevel gear engaged with the third hand tap gear.
3. the supporting system of novel axial exhaust turbine rotor according to claim 1, it is characterised in that: described
Rotation is provided with third shaft between four cavitys and the driving chamber, and the third shaft end in the 4th cavity is fixed
The 5th bevel gear with the 4th bevel gear cooperation is installed, the third shaft end in the driving chamber is fixedly mounted
There is the 6th bevel gear, the 4th shaft that front and back extends, the 4th shaft front and back two are rotatably provided in the driving chamber
Exterior space through end wall before and after the driving chamber is protruded into side end and end is fixedly installed with the first idler wheel, in the driving chamber
The 4th shaft outer surface be fixedly installed with the 7th bevel gear engaged with the 6th bevel gear, the fuselage front and back end
Rotatable second idler wheel is symmetrically arranged on wall.
4. the supporting system of novel axial exhaust turbine rotor according to claim 1, it is characterised in that: the cunning
Symmetrical and symmetrical third idler wheel before and after being provided with is rotated in moving frame bottom wall.
5. the supporting system of novel axial exhaust turbine rotor according to claim 1, it is characterised in that: described
Elasticity is provided with top pressure spring between two sliding shoes and the third cavity.
6. the supporting system of novel axial exhaust turbine rotor according to claim 1, it is characterised in that: described
Front and back is symmetrically arranged with opening to the tenth opposite cavity in seven cavity roofs, with the first sliding shoe roof, and the described tenth
Rotation is provided with the 5th shaft that left and right extends in cavity, the 5th shaft of front side and is fixedly installed on the tenth cavity
Third motor power connection in the end wall of left side, the 5th shaft outer surface is fixedly installed with the 4th idler wheel.
7. the supporting system of novel axial exhaust turbine rotor according to claim 1, it is characterised in that: the machine
It is fixedly installed with lamp holder on body roof, is fixedly installed with headlamp on the lamp holder roof.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810927783.6A CN109108850A (en) | 2018-08-15 | 2018-08-15 | The supporting system of novel axial exhaust turbine rotor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810927783.6A CN109108850A (en) | 2018-08-15 | 2018-08-15 | The supporting system of novel axial exhaust turbine rotor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109108850A true CN109108850A (en) | 2019-01-01 |
Family
ID=64852243
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810927783.6A Withdrawn CN109108850A (en) | 2018-08-15 | 2018-08-15 | The supporting system of novel axial exhaust turbine rotor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109108850A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112497167A (en) * | 2020-10-19 | 2021-03-16 | 杨金花 | Mechanical equipment processing assembly platform |
| CN114453166A (en) * | 2022-01-14 | 2022-05-10 | 宁波市欣磊金属制品有限公司 | Automatic piece equipment of getting of spraying |
-
2018
- 2018-08-15 CN CN201810927783.6A patent/CN109108850A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112497167A (en) * | 2020-10-19 | 2021-03-16 | 杨金花 | Mechanical equipment processing assembly platform |
| CN114453166A (en) * | 2022-01-14 | 2022-05-10 | 宁波市欣磊金属制品有限公司 | Automatic piece equipment of getting of spraying |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190101 |
|
| WW01 | Invention patent application withdrawn after publication |