CN109098854A - A kind of gas turbine - Google Patents
A kind of gas turbine Download PDFInfo
- Publication number
- CN109098854A CN109098854A CN201810942300.XA CN201810942300A CN109098854A CN 109098854 A CN109098854 A CN 109098854A CN 201810942300 A CN201810942300 A CN 201810942300A CN 109098854 A CN109098854 A CN 109098854A
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- Prior art keywords
- cavity
- shaft
- chamber
- gear
- turbine
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/26—Starting; Ignition
- F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
- F02C7/275—Mechanical drives
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gear Transmission (AREA)
Abstract
A kind of gas turbine, including main box, horizontally arranged turbine chamber is equipped in the main box, it is arranged on the right side of the turbine chamber for opening and is connected with the external world, the turbine chamber is intracavitary to be equipped with turbine mechanism, fixed block is equipped in the turbine chamber on the right side of the turbine mechanism, the back end surface of the fixed block is connect with the rear wall secure fit of the turbine chamber, combustion chamber is equipped in the main box on the left of the turbine chamber, ignition mechanism is installed in the combustion chamber roof, horizontally arranged chamber of calming the anger is equipped in the main box on the left of the combustion chamber, it is described calm the anger it is intracavitary be equipped with gas pressure mechanism, the main box on the left of the chamber of calming the anger is equipped with the inlet chamber of opening upwards, the inlet chamber is connected setting with the chamber of calming the anger, the first extended up and down sky is equipped in the main box on the left of the chamber of calming the anger Chamber, the main box of first cavity bottom is interior to be equipped with the second cavity.
Description
Technical field
The present invention relates to technical field of gas turbine, specially a kind of gas turbine.
Background technique
Gas turbine mainly uses combustion gas as working media, and working principle is to draw air into intracavitary raising air-flow of calming the anger
Then air is pressed into combustion chamber by pressure, light after mixing air with fuel and be pressurized acting drive turbine by fuel volumetric growth
Rotation, converts heat energy into mechanical energy, and indoor blade of calming the anger when due to just starting can not be driven by turbine to do work, and needs
External force intervention waits until that turbine can just remove external force, but traditional driver for driving pressure blade rotation after steady running
Structure is complicated that transmission process is unstable for structure, it is therefore desirable to design a kind of gas turbine of simple stable transmission of structure.
Summary of the invention
The purpose of the present invention is to provide a kind of gas turbines, for overcoming drawbacks described above in the prior art.According to this
A kind of steamer device of axial exhaust of invention, including main box, the main box is interior to be equipped with horizontally arranged turbine chamber,
It is arranged on the right side of the turbine chamber for opening and is connected with the external world, the turbine chamber is intracavitary is equipped with turbine mechanism, the turbine
Fixed block, the rear wall secure fit of the back end surface of the fixed block and the turbine chamber are equipped in the turbine chamber on the right side of structure
It connects, combustion chamber is equipped in the main box on the left of the turbine chamber, is installed with ignition mechanism in the combustion chamber roof, institute
State and be equipped with horizontally arranged chamber of calming the anger in the main box on the left of combustion chamber, it is described calm the anger it is intracavitary be equipped with gas pressure mechanism,
The main box on the left of the chamber of calming the anger is equipped with the inlet chamber of opening upwards, and the inlet chamber is connected with the chamber of calming the anger to be set
It sets, the first extended up and down cavity is equipped in the main box on the left of the chamber of calming the anger, first cavity bottom
The second cavity is equipped in the main box, being rotatably assorted to be connected with to control to extend between first cavity and the inlet chamber sets
The first rotating shaft set, first rotating shaft left side extending end are installed with the first bevel gear protruded into first cavity, institute
Extending end on the right side of first rotating shaft is stated to protrude into the inlet chamber and set with the connection that is rotatably assorted of the right side end wall of the inlet chamber
It sets, is circumferentially installed with first gear on the outer wall of the first rotating shaft in the inlet chamber, after the first gear
The second gear of kernel mating connection setting therewith is equipped in the inlet chamber of side, secure fit connection in the gear of calming the anger
The first gear shaft for having left and right extended, the left and right end of described first gear shaft or so extending end and the inlet chamber
Wall is rotatably assorted connection, is rotatably assorted between first cavity and second cavity and is connected with up and down extended second
Shaft, second shaft bottom extending end are installed with the second bevel gear protruded into second cavity, and described first turn
It is rotatably assorted between first cavity of axis bottom and the inlet chamber and is connected with the extended third shaft in left and right, it is described
Extending end is installed with the third hand tap gear protruded into first cavity on the left of third shaft, extends on the right side of the third shaft
End is protruded into the inlet chamber, is circumferentially installed on the second shaft outer wall in first cavity and described
4th bevel gear of third hand tap gear engagement mating connection setting, the second shaft outer wall at the top of the 4th bevel gear
Upper circumferential direction is installed with the 5th bevel gear that the setting that is cooperatively connected is engaged with the first bevel gear, the institute on the right side of second cavity
It states and offers the extended third cavity in left and right in main box, be rotatably assorted between second cavity and the third cavity
It is connected with the extended spline housing in left and right, the extended splined shaft in left and right, institute are slidably connected in the spline housing
It states extending end on the left of splined shaft and is installed with to protrude into second cavity and engage to be cooperatively connected with the second bevel gear and set
The 6th bevel gear set, the third cavity is interior to be equipped with the 4th extended shaft of left and right, extension on the left of the 4th shaft
End connect setting with extending end secure fit on the right side of the splined shaft, and left and right is slidably connected in the third cavity
Extended sliding block offers the thread cavity of opening to the right in the sliding block right end face, is equipped with left and right in the thread cavity
Extended screw rod, screw rod left side section is threadedly engaged with the thread cavity connect setting, extends end on the right side of the screw rod
End is cooperatively connected with the first motor power admittedly in end wall on the right side of the third cavity to be arranged, the sliding block left end face and institute
It states extending end on the right side of the 4th shaft and is rotatably assorted to connect and be arranged, peripheral outer wall of the 4th shaft close to the sliding block side
On be installed with the 7th bevel gear, the 4th cavity, the 4th cavity are installed in the main box of the third cavity top
It is rotatably assorted between the third cavity and is connected with the 5th extended up and down shaft, the 5th shaft bottom extends end
End is installed with the 8th bevel gear protruded into the third cavity, at the top of the 5th shaft extending end be installed with protrude into it is described
The 9th bevel gear in 4th cavity, is equipped with the 5th cavity in the main box of the third cavity bottom, and the described 5th
It is equipped with electricity storage mechanism in cavity, is equipped with part of the fuel supply on the right side of the 4th cavity, the main box left end face is equipped with
The L-type steel plate of one group of setting symmetrical above and below, the L-type steel plate are divided into level board and vertical panel, the level board with it is described vertical
The connection of plate secure fit, the vertical panel right end face are connect with the main box left end face secure fit, the level board
It is interior equipped with the thread groove being arranged up and down, the thread groove screw-internal thread fit is connected with up and down extended screw.
Further technical solution, the turbine mechanism include turbine shaft and multiple groups turbo blade, the turbine shaft
Left and right is extended, and section is stretched out through the fixed block and to the right outside the main box, the turbine on the right side of the turbine shaft
Blade is equidistantly arranged in the peripheral outer wall of the turbine shaft.
Further technical solution, the gas pressure mechanism include left and right be extended calm the anger shaft and multiple groups are calmed the anger leaf
Piece, the blade of calming the anger equidistantly are arranged in the peripheral outer wall of the shaft of calming the anger, on the left of the shaft of calming the anger extending end with
Extending end secure fit connection setting on the right side of the third shaft, the shaft right side extending end of calming the anger extend into the combustion
It burns indoor and connect setting with the turbine shaft left distal end secure fit.
Further technical solution, the electricity storage mechanism include solid embedded in the second motor, storage in the third cavity
Battery, rotor coil and permanent magnet, the rotor coil and second motor power, which are cooperatively connected, to be arranged, the battery
It is fixed on the 5th cavity bottom end wall, is electrically connected between the battery and the first motor, the battery
It being electrically connected between second motor, the permanent magnet is relative to rotor coil setting symmetrical above and below, and described
The tenth bevel gear of the setting that is cooperatively connected with power at the top of second motor, the tenth bevel gear position are equipped in three cavitys
At the relative position of the 8th bevel gear bottom.
Further technical solution, the part of the fuel supply include the main box positioned at the third cavity top
Interior fuel cavity, and the intracorporal feeding chamber of the main tank at the top of the fuel cavity, the feeding chamber bottom with it is described
Be connected setting at the top of fuel cavity, and be connected at the top of the feeding chamber with the bottom of combustion chamber setting, and the feeding chamber is located at
It is rotatably assorted on the right side of 4th cavity 16 and between the feeding chamber and the 4th cavity and is connected with what left and right was extended
Second gear shaft, extending end, which is installed with, on the left of the second gear shaft protrudes into the 4th cavity and with the described 9th
11st bevel gear of bevel gear engagement mating connection setting, second gear shaft right side extending end protrude into the supply
It is intracavitary and be rotatably assorted with end wall on the right side of the feeding chamber and connect setting, the second gear shaft in the feeding chamber
Outer wall on be circumferentially installed with third gear, be equipped in the feeding chamber on rear side of the third gear and be engaged with mating connection
The 4th gear being arranged is installed with the extended third rotary gear shaft in left and right, the third gear wheel in the 4th gear
The left and right extending end of shaft is rotatably assorted with the left and right extending end of the feeding chamber connect setting respectively.
Detailed description of the invention
Fig. 1 is a kind of gas turbine schematic diagram of internal structure in the present invention;
Fig. 2 is part of the fuel supply side schematic view in the present invention;
Fig. 3 is the side schematic view of first gear and second gear in the present invention;
Fig. 4 is a kind of main view of gas turbine in the present invention;
Fig. 5 is the schematic diagram of internal structure of L-type steel plate in the present invention.
Specific embodiment
Below with reference to Fig. 1-5, the present invention is described in detail.
Referring to Fig.1-5, a kind of gas turbine of embodiment according to the present invention, including main box 1, in the main box 1
Equipped with horizontally arranged turbine chamber 25, it is arranged on the right side of the turbine chamber 25 for opening and is connected with the external world, the turbine
It is equipped with turbine mechanism in chamber 25, is equipped with fixed block 26, the fixed block 26 in the turbine chamber 25 on the right side of the turbine mechanism
Back end surface connect with the rear wall secure fit of the turbine chamber 25, set in the main box 1 in 25 left side of the turbine chamber
Combuster 20, is installed with ignition mechanism 21 in 20 roof of combustion chamber, in the main box 1 in 20 left side of combustion chamber
Equipped with horizontally arranged chamber 22 of calming the anger, gas pressure mechanism, the described of 22 left side of chamber of calming the anger are equipped in the chamber 22 of calming the anger
It is equipped with the inlet chamber 14 of opening upwards in main box 1, the inlet chamber 14 is connected setting with the chamber 22 of calming the anger, described to calm the anger
The first extended up and down cavity 7, the master of 7 bottom of the first cavity are equipped in the main box 1 in 22 left side of chamber
The second cavity 2 is equipped in cabinet 1, being rotatably assorted to be connected with to control to extend between first cavity 7 and the inlet chamber 14 sets
The first rotating shaft 12 set, the 12 left side extending end of first rotating shaft are installed with the first cone tooth protruded into first cavity 7
Wheel 10, the 12 right side extending end of first rotating shaft protrude into the inlet chamber 14 and turn with the right side end wall of the inlet chamber 14
The dynamic setting that is cooperatively connected, is circumferentially installed with first gear on the outer wall of the first rotating shaft 12 in the inlet chamber 14
15, the inlet chamber 14 of the rear side of the first gear 15 is interior to be equipped with the second gear 58 for being engaged with the setting that is cooperatively connected,
Secure fit is connected with the extended first gear shaft 57 in left and right, the first gear shaft 57 in the second gear 58
Left and right extending end is rotatably assorted with the left hand end wall of the inlet chamber 14 connect respectively, first cavity 7 and described second
It is rotatably assorted between cavity 2 and is connected with the second extended up and down shaft 4, the 4 bottom extending end of the second shaft is fixed
There is the second bevel gear 3 protruded into second cavity 2, first cavity 7 and institute positioned at 12 bottom of first rotating shaft
It states to be rotatably assorted between inlet chamber 14 and is connected with the extended third shaft 13 in left and right, extend end on the left of the third shaft 13
End is installed with the third hand tap gear 9 protruded into first cavity 7, the 13 right side extending end of third shaft protrude into it is described into
In air cavity 14, circumferentially it is installed with and the third hand tap gear 9 on 4 outer wall of the second shaft in first cavity 7
Engagement is cooperatively connected the 4th bevel gear 8 of setting, 4 outer wall last week of second shaft positioned at 8 top of the 4th bevel gear
To being installed with the 5th bevel gear 11 for engaging the setting that is cooperatively connected with the first bevel gear 12, second cavity, 2 right side
The extended third cavity 36 in left and right is offered in the main box 1, between second cavity 2 and the third cavity 36
It is rotatably assorted and is connected with the extended spline housing 48 in left and right, be slidably connected with left and right in the spline housing 48 and be extended
Splined shaft 49, the 49 left side extending end of splined shaft be installed with protrudes into second cavity 2 and with the second cone tooth
6th bevel gear 50 of 3 engagement mating connection setting of wheel, interior the 4th shaft for being equipped with left and right and being extended of third cavity 36
41, the 41 left side extending end of the 4th shaft connect setting with the 49 right side extending end secure fit of splined shaft, described
It is slidably connected with the extended sliding block 37 in left and right in third cavity 36, offers opening in 37 right end face of sliding block
Thread cavity 33 to the right, is equipped with the extended screw rod 35 in left and right in the thread cavity 33, the 35 left side section of screw rod with it is described
Thread cavity 33 be threadedly engaged connection setting, the 35 right side extending end of screw rod with admittedly be embedded in the 36 right side end wall of third cavity
Interior 34 power of first motor, which is cooperatively connected, to be arranged, and 37 left end face of sliding block and the 41 right side extending end of the 4th shaft turn
The dynamic setting that is cooperatively connected, the 4th shaft 41 are installed with the 7th bevel gear in the peripheral outer wall of 37 side of sliding block
39, the 4th cavity 16, the 4th cavity 16 and the third are installed in the main box 1 at 36 top of the third cavity
It is rotatably assorted between cavity 36 and is connected with the 5th extended up and down shaft 6, the 6 bottom extending end of the 5th shaft is fixed
Have the 8th bevel gear 40 protruded into the third cavity 36, the 6 top extending end of the 5th shaft be installed with protrude into it is described
The 9th bevel gear 17 in 4th cavity 16, the main box 1 of 36 bottom of third cavity is interior to be equipped with the 5th cavity 47, institute
It states and is equipped with electricity storage mechanism in the 5th cavity 47, part of the fuel supply, 1 left side of main box are equipped on the right side of the 4th cavity 16
End face is equipped with the L-type steel plate 102 of one group of setting symmetrical above and below, and the L-type steel plate 102 divides for level board 106 and vertical panel
103, the level board 106 is connect with 103 secure fit of vertical panel, 103 right end face of vertical panel and the main tank
The connection of 1 left end face secure fit of body, the level board 106 is interior to be equipped with the thread groove 104 being arranged up and down, the thread groove
104 screw-internal thread fits are connected with screw 105 extended up and down.
Beneficial or illustratively, the turbine mechanism includes turbine shaft 23 and multiple groups turbo blade 24, the turbine
Shaft 23 or so is extended, and the 23 right side section of turbine shaft runs through the fixed block 26 for the connection setting that is rotatably assorted therewith
And stretch out to the right outside the main box 1, the turbo blade 24 is equidistantly arranged in the peripheral outer wall of the turbine shaft 23.
It is beneficial or illustratively, the gas pressure mechanism include left and right be extended calm the anger shaft 56 and multiple groups are calmed the anger leaf
Piece 19, the blade 19 of calming the anger equidistantly are arranged in the peripheral outer wall of the shaft 56 of calming the anger, prolong on the left of the shaft 56 of calming the anger
It stretches end and connect setting, the 56 right side extending end of shaft of calming the anger with the 13 right side extending end secure fit of third shaft
It extend into the combustion chamber 20 and extends left distal end secure fit with the turbine shaft 23 and connect setting.
Valuably or illustratively, the electricity storage mechanism include the second motor 44 admittedly in the third cavity 36,
Battery 46, rotor coil 46 and permanent magnet 43, the rotor coil 46 are set with 44 power of the second motor mating connection
Set, the battery 46 is fixed in 47 bottom end wall of the 5th cavity, the battery 46 and the first motor 34 it
Between be electrically connected, be electrically connected between the battery 46 and second motor 45, the permanent magnet 43 is relative to described
It the setting symmetrical above and below of rotor coil 46 and is individually fixed in 47 roof of the 5th cavity at the position that keeps left and the battery
In 46 top end surface, the tenth cone of the setting that is cooperatively connected with 44 power of the second motor is equipped in the third cavity 36
Gear 42, the tenth bevel gear 42 are located at the relative position of 40 bottom of the 8th bevel gear, and then realize first motor
Self-centered purpose can be carried out by battery with electric energy consumed by the second motor, save the operation of replacement battery.
Valuably or illustratively, the part of the fuel supply includes the main tank positioned at 36 top of third cavity
Fuel cavity 32 in body 1, and the feeding chamber 28 in the main box 1 at 32 top of fuel cavity, the feeding chamber
Be connected setting at the top of 28 bottoms and the fuel cavity 32, and 28 top of feeding chamber is connected with 20 bottom of combustion chamber to be set
It sets, the feeding chamber 28 is located at 16 right side of the 4th cavity and rotates between the feeding chamber 28 and the 4th cavity 16 and matches
It closes and is connected with the extended second gear shaft 29 in left and right, the 29 left side extending end of second gear shaft, which is installed with, to be protruded into
4th cavity 16 is interior and the 11st bevel gear 18 of the setting that is cooperatively connected is engaged with the 9th bevel gear 17, and described second
29 right side extending end of rotary gear shaft is protruded into the feeding chamber 28 and is rotatably assorted with the 28 right side end wall of feeding chamber and connect
It is arranged, is circumferentially installed with third gear 30 on the outer wall of the second gear shaft 29 in the feeding chamber 28, it is described
The 4th gear 54 for being engaged with the setting that is cooperatively connected, the 4th tooth are equipped in the feeding chamber 28 of 30 rear side of third gear
The extended third rotary gear shaft 53 in left and right, the left and right extending end point of the third gear wheel shaft 53 are installed in wheel 54
It is not rotatably assorted with the left hand end wall of the feeding chamber 28 and connect setting, fuel is passed through into supply by fuel cavity so as to realize
Chamber carries out the purpose of supply work into combustion chamber.
When original state, sliding block 37 is located at the right positions in third cavity 36 to the greatest extent, while screw rod 35 is most
Big degree protrudes into screw rod chamber 33, makes the 7th bevel gear 39 to the greatest extent far from the 8th bevel gear 40 and the tenth bevel gear
42, while making the 6th bevel gear 50 to the greatest extent far from second bevel gear 3.
When the engine operates, it is first turned on the second motor 45, battery 46 is powered to the second motor 45, the second motor
Then first motor 34 is opened in 45 work, battery 46 rotates first motor to the power supply of first motor 34, and first motor passes through
It drives screw rod 35 to push to be moved to the left with the sliding block 37 for connecting and being arranged that is threadedly engaged, meanwhile, sliding block 37 drives the 4th shaft
41 are moved to the left, and engage the 7th bevel gear 39 respectively with the tenth bevel gear 42 and the 8th bevel gear 40, at this time the tenth cone tooth
Wheel 42 rotates and the 7th bevel gear 39 is driven to rotate, and the 7th bevel gear 39 is made to drive the rotation of the 8th bevel gear 40, the 8th bevel gear
40 by driving the 5th shaft 6 to rotate and the 9th bevel gear 17 being driven to rotate, and is that the 9th bevel gear 17 passes through second gear shaft
29 drive third gear 30 to rotate, and third gear 30 drives the rotation of the 4th gear 54, and the fuel in fuel cavity 32 is sucked supply
Chamber 28 is simultaneously pushed into combustion chamber 20, while splined shaft 49 is moved to the left, and so that the 6th bevel gear 50 is engaged cooperation with second bevel gear 3 and connects
Setting is connect, while second bevel gear 3 drives the 4th bevel gear 8 and the 5th bevel gear 11 to rotate by the second shaft 4 of drive, simultaneously
5th bevel gear 11 drives first bevel gear 10 to rotate, and first bevel gear 10 is made to drive 15 turns of first gear by first rotating shaft 12
Dynamic, first gear 15 drives the rotation of second gear 58 for being engaged with connection setting to draw air into inlet chamber 14, while the 4th
Bevel gear 8 drives third hand tap gear 9 to rotate, and rotates third shaft 19 with action pneumatic shaft 56, and shaft of calming the anger 56 passes through drive
Blade 19 of calming the anger calms the anger the air sucking in inlet chamber 14 chamber 22, and air enters combustion chambers 20 through 22, opens dynamo exploder at this time
Structure 21 is lighted a fire, and fuel burns expansion work in combustion chamber 20, and main box 1 is discharged after driving turbo blade 24 to rotate, works as turbine
When 24 revolving speed of blade reaches a certain level, close first motor 44, at this time due to the 7th bevel gear 39 still with the tenth bevel gear 42
Engagement so coil rotor 45 continues to rotate, and is generated electricity, and electric energy is stored up by the magnetic field that cutting permanent magnet 43 generates
There are in battery 46.
The beneficial effects of the present invention are: when the engine operates, being first turned on the second motor, battery gives the second motor
Then first motor is opened in power supply, the work of the second motor, battery rotates first motor to first motor power supply, the first electricity
Machine is moved to the left by driving screw rod to push with the sliding block for connecting and being arranged that is threadedly engaged, meanwhile, sliding block drives the 4th shaft
It is moved to the left, engages the 7th bevel gear respectively with the tenth bevel gear and the 8th bevel gear, the tenth bevel gear rotation at this time is simultaneously
It drives the 7th bevel gear to rotate, so that the 7th bevel gear is driven the rotation of the 8th bevel gear, the 8th bevel gear is by driving the 5th shaft
It rotates and the 9th bevel gear is driven to rotate, be that the 9th bevel gear passes through the drive third gear rotation of second gear shaft, third tooth
Wheel drives the rotation of the 4th gear, by the fuel sucking feeding chamber in fuel cavity and is pushed into combustion chamber, while splined shaft is moved to the left,
The 6th bevel gear is set to engage mating connection setting with second bevel gear, while second bevel gear is by driving the second shaft to drive the
Four bevel gears and the 5th bevel gear rotate, while the 5th bevel gear drives first bevel gear rotation, make first bevel gear by the
One shaft drive first gear rotation, first gear drive be engaged with connection setting second gear rotation draw air into
Air cavity, while the 4th bevel gear drives third hand tap gear rotation, rotates third shaft band action pneumatic shaft, shaft of calming the anger passes through
The air in inlet chamber is sucked into chamber of calming the anger with action pneumatic blade, air opens ignition mechanism igniting through entering combustion chamber at this time,
Fuel in the combustion chamber do work by burning expansion, main box is discharged after driving turbo blade rotation, when turbo blade revolving speed reaches one
When determining degree, first motor is closed, at this time since the 7th bevel gear still engages with the tenth bevel gear, so coil rotor continues to turn
It is dynamic, and generated electricity by the magnetic field that cutting permanent magnet generates, and electric energy is stored in battery, to meet the first electricity
The self-sustaining purpose of electric energy self-supporting in machine and the second motor, and the configuration of the present invention is simple, easy to operate, stable transmission.
Those skilled in the art can define, can in the case of not departing from overall spirit of the invention and design
To make the various modifications for above embodiments.It falls within the scope of protection of the present invention.Protection scheme of the invention
It is subject to claims appended hereto.
Claims (5)
1. a kind of gas turbine, including main box, it is characterised in that: including main box, horizontal direction is equipped in the main box
The turbine chamber of setting, the turbine chamber right side are connected for opening setting and with the external world, and the turbine chamber is intracavitary to be equipped with turbine
Structure is equipped with fixed block, the back end surface of the fixed block and the turbine chamber in the turbine chamber on the right side of the turbine mechanism
The connection of rear wall secure fit, be equipped with combustion chamber in the main box on the left of the turbine chamber, it is solid in the combustion chamber roof
Equipped with ignition mechanism, horizontally arranged chamber of calming the anger, the chamber of calming the anger are equipped in the main box on the left of the combustion chamber
Interior to be equipped with gas pressure mechanism, the main box on the left of the chamber of calming the anger is equipped with the inlet chamber of opening upwards, the inlet chamber and institute
It states chamber of calming the anger to be connected setting, the first extended up and down cavity, institute is equipped in the main box on the left of the chamber of calming the anger
It states and is equipped with the second cavity in the main box of the first cavity bottom, be rotatably assorted between first cavity and the inlet chamber
It is connected with the extended first rotating shaft in left and right, extending end, which is installed with, on the left of the first rotating shaft protrudes into first cavity
First bevel gear, extending end protrudes into the inlet chamber and the right side end wall with the inlet chamber on the right side of the first rotating shaft
Be rotatably assorted connection setting, is circumferentially installed with first gear on the outer wall of the first rotating shaft in the inlet chamber, institute
State the second gear that kernel mating connection setting therewith is equipped in the inlet chamber of the rear side of first gear, the gear of calming the anger
Interior secure fit is connected with the extended first gear shaft in left and right, described first gear shaft or so extending end with it is described
The left hand end wall of inlet chamber is rotatably assorted connection, is rotatably assorted and is connected with up and down between first cavity and second cavity
The second extended shaft, second shaft bottom extending end are installed with the second cone tooth protruded into second cavity
Wheel is rotatably assorted between first cavity of the first rotating shaft bottom and the inlet chamber and is connected with what left and right was extended
Third shaft, extending end is installed with the third hand tap gear protruded into first cavity on the left of the third shaft, and described the
Extending end protrudes into the inlet chamber on the right side of three shafts, circumferential on the second shaft outer wall in first cavity
It is installed with the 4th bevel gear that the setting that is cooperatively connected is engaged with the third hand tap gear, the institute at the top of the 4th bevel gear
State the 5th bevel gear for being circumferentially installed on the second shaft outer wall and engaging the setting that is cooperatively connected with the first bevel gear, described the
The extended third cavity in left and right is offered in the main box on the right side of two cavitys, second cavity and the third are empty
It is rotatably assorted between chamber and is connected with the extended spline housing in left and right, left and right extension is slidably connected in the spline housing and is set
The splined shaft set, splined shaft left side extending end, which is installed with, to be protruded into second cavity and nibbles with the second bevel gear
The 6th bevel gear for closing the setting that is cooperatively connected, is equipped with the 4th extended shaft of left and right in the third cavity, and the described 4th
Extending end connect setting with extending end secure fit on the right side of the splined shaft on the left of shaft, and sliding is matched in the third cavity
It closes and is connected with the extended sliding block in left and right, the thread cavity of opening to the right, the screw thread are offered in the sliding block right end face
Intracavitary to be equipped with the extended screw rod in left and right, section is threadedly engaged with the thread cavity on the left of the screw rod connect setting, the spiral shell
Extending end is cooperatively connected with the first motor power admittedly in end wall on the right side of the third cavity and is arranged on the right side of bar, the sliding block
Left end face is rotatably assorted with extending end on the right side of the 4th shaft and connect setting, and the 4th shaft is close to the sliding block one
It is installed with the 7th bevel gear in the peripheral outer wall of side, is installed with the 4th cavity in the main box of the third cavity top,
It is rotatably assorted between 4th cavity and the third cavity and is connected with the 5th extended up and down shaft, described 5th turn
Axis bottom extending end is installed with the 8th bevel gear protruded into the third cavity, and extending end is solid at the top of the 5th shaft
It is empty that the 5th is equipped with equipped with the 9th bevel gear protruded into the 4th cavity, in the main box of the third cavity bottom
Chamber, the 5th cavity is interior to be equipped with electricity storage mechanism, and part of the fuel supply, the main box left side are equipped on the right side of the 4th cavity
End face is equipped with the L-type steel plate of one group of setting symmetrical above and below, and the L-type steel plate is divided into level board and vertical panel, the level board
It being connect with the vertical panel secure fit, the vertical panel right end face is connect with the main box left end face secure fit,
It is equipped with the thread groove being arranged up and down in the level board, the thread groove screw-internal thread fit is connected with extended up and down
Screw.
2. a kind of gas turbine according to claim 1, it is characterised in that: the turbine mechanism includes turbine shaft and more
Group turbo blade, turbine shaft or so are extended, and section stretches out through the fixed block and to the right institute on the right side of the turbine shaft
It states outside main box, the turbo blade is equidistantly arranged in the peripheral outer wall of the turbine shaft.
3. a kind of gas turbine according to claim 1, it is characterised in that: the gas pressure mechanism includes that left and right is extended
Calm the anger shaft and multiple groups are calmed the anger blade, the blade of calming the anger equidistantly is arranged in the peripheral outer wall of the shaft of calming the anger, described
Extending end connect setting, the shaft right side of calming the anger with extending end secure fit on the right side of the third shaft on the left of shaft of calming the anger
Side extending end extend into the combustion chamber and connect setting with the turbine shaft left distal end secure fit.
4. a kind of gas turbine according to claim 1, it is characterised in that: the electricity storage mechanism includes solid embedded in described
The second motor, battery, rotor coil and permanent magnet in third cavity, the rotor coil and second motor power
Be cooperatively connected setting, and the battery is fixed on the 5th cavity bottom end wall, the battery and the first motor
Between be electrically connected, be electrically connected between the battery and second motor, the permanent magnet is relative to the rotor
Coil setting symmetrical above and below, interior the tenth be equipped with power mating connection setting at the top of second motor of the third cavity
Bevel gear, the tenth bevel gear are located at the relative position of the 8th bevel gear bottom.
5. a kind of gas turbine according to claim 1, it is characterised in that: the part of the fuel supply includes positioned at described
The intracorporal fuel cavity of the main tank of third cavity top, and the intracorporal supply of the main tank at the top of the fuel cavity
Be connected setting at the top of chamber, the feeding chamber bottom and the fuel cavity, the feeding chamber top and the bottom of combustion chamber phase
Connection setting, the feeding chamber are located on the right side of the 4th cavity and are rotatably assorted between the feeding chamber and the 4th cavity
It is connected with the extended second gear shaft in left and right, extending end, which is installed with, on the left of the second gear shaft protrudes into described the
The 11st bevel gear of the setting that is cooperatively connected, the second gear shaft right side are engaged in four cavitys and with the 9th bevel gear
Extending end, which is protruded into the feeding chamber and is rotatably assorted with end wall on the right side of the feeding chamber, connect setting, is located at the feeding chamber
Third gear is circumferentially installed on the outer wall of the interior second gear shaft, in the feeding chamber on rear side of the third gear
Equipped with the 4th gear for being engaged with the setting that is cooperatively connected, the extended third gear in left and right is installed in the 4th gear
Shaft, the left and right extending end of the third gear wheel shaft are rotatably assorted with the left and right extending end of the feeding chamber company respectively
Connect setting.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201810942300.XA CN109098854A (en) | 2018-08-17 | 2018-08-17 | A kind of gas turbine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201810942300.XA CN109098854A (en) | 2018-08-17 | 2018-08-17 | A kind of gas turbine |
Publications (1)
Publication Number | Publication Date |
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CN109098854A true CN109098854A (en) | 2018-12-28 |
Family
ID=64850224
Family Applications (1)
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CN201810942300.XA Withdrawn CN109098854A (en) | 2018-08-17 | 2018-08-17 | A kind of gas turbine |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111298929A (en) * | 2019-12-10 | 2020-06-19 | 广州达都动力科技有限公司 | Low-speed operable jet propulsion unit |
-
2018
- 2018-08-17 CN CN201810942300.XA patent/CN109098854A/en not_active Withdrawn
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111298929A (en) * | 2019-12-10 | 2020-06-19 | 广州达都动力科技有限公司 | Low-speed operable jet propulsion unit |
CN111298929B (en) * | 2019-12-10 | 2020-10-09 | 东阳格盘机械科技有限公司 | Low-speed operable jet propulsion unit |
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