CN206205998U - Continuous rotation pinking tank - Google Patents
Continuous rotation pinking tank Download PDFInfo
- Publication number
- CN206205998U CN206205998U CN201621195676.1U CN201621195676U CN206205998U CN 206205998 U CN206205998 U CN 206205998U CN 201621195676 U CN201621195676 U CN 201621195676U CN 206205998 U CN206205998 U CN 206205998U
- Authority
- CN
- China
- Prior art keywords
- rotation
- tank
- detonation combustor
- shell
- pinking
- 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
- 238000005474 detonation Methods 0.000 claims abstract description 57
- 238000002485 combustion reaction Methods 0.000 claims abstract description 31
- 239000000446 fuel Substances 0.000 claims abstract description 16
- 239000000567 combustion gas Substances 0.000 claims abstract description 8
- 230000000149 penetrating effect Effects 0.000 claims abstract description 6
- 239000007789 gas Substances 0.000 claims description 51
- 238000010304 firing Methods 0.000 claims description 10
- 230000005540 biological transmission Effects 0.000 claims description 9
- 230000006835 compression Effects 0.000 claims description 5
- 238000007906 compression Methods 0.000 claims description 5
- 238000011144 upstream manufacturing Methods 0.000 claims description 4
- 238000001816 cooling Methods 0.000 claims description 3
- 238000002156 mixing Methods 0.000 claims description 2
- 238000005516 engineering process Methods 0.000 abstract description 7
- 239000002737 fuel gas Substances 0.000 description 7
- 239000000203 mixture Substances 0.000 description 3
- 230000033228 biological regulation Effects 0.000 description 2
- 238000004200 deflagration Methods 0.000 description 2
- 239000000809 air pollutant Substances 0.000 description 1
- 231100001243 air pollutant Toxicity 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 210000000988 bone and bone Anatomy 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 238000005183 dynamical system Methods 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000000605 extraction Methods 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 230000002045 lasting effect Effects 0.000 description 1
- DOTMOQHOJINYBL-UHFFFAOYSA-N molecular nitrogen;molecular oxygen Chemical compound N#N.O=O DOTMOQHOJINYBL-UHFFFAOYSA-N 0.000 description 1
- 238000004064 recycling Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
Landscapes
- Toys (AREA)
Abstract
The utility model provides a kind of continuous rotation pinking tank, and it includes power set and tank body.Power set include shell, centerbody, rotation detonation combustor, oil circuit component, igniter and drive mechanism.Shell has air intake and exhaust outlet.Centerbody has along the intermediate throughholes for axially penetrating through centerbody of centerbody.Rotation detonation combustor is sheathed on centerbody and is fixedly connected on shell, and the air intake of shell is communicated in rotation detonation combustor.Oil circuit component is controlled to be communicated in rotation detonation combustor.Igniter is fixedly installed on rotation detonation combustor, for being lighted a fire to the combustion gas that the fuel and air that enter in rotation detonating combustion room are formed, and then combustion gas rotation detonating combustion.The power turbine of drive mechanism under the gas-powered after rotating detonating combustion rotary motion for being done work to tank body.As a result of rotation pinking technology, its high combustion efficiency, stability and good reliability, save fuel, extend service life.
Description
Technical field
The utility model is related to power technology field, more particularly to a kind of continuous rotation pinking tank.
Background technology
Tank is the important equipment of army operation, and dynamical system is the core of tank, at present, the T-80 series of Russia
The M1 series main battle tanks in main battle tank and the U.S. are already equipped with gas turbine nearly 50 years as main power plant, China the
One tank gas turbine also in test run in 2014 and is crowned with complete success, it is seen that gas turbine is expected to turn into tank in future
The major impetus device of equipment.Along with the appearance of high power density diesel engine, the quality of gas turbine and Diesel engine is asked
There is very big dispute in topic, traditional gas turbine has the advantages that power big, small volume, lightweight, and possesses well
Starting performance, meanwhile, the big shortcoming of gas turbine engine for tank fuel consumption also clearly, is made to lasting operation and logistics supply supply
Into very big difficulty, as bone of contention.Technological improvement is carried out to gas turbine, it is always tank power plant to improve performance
Main development direction.
Utility model content
In view of problem present in background technology, the purpose of this utility model is that a kind of continuous rotation pinking of offer is smooth
Gram, the high combustion efficiency of its power set, stability and good reliability, save fuel, extend service life.
To achieve these goals, the utility model provides a kind of continuous rotation pinking tank, and it includes power set
And tank body.Power set provide power, including shell, centerbody, rotation detonation combustor, oil circuit group for tank body
Part, igniter and drive mechanism.
Shell has：Air intake, is arranged at the front end of shell, in a ring, connects outside atmosphere；And exhaust outlet, if
It is placed in the rear end of shell.Centerbody is in the form of a column, and is fixedly installed on the middle part of shell, and with axially penetrating through center along centerbody
The intermediate throughholes of body.Rotation detonation combustor is sheathed on centerbody and is fixedly connected on shell, and the air intake of shell is connected
In rotation detonation combustor, with air-supplied to rotation detonation combustor.Oil circuit component is controlled to be communicated in rotation detonation combustor,
Fuel is provided with to rotation detonation combustor.Igniter is fixedly installed on rotation detonation combustor, for quick-fried to entering rotation
The combustion gas that fuel and air in shake combustion chamber are formed is lighted a fire, and then combustion gas rotation detonating combustion.Drive mechanism includes：The
One calms the anger uses component, is arranged in the intermediate throughholes of centerbody, for compressing the air entered in shell；Second calms the anger uses component,
First is arranged in calm the anger with component, for the air that further compression enters in shell；Power turbine, in rotation detonating combustion
Rotary motion under gas-powered afterwards；And power transmission shaft, one end is connected to power turbine, and the other end is connected to tank body,
So that power turbine does work to tank body.
The beneficial effects of the utility model are as follows：
According in continuous rotation pinking tank of the present utility model, power set are using the gas of continuous flowing as work
Make medium, send into and mix in rotation detonation combustor and rotate detonating combustion to produce high temperature high by by outside atmosphere and fuel
Compression ignition gas, is then calmed the anger to the first of drive mechanism using high-temperature high-pressure fuel gas and is calmed the anger use with component, power turbine and second
Component expansion work.Now a part of heat energy of high-temperature high-pressure fuel gas is converted into the mechanical energy of power turbine and revolves power turbine
Transhipment is dynamic.Because power turbine is connected to tank body via power transmission shaft, so as to realize that power turbine does work to tank body.This
The continuous rotation pinking tank of utility model is based on employing rotation pinking technology, and it has compared with traditional deflagration is burnt
Efficiency of combustion higher, saves fuel.Additionally, rotation detonating combustion more stablize, improve power set stability and
Reliability, extends service life.
Brief description of the drawings
Fig. 1 is the overall structure diagram according to continuous rotation pinking tank of the present utility model；
Fig. 2 is the first structural representation calmed the anger with component in Fig. 1；
Fig. 3 is the structural representation of the power turbine in Fig. 1；
Fig. 4 is the second structural representation calmed the anger with component in Fig. 1；
Fig. 5 is the overall structure stereogram of the interior annular flow distribution plate in Fig. 1 and exterior annular flow distribution plate；
Fig. 6 is the deformation pattern of Fig. 5；
Fig. 7 is the sectional view after line A-A cutting along Fig. 1；
Fig. 8 is the sectional view after line B-B cutting along Fig. 1.
Wherein, description of reference numerals is as follows：
Perforation in the middle of 1 power set 16131
The power turbine of 11 shell 162
The power transmission shaft of 111 air intake 163
112 exhaust outlets 164 second are calmed the anger and use component
The compressor of 12 centerbody 1,641 second
The turbine of 121 intermediate throughholes 1,642 second
The rotating shaft of 122 outside wall surface 1,643 second
The 13 rotation interior annular flow distribution plates of detonation combustor 17
The perforate of 131 air inlet 171
The exterior annular flow distribution plate of 132 inwall 18
133 outer walls 181 are open
134 gas outlet 19 blends room
135 annular firing chamber C1 clutch shaft bearings
14 oil circuit component C2 second bearings
141 the first gas channels of oil feed line T1
142 the second gas channels of cartridge T2
143 the first adjustable guiders of nozzle F1
15 the second adjustable guiders of igniter F2
16 drive mechanism P blast pipes
161 first calm the anger with component G boilers
The tank body of 1611 first compressor 2
The decelerator of 1612 first turbine 3
1613 first rotating shafts
Specific embodiment
With reference to the accompanying drawings come describe in detail according to it is of the present utility model it is continuous rotation pinking tank.
Referring to figs. 1 to Fig. 8, according to continuous rotation pinking tank of the present utility model, it includes power set 1 and tank master
Body 2 (refers mainly to the crawler belt or tire of tank) here.Power set 1 are that tank body 2 provides power, including shell 11, center
Body 12, rotation detonation combustor 13, oil circuit component 14, igniter 15 and drive mechanism 16.
Shell 11 has：Air intake 111, is arranged at the front end of shell 11, in a ring, connects outside atmosphere；And row
Gas port 112, is arranged at the rear end of shell 11.Centerbody 12 is in the form of a column, and is fixedly installed on the middle part of shell 11, and with along center
The intermediate throughholes 121 for axially penetrating through centerbody 12 of body 12.Rotation detonation combustor 13 is sheathed on centerbody 12 and is fixedly connected
Rotation detonation combustor 13 is communicated in the air intake 111 of shell 11, and shell 11, is fed with to rotation detonation combustor 13
Air.Oil circuit component 14 is controlled to be communicated in rotation detonation combustor 13, and fuel is provided with to rotation detonation combustor 13.Igniter
15 are fixedly installed on rotation detonation combustor 13, for what is formed to the fuel and air that enter in rotation detonation combustor 13
Combustion gas is lighted a fire, and then combustion gas rotation detonating combustion.
Drive mechanism 16 includes：First calms the anger with component 161, the intermediate throughholes 121 of centerbody 12 is arranged in, for compressing
Air into shell 11；Second calms the anger with component 164, is arranged in first and calms the anger with component 161, for further compression
Air into shell 11；Power turbine 162, the rotary motion under the gas-powered after rotating detonating combustion；And transmission
Axle 163, one end is connected to power turbine 162, and the other end is connected to tank body 2, so that power turbine 162 is to tank body
2 actings.
According in continuous rotation pinking tank of the present utility model, power set 1 are using the continuous gas conduct flowed
Working media, sends into and mix in rotation detonation combustor 13 and rotate detonating combustion to produce height by by outside atmosphere and fuel
Warm high-pressure gas, then using high-temperature high-pressure fuel gas to the first of drive mechanism 16 calm the anger with component 161, power turbine 162 with
And second calm the anger with the expansion work of component 164.Now a part of heat energy of high-temperature high-pressure fuel gas is converted into the machine of power turbine 162
Tool energy and make the rotary motion of power turbine 162.Because power turbine 162 is connected to tank body 2 via power transmission shaft 163, so that
Realize that power turbine 162 does work to tank body 2.Continuous rotation pinking tank of the present utility model is based on employing rotation pinking
Technology, it, with efficiency of combustion higher, saves fuel compared with traditional deflagration is burnt.Additionally, rotation detonating combustion is more
Plus stabilization, the stability and reliability of power set 1 are improve, extend service life.
According to continuous rotation pinking tank of the present utility model, in one embodiment, reference picture 1, continuous rotation pinking is smooth
Gram may also include：Decelerator 3, is arranged on the power transmission shaft 163 between power turbine 162 and tank body 2, power turbine 162
Tank body 2 is connected to via decelerator 3 to be done work with to tank body 2.
According to it is of the present utility model it is continuous rotation pinking tank, in one embodiment, reference picture 2, first calms the anger uses component
161 may include：First compressor 1611, is arranged at the upstream of rotation detonation combustor 13；First turbine 1612, is arranged at rotation
The downstream of detonation combustor 13；And first rotating shaft 1613, the intermediate throughholes 121 of centerbody 12 are worn, pressed for connecting first
The turbine 1612 of mechanism of qi 1611 and first.Wherein, the high-temperature high-pressure fuel gas discharged in rotation detonation combustor 13 are to the first turbine
1612 expansion works, the rotary motion of the first turbine 1612 simultaneously drives the first compressor 1611 to work with right by first rotating shaft 1613
It is compressed into the air in shell 11.
According in continuous rotation pinking tank of the present utility model, reference picture 1, first rotating shaft 1613 can be by first axle
Hold C1 and be connected to centerbody 12.
According to it is of the present utility model it is continuous rotation pinking tank, in one embodiment, reference picture 4, first rotating shaft 1613 can
With the middle perforation 16131 for axially penetrating through first rotating shaft 1613 along centerbody 12.Second calms the anger can also be wrapped with component 164
Include：Second compressor 1641, is arranged at the upstream of the first compressor 1611；Second turbine 1642, is arranged at the first turbine 1612
Downstream；And second rotating shaft 1643, be arranged in first rotating shaft 1613 in the middle of perforation 16131, for connecting the second compressor
1641 and second turbine 1642.In this embodiment, power turbine 162 and decelerator 3 are directly mounted at power transmission shaft 163.Its
In, to the expansion work of the second turbine 1642, the second turbine 1642 revolves the high-temperature high-pressure fuel gas discharged in rotation detonation combustor 13
Turn move through the second rotating shaft 1643 drive the second compressor 1641 work with to via the first compressor 1611 compress after
Air is further compressed.
According in continuous rotation pinking tank of the present utility model, reference picture 1, the second rotating shaft 1643 can be by the second axle
Hold C2 and be connected to first rotating shaft 1613.
According in continuous rotation pinking tank of the present utility model, reference picture 1, rotation detonation combustor 13 can have：
Air inlet 131；The first gas channel T1 is formed between inwall 132, and the outside wall surface 122 of centerbody 12；Outer wall 133, it is and interior
Wall 132 forms the annular firing chamber 135 of rotation detonation combustor 13 together, and the air intake 111 of shell 11 is via air inlet 131
Annular firing chamber 135 is communicated in air-supplied to annular firing chamber 135, and second is formed between outer wall 133 and shell 11
Gas channel T2；And gas outlet 134, for the gas discharge rotation detonation combustor 13 after rotation detonating combustion.Wherein, flow through
Air in first gas channel T1 and the second gas channel T2 is mainly used in cooling rotation detonation combustor 13.
Remark additionally herein, compared with the combustion chamber of traditional power set, continuous rotation of the present utility model
The size of the rotation detonation combustor 13 in pinking tank is relatively small, so as to reduce the overall dimensions of power set 1.
According to continuous rotation pinking tank of the present utility model, in one embodiment, reference picture 1 rotates detonation combustor
13 front portion can be the big irregular deformation cavity in the middle narrow two (pressure for changing the air entered via air inlet 131
Power), and afterbody (part of finger ring shape combustion chamber 135) can be the circular cylindrical cavity (for rotating detonating combustion) of rule.Here, by
In rotation detonation combustor 13 afterbody for prismatic, therefore combustion process in annular firing chamber 135 is by general etc.
Compression ignition burns and is changed into approximate isochoric combustion, significantly improves efficiency of combustion, burning velocity soon, and then can be provided for tank body 2
Bigger power.
According to continuous rotation pinking tank of the present utility model, in one embodiment, reference picture 1, power set 1 can also be wrapped
Include：Interior annular flow distribution plate 17, is arranged at the first gas channel T1 porch, enters in the first gas channel T1 for adjusting
Air mass flow.
In one embodiment, reference picture 6 and Fig. 7, interior annular flow distribution plate 17 can be lamina, through setting on lamina
There is perforate 171 to admit air into the first gas channel T1.
In one embodiment, reference picture 5 and Fig. 7, interior annular flow distribution plate 17 can be doubling plate, run through setting on each laminate
Perforate 171 is equipped with to admit air into the first gas channel T1.Wherein, the wherein laminate in doubling plate is fixedly connected on center
The inwall 132 of body 12 and rotation detonation combustor 13, and another laminate can rotary motion adjusting into the first gas channel
The air mass flow of T1.Here, interior annular flow distribution plate 17 changes perforate 171 based on the dislocation between the two-layer in doubling plate
Size, and then realize the regulation of air mass flow.
According to continuous rotation pinking tank of the present utility model, in one embodiment, reference picture 1, power set 1 can also be wrapped
Include：Exterior annular flow distribution plate 18, is arranged at the second gas channel T2 porch, enters in the second gas channel T2 for adjusting
Air mass flow.
In one embodiment, reference picture 6 and Fig. 7, exterior annular flow distribution plate 18 can be lamina, through setting on lamina
There is opening 181 to admit air into the second gas channel T2.
In one embodiment, reference picture 5 and Fig. 7, exterior annular flow distribution plate 18 can be doubling plate, run through setting on each laminate
Opening 181 is equipped with to admit air into the second gas channel T2.Wherein, the wherein laminate in doubling plate is fixedly connected on shell
11 and the outer wall 133 of rotation detonation combustor 13, and another laminate can rotary motion adjusting into the second gas channel T2
Air mass flow.Here, exterior annular flow distribution plate 18 changes the big of opening 181 based on the dislocation between the two-layer in doubling plate
It is small, and then realize the regulation of air mass flow.
According in continuous rotation pinking tank of the present utility model, reference picture 1 and Fig. 8, oil circuit component 14 may include：For
Oil pipe line 141；Cartridge 142, is arranged at the outer wall 133 of rotation detonation combustor 13, is communicated in oil feed line 141 and rotation is quick-fried
Shake the annular firing chamber 135 of combustion chamber 13；And multiple nozzles 143, it is disposed through rotating the outer wall 133 of detonation combustor 13
With the corresponding position of cartridge 142 so that fuel in cartridge 142 enters rotation detonation combustor 13 via nozzle 143.
According in continuous rotation pinking tank of the present utility model, reference picture 1, power set 1 may also include：Blending room
19, the gas outlet 134 of the first gas channel T1, the second gas channel T2 and rotation detonation combustor 13 is connected, so that cooling
Air is blended with the gas after rotation detonating combustion.
According to continuous rotation pinking tank of the present utility model, in one embodiment, reference picture 1, power set 1 can also be wrapped
Include：First adjustable guider F1, is fixedly installed at the air intake 111 of shell 11；And the second adjustable guider F2, it is fixed
It is arranged at the porch of power turbine 162.First adjustable guider F1 is used to adjust the flowing side of the air entered in shell 11
To, and the second adjustable guider F2 is used to adjust into the flow direction of the high-temperature high-pressure fuel gas in power turbine 162 to control
The rotating speed and rotation direction (such as under brake condition) of power turbine 162.
According in continuous rotation pinking tank of the present utility model, reference picture 1, continuous rotation pinking tank can also be wrapped
Include：Blast pipe P, the exhaust outlet 112 for being arranged on the afterbody of shell 11 sentences the tail gas extraction for discharging power set 1.Due to this reality
Detonating combustion technology is employed with new continuous rotation pinking tank, ratio of combustion is more abundant, cause nitrogen oxygen in the tail gas for producing
The content of the air pollutants such as compound is substantially reduced, so as to reduce the pollution to environment.
According in continuous rotation pinking tank of the present utility model, reference picture 1, continuous rotation pinking tank can also be wrapped
Include：Boiler G, is communicated in blast pipe P so that the tail gas in blast pipe P is heated to boiler G, to realize the recycling of used heat,
So as to save the energy.Such as, the steam for being produced in boiler G can be used for for continuous rotation pinking tank generates electricity or heats.
Claims (10)
1. one kind continuously rotates pinking tank, including：
Tank body (2)；
Power set (1), are that tank body (2) provides power；
Characterized in that, power set (1) include：
Shell (11), has：
Air intake (111), is arranged at the front end of shell (11), in a ring, connects outside atmosphere；And
Exhaust outlet (112), is arranged at the rear end of shell (11)；
Centerbody (12), is in the form of a column, and is fixedly installed on the middle part of shell (11), and with along in the axially penetrating through of centerbody (12)
The intermediate throughholes (121) of heart body (12)；
Rotation detonation combustor (13), be sheathed on centerbody (12) and be fixedly connected on shell (11), and shell (11) air
Entrance (111) is communicated in rotation detonation combustor (13), with air-supplied to rotation detonation combustor (13)；
Oil circuit component (14), it is controlled to be communicated in rotation detonation combustor (13), provide fuel with to rotation detonation combustor (13)；
Igniter (15), is fixedly installed on rotation detonation combustor (13), for entering in rotation detonation combustor (13)
Fuel and air formed combustion gas lighted a fire, and then combustion gas rotation detonating combustion；And
Drive mechanism (16), including：
First is calmed the anger with component (161), is arranged in the intermediate throughholes (121) of centerbody (12), and shell (11) is entered for compressing
In air；
Second is calmed the anger with component (164), is arranged in first and calms the anger with component (161), and shell is entered for further compression
(11) air in；
Power turbine (162), the rotary motion under the gas-powered after rotating detonating combustion；And
Power transmission shaft (163), one end is connected to power turbine (162), and the other end is connected to tank body (2), so that power whirlpool
Wheel (162) does work to tank body (2).
2. continuous rotation pinking tank according to claim 1, it is characterised in that continuous rotation pinking tank also includes：
Decelerator (3), is arranged on the power transmission shaft (163) between power turbine (162) and tank body (2), power turbine (162) warp
Tank body (2) is connected to by decelerator (3) to be done work with to tank body (2).
3. it is according to claim 1 it is continuous rotation pinking tank, it is characterised in that first calms the anger is included with component (161)：
First compressor (1611), is arranged at the upstream of rotation detonation combustor (13)；
First turbine (1612), is arranged at the downstream of rotation detonation combustor (13)；And
First rotating shaft (1613), wears the intermediate throughholes (121) of centerbody (12), for connecting the first compressor (1611) and the
One turbine (1612).
4. it is according to claim 3 it is continuous rotation pinking tank, it is characterised in that
First rotating shaft (1613) is with the middle perforation (16131) for axially penetrating through first rotating shaft (1613) along centerbody (12)；
Second calms the anger is included with component (164)：
Second compressor (1641), is arranged at the upstream of the first compressor (1611)；
Second turbine (1642), is arranged at the downstream of the first turbine (1612)；And
Second rotating shaft (1643), is arranged in the middle perforation (16131) of first rotating shaft (1613), for connecting the second compressor
And the second turbine (1642) (1641).
5. it is according to claim 1 it is continuous rotation pinking tank, it is characterised in that rotation detonation combustor (13) have：
Air inlet (131)；
The first gas channel (T1) is formed between inwall (132), and the outside wall surface (122) of centerbody (12)；
Outer wall (133), forms the annular firing chamber (135) of rotation detonation combustor (13), shell (11) together with inwall (132)
Air intake (111) to be communicated in annular firing chamber (135) via air inlet (131) empty to feed to annular firing chamber (135)
The second gas channel (T2) is formed between gas, and outer wall (133) and shell (11)；And
Gas outlet (134), for gas discharge rotation detonation combustor (13) after rotation detonating combustion.
6. it is according to claim 5 it is continuous rotation pinking tank, it is characterised in that power set (1) also include：
Interior annular flow distribution plate (17), is arranged at the first gas channel (T1) porch, and the first gas channel is entered for adjusting
(T1) air mass flow in.
7. it is according to claim 5 it is continuous rotation pinking tank, it is characterised in that power set (1) also include：
Exterior annular flow distribution plate (18), is arranged at the second gas channel (T2) porch, and the second gas channel is entered for adjusting
(T2) air mass flow in.
8. it is according to claim 5 it is continuous rotation pinking tank, it is characterised in that oil circuit component (14) includes：
Oil feed line (141)；
Cartridge (142), is arranged at the outer wall (133) of rotation detonation combustor (13), is communicated in oil feed line (141) and rotation
The annular firing chamber (135) of detonation combustor (13)；And
Multiple nozzles (143), be disposed through rotate detonation combustor (13) outer wall (133) it is corresponding with cartridge (142)
Position so that fuel in cartridge (142) enters rotation detonation combustor (13) via nozzle (143).
9. it is according to claim 5 it is continuous rotation pinking tank, it is characterised in that power set (1) also include：Blending room
(19), the gas outlet (134) of the first gas channel of connection (T1), the second gas channel (T2) and rotation detonation combustor (13),
So that the air of cooling is blended with the gas after rotation detonating combustion.
10. it is according to claim 1 it is continuous rotation pinking tank, it is characterised in that power set (1) also include：
First adjustable guider (F1), is fixedly installed on air intake (111) place of shell (11)；And
Second adjustable guider (F2), is fixedly installed on the porch of power turbine (162).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621195676.1U CN206205998U (en) | 2016-10-28 | 2016-10-28 | Continuous rotation pinking tank |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621195676.1U CN206205998U (en) | 2016-10-28 | 2016-10-28 | Continuous rotation pinking tank |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206205998U true CN206205998U (en) | 2017-05-31 |
Family
ID=58751736
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621195676.1U Active CN206205998U (en) | 2016-10-28 | 2016-10-28 | Continuous rotation pinking tank |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206205998U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106337738A (en) * | 2016-10-28 | 2017-01-18 | 清华大学 | Continuously rotating detonation tank |
| CN110219735A (en) * | 2018-03-01 | 2019-09-10 | 通用电气公司 | Turbogenerator with rotation detonation combustion system |
| CN113266850A (en) * | 2017-06-09 | 2021-08-17 | 通用电气公司 | Variable geometry rotary detonation combustor and method of operating same |
-
2016
- 2016-10-28 CN CN201621195676.1U patent/CN206205998U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106337738A (en) * | 2016-10-28 | 2017-01-18 | 清华大学 | Continuously rotating detonation tank |
| CN113266850A (en) * | 2017-06-09 | 2021-08-17 | 通用电气公司 | Variable geometry rotary detonation combustor and method of operating same |
| CN110219735A (en) * | 2018-03-01 | 2019-09-10 | 通用电气公司 | Turbogenerator with rotation detonation combustion system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106285945B (en) | Continuous rotation pinking generator | |
| CN104153884B (en) | A kind of rotation pinking gas turbine | |
| CN102165168B (en) | Gas turbine for discontinuous combustion | |
| CN100390376C (en) | External combustion rotary piston engine | |
| CN206205998U (en) | Continuous rotation pinking tank | |
| CN204082338U (en) | A kind of rotation pinking gas turbine | |
| CN108708788A (en) | Double-combustion-chamber ramjet engine and hypersonic aircraft | |
| CN206205999U (en) | Continuous rotation pinking generator | |
| CN105972638B (en) | A kind of reverse-flow type pulse detonation combustor | |
| US3541787A (en) | Self-compressed continuous circular internal combustion engine | |
| CN101275741A (en) | Pulse vector high-pressure burner | |
| CN206205997U (en) | Continuous rotation pinking naval vessel | |
| CN106337738B (en) | Continuous rotation pinking tank | |
| CN104963774B (en) | A kind of turbine | |
| CN108518673A (en) | Vortex-spraying type combustor | |
| CN100540864C (en) | Rotary engine | |
| CN102278198B (en) | Water-oil mixed combustion rotating engine | |
| CN102235234B (en) | Ignition type roll spin engine | |
| CN108757221A (en) | A kind of liquid Asia burning ramjet | |
| CN106368820B (en) | Continuous rotation pinking naval vessel | |
| CN202055913U (en) | Water-oil combustion type rotary engine | |
| CN109356718B (en) | Simple cycle engine with combustion chamber compressor driven by continuously variable transmission | |
| CN1197159A (en) | Dual rotors reversly-acting rotary I. C. engine | |
| CN106593650A (en) | Detonation turbine engine | |
| RU2101517C1 (en) | Coal-burning engine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant |