CN105863747A - Novel turbine engine - Google Patents

Novel turbine engine Download PDF

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Publication number
CN105863747A
CN105863747A CN201610289838.6A CN201610289838A CN105863747A CN 105863747 A CN105863747 A CN 105863747A CN 201610289838 A CN201610289838 A CN 201610289838A CN 105863747 A CN105863747 A CN 105863747A
Authority
CN
China
Prior art keywords
turbine
housing
turbo blade
closed
novel
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.)
Pending
Application number
CN201610289838.6A
Other languages
Chinese (zh)
Inventor
李宏生
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN201610289838.6A priority Critical patent/CN105863747A/en
Publication of CN105863747A publication Critical patent/CN105863747A/en
Pending legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08Cooling; Heating; Heat-insulation
    • F01D25/12Cooling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/141Shape, i.e. outer, aerodynamic form

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

The invention provides a novel turbine engine which comprises a shell, a gas compressor, a combustion chamber and a turbine. The gas compressor, the combustion chamber and the turbine are arranged in the shell. A water inlet device is arranged in the space between the outer rear side of the combustion chamber and the turbine. Due to the water inlet device, the purpose of prolonging the service life by lowering the heat of the engine is achieved, water discharged by the water inlet device is vaporized instantly, turbine blades are promoted to rotate, and the power of the turbine engine is improved. In addition, a closed turbine structure is mounted behind the turbine, blocks the space of the rear portion of the shell and shares a shaft with the turbine. An energy inlet is formed in one side of the closed turbine structure; an energy outlet is formed in the other side of the closed turbine structure; the energy inlet communicates with the space on the rear portion of the shell; and the energy outlet is used as a tail gas discharge opening. By the adoption of the closed turbine structure, waste gas discharged by the engine can be recycled, and therefore the acting power of gas is improved.

Description

Novel turbine electromotor
Technical field
The present invention relates to a kind of Novel turbine electromotor, belong to technical field of engines.
Background technology
Existing turbogenerator, owing to running in high temperature environments for a long time, therefore greatly reduces service life.Additionally, it is existing Turbogenerator there is the problem that is short of power.
Summary of the invention
For above not enough, the present invention provides a kind of Novel turbine electromotor, reduces the heat of electromotor by increasing water feed apparatus Amount, thus increase the service life.
Technical scheme: Novel turbine electromotor, compressor, combustor and the whirlpool being provided with including housing and enclosure interior Wheel, is provided with water feed apparatus at the space between combustor outside back and turbine.
Closed type turbine structure is installed at the rear of described turbine, closed type turbine structure by the steric block of rear and with Turbine common axis;The side of described closed type turbine structure is provided with energy inlet, and the opposite side of closed type turbine structure is provided with energy Outlet, described energy inlet connects with the space of rear, and described energy outlet drains mouth as tail gas.Closed type turbine is tied The employing of structure, waste gas recovery recycling electromotor can discharged, and then improve the working power of gas.
Described closed type turbine structure is: constituted a closed cavity by circular shell and both sides end cap, at closed cavity Internally installed have turbo blade, and the interior center of turbo blade and axle assembly connection, between outward flange and the circular shell of turbo blade And it is respectively kept with running clearance between the outward flange of turbo blade and both sides end cap.Described turbo blade is straight-tooth shape.
The turbine structure that the present invention increases is enclosed construction, and due to the outside by the inwall of turbine circular shell Yu turbo blade Edge is designed to fit tightly and can enable the freely rotatable structure of turbo blade, is similar to piston structure, hence in so that enter new The gas of type turbogenerator can fully drive turbo blade to rotate and make energy dissipation be preferably minimized, thus improves doing of gas Effect rate.
Beneficial effects of the present invention: the turbogenerator that the present invention provides, owing to adding water feed apparatus, not only by reduction Heat of engine reaches the purpose increased the service life, and the instant water that water feed apparatus can be made to discharge vaporizes, and then promotes whirlpool The rotation of impeller blade, improves the power of turbogenerator.
Accompanying drawing explanation
Fig. 1 is the structural representation one of the present invention.
Fig. 2 is the structural representation two of the present invention.
Fig. 3 is the structural representation of inventive closure formula turbine structure.
Detailed description of the invention
A kind of Novel turbine electromotor as shown in Figure 1 to Figure 3, including housing 2 and housing 2 internal be provided with compressor 1, Combustor 3 and turbine 4, be provided with water feed apparatus 9 at the space between combustor 3 outside back and turbine 4.
Being provided with closed type turbine structure 6 at the rear of described turbine 4, closed type turbine structure 6 is by the space at housing 2 rear portion Block and with turbine 4 common axis 8;The side of described closed type turbine structure 6 is provided with energy inlet 5, closed type turbine structure The opposite side of 6 is provided with energy outlet 7, and described energy inlet 5 connects with the space at housing 2 rear portion, and described energy outlet 7 is made Mouth is drained for tail gas.
Described closed type turbine structure 6 is: constituted a closed cavity by circular shell 11 and both sides end cap 12, is closing The internally installed of formula cavity has turbo blade 10, and the interior center of turbo blade 4 and axle 8 assembly connection, outside turbo blade 10 It is respectively kept with running clearance between edge and circular shell 5 and between the outward flange of turbo blade 10 and both sides end cap 12.Institute State turbo blade 10 in straight-tooth shape.
During work, the waste gas that combustor 3 gives off enters in closed type turbine structure 6 through turbine 4 and energy inlet 5, by Inwall in outward flange and the circular shell 11 of turbo blade 10 rotates laminating, and therefore waste gas continues to press on turbo blade 10 and revolves Turning, when waste gas rotates to energy outlet 7 along with turbo blade 10, waste gas is discharged, and now turbo blade 10 generation is dynamic Continuation drive turbine 4 is rotated by power, thus improves the working power of turbogenerator self.

Claims (4)

1. Novel turbine electromotor, including internal compressor (1), combustor (3) and the whirlpool being provided with of housing (2) and housing (2) Wheel (4), it is characterised in that: it is provided with water feed apparatus at the space between combustor (3) outside back and turbine (4) (9)。
2. Novel turbine electromotor as claimed in claim 1, it is characterised in that: at the rear of described turbine (4), closing is installed Formula turbine structure (6), closed type turbine structure (6) by the steric block at housing (2) rear portion and shares with turbine (4) Axle (8);The side of described closed type turbine structure (6) is provided with energy inlet (5), closed type turbine structure (6) Opposite side is provided with energy outlet (7), and described energy inlet (5) connects with the space at housing (2) rear portion, described energy Outlet (7) drains mouth as tail gas.
3. Novel turbine electromotor as claimed in claim 2, it is characterised in that described closed type turbine structure (6) is: by ring-type Housing (11) and both sides end cap (12) constitute a closed cavity, and internally installed at closed cavity has turbine leaf Sheet (10), the interior center of turbo blade (4) and axle (8) assembly connection, the outward flange of turbo blade (10) is with ring-type It is respectively kept with running clearance between housing (5) and between the outward flange of turbo blade (10) and both sides end cap (12).
4. Novel turbine electromotor as claimed in claim 3, it is characterised in that: described turbo blade (10) is in straight-tooth shape.
CN201610289838.6A 2016-04-23 2016-04-23 Novel turbine engine Pending CN105863747A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610289838.6A CN105863747A (en) 2016-04-23 2016-04-23 Novel turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610289838.6A CN105863747A (en) 2016-04-23 2016-04-23 Novel turbine engine

Publications (1)

Publication Number Publication Date
CN105863747A true CN105863747A (en) 2016-08-17

Family

ID=56630298

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610289838.6A Pending CN105863747A (en) 2016-04-23 2016-04-23 Novel turbine engine

Country Status (1)

Country Link
CN (1) CN105863747A (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB884646A (en) * 1958-11-26 1961-12-13 Daimler Benz Ag Improvements relating to gas turbine power plants
CN102410056A (en) * 2010-09-20 2012-04-11 谭波 Waste gas turbine
CN203239459U (en) * 2013-03-07 2013-10-16 李一习 Turboshaft engine for vehicles
CN104675520A (en) * 2013-11-29 2015-06-03 杨兴隆 Novel super-energy-saving gas turbine
CN104763573A (en) * 2015-03-05 2015-07-08 李宏生 Turbine structure
CN104989579A (en) * 2015-07-01 2015-10-21 李宏生 Novel water conservancy steam power generation turbine
CN206071653U (en) * 2016-04-23 2017-04-05 李宏生 Novel turbine electromotor

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB884646A (en) * 1958-11-26 1961-12-13 Daimler Benz Ag Improvements relating to gas turbine power plants
CN102410056A (en) * 2010-09-20 2012-04-11 谭波 Waste gas turbine
CN203239459U (en) * 2013-03-07 2013-10-16 李一习 Turboshaft engine for vehicles
CN104675520A (en) * 2013-11-29 2015-06-03 杨兴隆 Novel super-energy-saving gas turbine
CN104763573A (en) * 2015-03-05 2015-07-08 李宏生 Turbine structure
CN104989579A (en) * 2015-07-01 2015-10-21 李宏生 Novel water conservancy steam power generation turbine
CN206071653U (en) * 2016-04-23 2017-04-05 李宏生 Novel turbine electromotor

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DD01 Delivery of document by public notice

Addressee: Li Hongsheng

Document name: Notice of First Examination Opinion

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WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20160817