CN110486136A - A kind of axis Transmission Engine cooling system - Google Patents

A kind of axis Transmission Engine cooling system Download PDF

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Publication number
CN110486136A
CN110486136A CN201810946515.9A CN201810946515A CN110486136A CN 110486136 A CN110486136 A CN 110486136A CN 201810946515 A CN201810946515 A CN 201810946515A CN 110486136 A CN110486136 A CN 110486136A
Authority
CN
China
Prior art keywords
fan
turbine
engine
duct
cooling system
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
CN201810946515.9A
Other languages
Chinese (zh)
Inventor
靳北彪
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.)
Entropy Zero Technology Logic Engineering Group Co Ltd
Original Assignee
Entropy Zero Technology Logic Engineering Group Co Ltd
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 Entropy Zero Technology Logic Engineering Group Co Ltd filed Critical Entropy Zero Technology Logic Engineering Group Co Ltd
Publication of CN110486136A publication Critical patent/CN110486136A/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
    • F01NGAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR MACHINES OR ENGINES IN GENERAL; GAS-FLOW SILENCERS OR EXHAUST APPARATUS FOR INTERNAL COMBUSTION ENGINES
    • F01N5/00Exhaust or silencing apparatus combined or associated with devices profiting from exhaust energy
    • F01N5/02Exhaust or silencing apparatus combined or associated with devices profiting from exhaust energy the devices using heat
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P11/00Component parts, details, or accessories not provided for in, or of interest apart from, groups F01P1/00 - F01P9/00
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P5/00Pumping cooling-air or liquid coolants
    • F01P5/02Pumping cooling-air; Arrangements of cooling-air pumps, e.g. fans or blowers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P5/00Pumping cooling-air or liquid coolants
    • F01P5/02Pumping cooling-air; Arrangements of cooling-air pumps, e.g. fans or blowers
    • F01P2005/025Pumping cooling-air; Arrangements of cooling-air pumps, e.g. fans or blowers using two or more air pumps
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Abstract

The invention discloses a kind of axis Transmission Engine cooling systems, including fan and turbine, the fan is arranged in duct, the turbine is arranged in the duct, from the fan in setting gradually radiator and exhaust entrance in the duct and in the fan and the turbine, the fan and turbomachinery transmission are arranged on the direction of the turbine.Axis Transmission Engine cooling system disclosed in this invention can efficiently cool down engine using the waste heat of engine, and then promote the whole efficiency of engine.

Description

A kind of axis Transmission Engine cooling system
Technical field
The present invention relates to thermal energy and dynamic field more particularly to axis Transmission Engine cooling systems.
Background technique
The wasted work of engine-cooling system is generally 5% to the 10% of engine power, if it is possible to utilize engine Waste heat reduces or completely eliminates this part of wasted work and is of great significance to the promotion of overall engine efficiency.Therefore, it is necessary to send out Bright one kind can utilize the novel cooling system of engine of engine complementary energy.
Summary of the invention
To solve the above-mentioned problems, technical solution proposed by the present invention is as follows:
Scheme 1: a kind of axis Transmission Engine cooling system, including fan and turbine, the fan are arranged in duct, institute Turbine is stated to be arranged in the duct, from the fan on the direction of the turbine in the duct and in the fan Radiator and exhaust entrance are set gradually between the turbine, the fan and turbomachinery transmission are arranged.
Scheme 2: on the basis of scheme 1, further setting is used for and driving engine on the line shaft of the fan The structure of connection.
Scheme 3: on the basis of scheme 1, further setting is used for and driving engine on the line shaft of the turbine The structure of connection.
Scheme 4: on the basis of scheme 2, further setting is used for and driving engine on the line shaft of the turbine The structure of connection.
Scheme 5: in scheme 2 to 4 on the basis of either a program, further make described for being connect with driving engine Structure and engine power system transmission are arranged.
Scheme 6: in scheme 1 to 4 on the basis of either a program, further make the exhaust of the exhaust entrance and engine Road connection setting.
Scheme 7: on the basis of scheme 5, the exhaust entrance is further made to be connected to setting with the exhaust duct of engine.
Scheme 8: a kind of axis Transmission Engine cooling system, including fan and turbine, the fan are arranged in duct A, The turbine is arranged in duct B, in the downstream of the fan in radiator, the outlet of the duct A are arranged in the duct A Setting is connected to the low-pressure fluid entrance of jet pump, the fluid outlet of the jet pump is connected to the fluid inlet of the duct B Setting, the fan and turbomachinery transmission are arranged.
Scheme 9: on the basis of scheme 8, further setting is used for and driving engine on the line shaft of the fan The structure of connection.
Scheme 10: on the basis of scheme 8, further setting is used for and driving engine on the line shaft of the turbine The structure of connection.
Scheme 11: on the basis of scheme 9, further setting is used for and driving engine on the line shaft of the turbine The structure of connection.
Scheme 12: in scheme 9 to 11 on the basis of either a program, further make described for being connect with driving engine Structure and engine power system transmission be arranged.
Scheme 13: in scheme 8 to 11 on the basis of either a program, further make the driving fluid entrance of the jet pump Setting is connected to the exhaust duct of engine.
Scheme 14: on the basis of scheme 12, further make driving fluid entrance and the row of engine of the jet pump Air flue connection setting.
In the present invention, it is selectively chosen two parts for making the duct A and the duct B be set as same duct.
In the present invention, so-called " A and B transmission are arranged " refers to the machine of the mechanical connection setting piece and B and/or B of A and/or A Tool connects setting piece transmission setting.
In the present invention, necessary component, list should be set in necessary place according to the well-known technique of thermal energy and dynamic field Member or system etc..
Beneficial effects of the present invention are as follows: axis Transmission Engine cooling system disclosed in this invention can efficiently utilize hair The waste heat of motivation cools down engine, and then promotes the whole efficiency of engine.
Detailed description of the invention
Fig. 1: the structural schematic diagram of the embodiment of the present invention 1;
Fig. 2: the structural schematic diagram of the embodiment of the present invention 5;
Fig. 3: the structural schematic diagram of the embodiment of the present invention 6;
Fig. 4: the structural schematic diagram of the embodiment of the present invention 7;
In figure: 1 fan, 2 turbines, 3 ducts, 5 radiators, 6 exhaust entrances, the exhaust duct of 7 engines, 8 jet pumps, 31 contain Road A, 32 duct B.
Specific embodiment
Embodiment 1
A kind of axis Transmission Engine cooling system, as shown in Figure 1, including fan 1 and turbine 2, the setting of fan 1 is being contained In road 3, the turbine 2 is arranged in the duct 3, from the fan 1 on the direction of the turbine 2 in the duct 3 It is interior and radiator 5 and exhaust entrance 6 are set gradually between the fan 1 and the turbine 2, the fan 1 and the turbine 2 Machine driving setting.
Embodiment 2
A kind of axis Transmission Engine cooling system, on the basis of embodiment 1, further in the line shaft of the fan 1 The upper structure being arranged for being connect with driving engine.
Embodiment 3
A kind of axis Transmission Engine cooling system, on the basis of embodiment 1, further in the line shaft of the turbine 2 The upper structure being arranged for being connect with driving engine.
Embodiment 4
A kind of axis Transmission Engine cooling system, on the basis of embodiment 2, further in the line shaft of the turbine 2 The upper structure being arranged for being connect with driving engine.
Embodiment 5
A kind of axis Transmission Engine cooling system, as shown in Fig. 2, on the basis of embodiment 1, further making the exhaust Entrance 6 is connected to setting with the exhaust duct 7 of engine.
As disposable embodiment, the embodiment of the present invention 2 to embodiment 4 can further make the exhaust entrance 6 Setting is connected to the exhaust duct 7 of engine.
Embodiment 6
A kind of axis Transmission Engine cooling system, as shown in figure 3, including fan 1 and turbine 2, the setting of fan 1 is being contained In road A 31, the turbine 2 is arranged in duct B 32, in the downstream of the fan 1 in setting heat dissipation in the duct A 31 Device 5, the outlet of the duct A 31 are connected to setting with the low-pressure fluid entrance of jet pump 8, the fluid outlet of the jet pump 8 with The fluid inlet of the duct B 32 is connected to setting, and the fan 1 is arranged with 2 machine driving of turbine.
As disposable embodiment, the embodiment of the present invention 6, which can be further arranged on the line shaft of the fan 1, to be used In the structure being connect with driving engine.
As disposable embodiment, the embodiment of the present invention 6 and its disposable embodiment can be further in institutes State the structure being arranged on the line shaft of turbine 2 for connecting with driving engine.
Embodiment 7
A kind of axis Transmission Engine cooling system, as shown in figure 4, further making the jet stream on the basis of embodiment 6 The driving fluid entrance of pump 8 is connected to setting with the exhaust duct 7 of engine.
As disposable embodiment, the disposable embodiment of the embodiment of the present invention 6 can further make described The driving fluid entrance of jet pump 8 is connected to setting with the exhaust duct 7 of engine.
As disposable embodiment, the aforementioned all realities comprising the structure for being connect with driving engine of the present invention Applying mode can further be such that the structure for connecting with driving engine and engine power system transmission is arranged.
It is clear that the invention is not restricted to above embodiments, according to techniques known and technology disclosed in this invention Scheme, can derive or associate many variant schemes out, and all these variant schemes also are regarded as being protection model of the invention It encloses.

Claims (10)

1. a kind of axis Transmission Engine cooling system, including fan (1) and turbine (2), it is characterised in that: the fan (1) sets It sets in duct (3), turbine (2) setting is in the duct (3), in the side from the fan (1) to the turbine (2) Set gradually in the duct (3) and between the fan (1) and the turbine (2) upwards radiator (5) and be vented into Mouth (6), the fan (1) and the turbine (2) machine driving are arranged.
2. axis Transmission Engine cooling system as described in claim 1, it is characterised in that: on the line shaft of the fan (1) Structure for connecting with driving engine is set.
3. axis Transmission Engine cooling system as described in claim 1, it is characterised in that: on the line shaft of the turbine (2) Structure for connecting with driving engine is set.
4. axis Transmission Engine cooling system as claimed in claim 2, it is characterised in that: on the line shaft of the turbine (2) Structure for connecting with driving engine is set.
5. the axis Transmission Engine cooling system as described in any one of claim 2 to 4, it is characterised in that: described to be used for and hair The structure of motivation transmission connection and engine power system transmission are arranged.
6. the axis Transmission Engine cooling system as described in any one of claims 1 to 4, it is characterised in that: the exhaust entrance (6) setting is connected to the exhaust duct of engine (7).
7. axis Transmission Engine cooling system as claimed in claim 5, it is characterised in that: the exhaust entrance (6) and engine Exhaust duct (7) be connected to setting.
8. a kind of axis Transmission Engine cooling system, including fan (1) and turbine (2), it is characterised in that: the fan (1) sets It sets in duct A (31), turbine (2) setting is in duct B (32), in the downstream of the fan (1) in the duct A (31) radiator (5) are set in, the outlet of the duct A (31) is connected to setting with the low-pressure fluid entrance of jet pump (8), described The fluid outlet of jet pump (8) is connected to setting with the fluid inlet of the duct B (32), the fan (1) and the turbine (2) Machine driving setting.
9. axis Transmission Engine cooling system as claimed in claim 8, it is characterised in that: on the line shaft of the fan (1) Structure for connecting with driving engine is set, and/or is arranged on the line shaft of the turbine (2) for being passed with engine The structure of dynamic connection.
10. axis Transmission Engine cooling system as claimed in claim 9, it is characterised in that: described for connecting with driving engine Structure and the engine power system transmission connect is arranged.
CN201810946515.9A 2017-08-29 2018-08-20 A kind of axis Transmission Engine cooling system Pending CN110486136A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201710758918 2017-08-29
CN2017107589186 2017-08-29

Publications (1)

Publication Number Publication Date
CN110486136A true CN110486136A (en) 2019-11-22

Family

ID=68545603

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201810946515.9A Pending CN110486136A (en) 2017-08-29 2018-08-20 A kind of axis Transmission Engine cooling system

Country Status (1)

Country Link
CN (1) CN110486136A (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201851226U (en) * 2010-08-06 2011-06-01 靳北彪 Compressed exhausting and self-cooling system
CN102213158A (en) * 2010-08-06 2011-10-12 靳北彪 Compression type exhaust gas self cooling system
CN103029839A (en) * 2011-12-23 2013-04-10 摩尔动力(北京)技术股份有限公司 External combustion aerial vehicle
CN103046992A (en) * 2011-12-29 2013-04-17 摩尔动力(北京)技术股份有限公司 Unpowered fan radiator
CN104595032A (en) * 2014-11-19 2015-05-06 上海交通大学 Multi-fan turbine thrust system with ultra-large bypass ratio

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN201851226U (en) * 2010-08-06 2011-06-01 靳北彪 Compressed exhausting and self-cooling system
CN102213158A (en) * 2010-08-06 2011-10-12 靳北彪 Compression type exhaust gas self cooling system
CN103029839A (en) * 2011-12-23 2013-04-10 摩尔动力(北京)技术股份有限公司 External combustion aerial vehicle
CN103046992A (en) * 2011-12-29 2013-04-17 摩尔动力(北京)技术股份有限公司 Unpowered fan radiator
CN104595032A (en) * 2014-11-19 2015-05-06 上海交通大学 Multi-fan turbine thrust system with ultra-large bypass ratio

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Application publication date: 20191122

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