CN101008342A - Inner wing air heat dissipation equipment - Google Patents

Inner wing air heat dissipation equipment Download PDF

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Publication number
CN101008342A
CN101008342A CNA2007100131826A CN200710013182A CN101008342A CN 101008342 A CN101008342 A CN 101008342A CN A2007100131826 A CNA2007100131826 A CN A2007100131826A CN 200710013182 A CN200710013182 A CN 200710013182A CN 101008342 A CN101008342 A CN 101008342A
Authority
CN
China
Prior art keywords
air
heat dissipation
cylinder
inner wing
dissipation equipment
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
CNA2007100131826A
Other languages
Chinese (zh)
Inventor
宋绪文
武斌
朱明�
张传彪
霍玉军
张峰
贾洪涛
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.)
SHANDONG TONGCHUANG QUICHE SHANRE ZHUANGZHI CO Ltd
Original Assignee
宋绪文
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 宋绪文 filed Critical 宋绪文
Priority to CNA2007100131826A priority Critical patent/CN101008342A/en
Publication of CN101008342A publication Critical patent/CN101008342A/en
Pending legal-status Critical Current

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    • 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

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Abstract

The invention relates to an internal fin air radiator for radiating the heat of inlet air in high-power internal-combustion engine. The invention uses air tube 2 and internal fin 3 to radiate the heat of air, and cool the inlet air of cylinder, to improve the air density of cylinder and burn the fuel completely, reduce the waste pollution.

Description

Inner wing air heat dissipation equipment
Technical field
The present invention relates to a kind of device that the inlet air of high-power internal combustion engine cylinder is dispelled the heat, specifically a kind of inner wing air heat dissipation equipment, it can carry out cooling heat dissipation to the air that high-power internal combustion engine motor enters cylinder, to reduce the temperature that high-power internal combustion engine motor enters the air of cylinder, improve the density of inlet air, make cylinder more abundant the right burning work of right material.
Background technique
The domestic air that high-power internal combustion engine motor is entered in the cylinder does not all have good heat dissipating method at present, even does not fundamentally have sink.According to the principle of expanding with heat and contract with cold, the air temperature that enters in the cylinder is high more, and the density of air is just more little in the cylinder, air density is more little, and the air quantity that enters in the cylinder is just few more, so the burning of fuel is just insufficient during cylinder operation, the response of waste gas discharge capacity increases, and severe contamination ambient air.
Summary of the invention
The present invention provides a kind of simple in structure for overcoming the prior art deficiency, and volume is little easy to use, can realize the air that high-power internal combustion engine motor enters cylinder is carried out the inner wing air heat dissipation equipment of cooling heat dissipation.
The objective of the invention is to adopt following proposal to realize: the internal combustion engine inner wing air heat dissipation equipment, be by suction chamber, airflow duct, internal fin, discharge chamber constitute, design is by loading onto internal fin in airflow duct, internal fin mainly plays the effect of the air of the cylinder that enters internal combustion engine being carried out the heat conduction cooling, and all air that enter cylinder must cool off by internal fin.
After air cools off by internal fin, reach the purpose of cooling, improve the air density that enters in the cylinder, increased the air quantity that enters in the cylinder, make the burning that enters cylinder fuel more abundant, the discharge capacity of carbon dioxide is greatly reduced.
Description of drawings
Fig. 1 is an inner wing air heat dissipation equipment general assembly drawing of the present invention;
Fig. 2 is the airflow duct of inner wing air heat dissipation equipment of the present invention and the ssembly drawing of internal fin;
Fig. 3 is the sectional view of Fig. 2;
Fig. 4 is the internal fin figure of inner wing air heat dissipation equipment of the present invention;
Fig. 5 is the sectional view of Fig. 4.
Wherein, 1, suction chamber, 2, airflow duct, 3, internal fin, 4, discharge chamber.
Embodiment
Below in conjunction with accompanying drawing and embodiment, the present invention is further described.
Embodiment:
As Fig. 1, Fig. 2, shown in Figure 3, inner wing air heat dissipation equipment is mainly by suction chamber 1, airflow duct 2, and internal fin 3, discharge chamber 4 constitutes.The upper end of airflow duct 2 communicates with suction chamber 1, and the lower end communicates with discharge chamber 4.Internal fin 3 designs are installed in the airflow duct 2, it mainly plays a part the conduction heat (because of the temperature of nature is good conduction material) in the air of nature uniformly of the hot airs in the airflow duct 2, internal fin 3 is aluminum alloy plate materials of selecting good heat conductivity for use, be pressed into saw wing shape with press machine, please refer to Fig. 4, Fig. 5, its interior wing angle is designed to angle 45 and spends to 70 degree.
During work, please refer to Fig. 1, the above high temperature air of 80 degree by the supply of pneumatics pump, enter suction chamber 1, then through airflow duct 2 and internal fin 3, at this moment airflow duct 2 and internal fin 3, all be full of high temperature air, because the outside of airflow duct 2 is in the normal temperature air of nature, therefore the temperature of the high temperature air in the airflow duct 2 is delivered in the air of nature uniformly by internal fin 3 and airflow duct 2, because of the air of nature is a kind of good heat radiation material, thus the above air of 80 degree of supplying with by the pneumatics pump through internal fin 3 and airflow duct 2 with thermal energy conduction to nature air, therefore reached the purpose of cooling, cooling can drop to 45 degree by 80 degree, promptly by the air temperature that enters 80 degree in the suction chamber 1, through airflow duct 2, behind internal fin 3 and the discharge chamber 4, air can drop to 45 degree.Temperature drops to 45 when spending, at this moment air enters in the cylinder through discharge chamber 4, principle according to rising-heat contracting-cold, improved the density of air behind the air cooling-down, the air quantity response that enters in the cylinder increases, and institute is so that during the cylinder acting, the burning of fuel is more abundant, be improved thereby the motor worker is led, the carbon dioxide pollution of discharge greatly reduces.

Claims (2)

1, a kind of inner wing air heat dissipation equipment, the inner wing air heat dissipation equipment that it is made of suction chamber 1, airflow duct 2, internal fin 3, discharge chamber 4, it is characterized in that: the upper end of airflow duct 2 is connected with suction chamber 1 and communicates, the lower end of airflow duct 2 is connected with discharge chamber 4 and communicates, and internal fin 3 design and installations are in airflow duct 2.
2, inner wing air heat dissipation equipment according to claim 1 is characterized in that: the design angle at the interior wing angle of described internal fin 3 be 45 spend to 70 the degree.
CNA2007100131826A 2007-01-24 2007-01-24 Inner wing air heat dissipation equipment Pending CN101008342A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNA2007100131826A CN101008342A (en) 2007-01-24 2007-01-24 Inner wing air heat dissipation equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNA2007100131826A CN101008342A (en) 2007-01-24 2007-01-24 Inner wing air heat dissipation equipment

Publications (1)

Publication Number Publication Date
CN101008342A true CN101008342A (en) 2007-08-01

Family

ID=38696953

Family Applications (1)

Application Number Title Priority Date Filing Date
CNA2007100131826A Pending CN101008342A (en) 2007-01-24 2007-01-24 Inner wing air heat dissipation equipment

Country Status (1)

Country Link
CN (1) CN101008342A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114934840A (en) * 2022-06-01 2022-08-23 浙江银轮新能源热管理系统有限公司 Intercooler core and intercooler assembly

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114934840A (en) * 2022-06-01 2022-08-23 浙江银轮新能源热管理系统有限公司 Intercooler core and intercooler assembly
CN114934840B (en) * 2022-06-01 2023-11-03 浙江银轮新能源热管理系统有限公司 Intercooler core and intercooler assembly

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Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
ASS Succession or assignment of patent right

Owner name: SHANDONG TONGCHUANG AUTOMOBILE HEAT RADIATING DEV

Free format text: FORMER OWNER: SONG XUWEN

Effective date: 20071214

C41 Transfer of patent application or patent right or utility model
TA01 Transfer of patent application right

Effective date of registration: 20071214

Address after: Postal code of Ningyang Industrial Park, Shandong Province: 271411

Applicant after: Shandong Tongchuang Quiche Shanre Zhuangzhi Co., Ltd.

Address before: Shandong province Tai'an County Ningyang kiln high tech Zone Code: 271000

Applicant before: Song Xuwen

C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication