CN113217182A - 双斜面体，多滑片，多燃烧室，滚动循环，轮流做功发动机 - Google Patents
双斜面体，多滑片，多燃烧室，滚动循环，轮流做功发动机 Download PDFInfo
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- CN113217182A CN113217182A CN202110493349.3A CN202110493349A CN113217182A CN 113217182 A CN113217182 A CN 113217182A CN 202110493349 A CN202110493349 A CN 202110493349A CN 113217182 A CN113217182 A CN 113217182A
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- 238000002485 combustion reaction Methods 0.000 claims abstract description 26
- 230000006835 compression Effects 0.000 claims abstract description 4
- 238000007906 compression Methods 0.000 claims abstract description 4
- 230000000295 complement effect Effects 0.000 claims description 3
- 238000002347 injection Methods 0.000 claims description 2
- 239000007924 injection Substances 0.000 claims description 2
- 238000005096 rolling process Methods 0.000 claims description 2
- 238000004880 explosion Methods 0.000 claims 1
- 238000007789 sealing Methods 0.000 claims 1
- 239000003502 gasoline Substances 0.000 abstract description 5
- 239000002360 explosive Substances 0.000 abstract description 3
- 239000000567 combustion gas Substances 0.000 abstract 1
- 239000007789 gas Substances 0.000 description 7
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 6
- 239000000498 cooling water Substances 0.000 description 3
- 239000002283 diesel fuel Substances 0.000 description 3
- 229910052742 iron Inorganic materials 0.000 description 3
- 239000000446 fuel Substances 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 239000002912 waste gas Substances 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000007123 defense Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 239000003350 kerosene Substances 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000003345 natural gas Substances 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 239000007858 starting material Substances 0.000 description 1
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B53/00—Internal-combustion aspects of rotary-piston or oscillating-piston engines
- F02B53/04—Charge admission or combustion-gas discharge
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B55/00—Internal-combustion aspects of rotary pistons; Outer members for co-operation with rotary pistons
- F02B55/02—Pistons
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B55/00—Internal-combustion aspects of rotary pistons; Outer members for co-operation with rotary pistons
- F02B55/02—Pistons
- F02B55/04—Cooling thereof
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B55/00—Internal-combustion aspects of rotary pistons; Outer members for co-operation with rotary pistons
- F02B55/08—Outer members for co-operation with rotary pistons; Casings
- F02B55/10—Cooling thereof
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B55/00—Internal-combustion aspects of rotary pistons; Outer members for co-operation with rotary pistons
- F02B55/14—Shapes or constructions of combustion chambers
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- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
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- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Geometry (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
双斜面体，多滑片，多燃烧室，滚动循环，轮流做功发动机本发动机由固定的配合的斜面体4，配合的斜面体9，与转动的滑片轮5构成。滑片轮5中装有滑片组，滑片组包括滑片1，弹簧11，滑柱12，圆珠13组成。斜面体4的斜面与滑片1，滑片轮5，包容成与滑片数相同的燃烧室3，在运行中只用一套进气管路，排气管路，一套供油，点火机构，各燃烧室3轮流完成吸气，压缩，供油，点火，爆发做功，排气，再吸气的工作。燃烧气体，在燃烧室3内边转动，边然烧，边爆发做功，容积边增大，边排气，再吸气......。火花塞、喷油嘴，排气口、吸气口安装在斜面体内。只用一套吸气，排气，供油点火机构，发动机八个以上的燃烧室始终一半在吸气，压缩，供油，一半在点火，爆发，做工排气，发动机省去了气缸、气门、设施，活塞，连机，曲轴，配重轮，配重铁等设施，发动机结构紧凑，重量轻，马力大，省铁省油，噪音低，有替代现时应用的柴油机，汽油机的优势。
Description
技术领域：本发动机属内燃烧机，属燃油发动机或燃气发动机，可用汽油、柴油、煤油、天然气、液化气等多种燃料。
技术背景：现实应用的有百年以上历史的汽油机、柴油机，广泛应用在工业，农业，交通，国防中发挥着重要做用，但对比本专利特点是；
由于活塞频繁往复运动，所产生的噪音大，能量消耗大，磨损大。
燃气轮机没有瞬间封闭爆发做功的优点。
发明内容：发明目的是提供一种双斜面体，多滑片，多燃烧室滚动循环发动机。省去了汽油机，柴油机中的气门，活塞，连杆，曲轴，配重轮，配重铁等设施，使发动机在马力不变情况下重量减轻一半。
技术方案：本发明是通过以下技术方案来实现的，斜面体4是一个内空圆柱体，一端固定在机体上，另一端有一个圆滑的斜面，斜面顶着滑片1，滑片顶着弹簧，11，弹簧顶着滑柱12，滑柱顶着圆珠13，滑珠顶着配合斜面体9的斜面。
斜面体4，配合斜面体9的两斜面对称，互补，平行，滑片轮每转一周，两斜面相互推动滑片组做一次与轴向平行的往复运动。保证封闭的燃烧室空间能够有序的变化一次。
斜面体4的最长处凹槽处装有喷油咀，火花塞，斜面体4最短处有排气口，吸气口。
滑片轮5上装有8组以上的滑片组。由滑片轮5，滑片1，斜面体4，形成与滑片1个数相同的燃烧室3。
滑片轮5每转一周，各滑片组，做与轴向平行的往复运动一次，各燃烧室3 的空间变化一次，燃烧室在斜面体4最短处，燃烧室3内空间最大，进行吸气，之后边转动，边进行压缩，转至斜面体最长处，燃烧室空间最小，气体被压缩到最高气压，喷油咀供油，火花塞点火，油气混合体，爆发做功，燃烧室边转动，边做功，容积边自动变大，转到斜面体最短处，有排气口，进行排气，又转到进气口，由于高温的废气排除，吸入新鲜的冷空气，各燃烧室循环不断。
滑片轮每转动一周，滑片组在两斜面的相互推动下，做一次与轴向平行的往复运动，各燃烧室各做一次吸气，压缩，供油，点火，爆发做功，排气的工作。
具体事实方法：结合附图进一步说明：图1为组合示意图，图2为滑片轮5 的左视剖面图，图3为斜面体4的右视剖面图。
工做时由人力或起动机，给一个起始动力，当其中任意一个燃烧室内3，对着吸气口时2，就开始吸入空气，之后边转动边压缩，转动到喷油咀6，火花塞7处点火，油汽混合体爆发做功，燃烧室3边转动容积边增大，转动到排气口8处排出废气，再转到吸气口2处吸入新鲜的冷空气，各燃烧室循环不断。
本发动机结构紧凑，体积小重量轻，省铁、省油、噪音低调速，加速，减速性能好。
当某一燃烧室3在喷油点火位置时空间最小，由配合斜面体9的斜面，推动圆珠使滑片组向燃烧室方向移动，使滑片与斜面体4的斜面良好接触当这一燃烧室转到排气口8，吸气口2处，由斜面体4的斜面推动滑片压缩入滑片轮内，使燃烧室3空间变小以利气体压缩。
本发动机的冷却系统：可在斜面体中加工成中空的冷却水道又可在滑片轮外用铁板封包，封包外用冷却水，封包，用柴机油由滑片轮击溅润滑，调速机构用柴油机油泵中的调速器改装成。
Claims (1)
1.双斜面体，多滑片，多燃烧室，滚动循环，轮流做功发动机。
本发动机由固定的配合斜面体9，斜面体4，与转动的滑片轮构成。斜面体中有火花塞，喷油咀进气口，排气口。滑片轮中装有滑片、弹簧、滑柱、园珠组成的滑片组，斜面体的斜面顶着弹簧，弹簧项着滑柱，滑柱顶着园珠，园珠顶着配合斜面体的斜面，两斜面体的两斜面对称，互补，平行，运转中滑片组在两斜面的相互推动下，每转一周，滑片组往复运动一次，每转一周，各燃烧室，空间变化一次，两斜面对称，互补，平行，保证燃烧室的瞬间封闭。保证燃烧室空间的有序变化。
只用一套吸气，排气管路，一套喷油咀，火花塞，多个燃烧室，一半在吸气，压缩，供油，一半在点火，爆发做功，排气，轮流循环不断。
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| CN202110493349.3A CN113217182A (zh) | 2021-04-27 | 2021-04-27 | 双斜面体，多滑片，多燃烧室，滚动循环，轮流做功发动机 |
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| CN202110493349.3A CN113217182A (zh) | 2021-04-27 | 2021-04-27 | 双斜面体，多滑片，多燃烧室，滚动循环，轮流做功发动机 |
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