TR201705836A2 - INSIDE COMBUSTION ROTATING PISTON ONE-WAY BEARING MOTOR - Google Patents
INSIDE COMBUSTION ROTATING PISTON ONE-WAY BEARING MOTOR Download PDFInfo
- Publication number
- TR201705836A2 TR201705836A2 TR2017/05836A TR201705836A TR201705836A2 TR 201705836 A2 TR201705836 A2 TR 201705836A2 TR 2017/05836 A TR2017/05836 A TR 2017/05836A TR 201705836 A TR201705836 A TR 201705836A TR 201705836 A2 TR201705836 A2 TR 201705836A2
- Authority
- TR
- Turkey
- Prior art keywords
- rotor
- engine
- bearing
- internal combustion
- output shaft
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 48
- 238000004880 explosion Methods 0.000 claims abstract description 26
- 230000033001 locomotion Effects 0.000 claims abstract description 25
- 238000007789 sealing Methods 0.000 claims description 16
- 239000000203 mixture Substances 0.000 claims description 12
- 239000000446 fuel Substances 0.000 claims description 7
- 238000005461 lubrication Methods 0.000 claims description 7
- 230000006835 compression Effects 0.000 claims description 5
- 238000007906 compression Methods 0.000 claims description 5
- 239000007789 gas Substances 0.000 claims description 3
- 230000001050 lubricating effect Effects 0.000 claims description 3
- 238000001816 cooling Methods 0.000 claims description 2
- 238000005474 detonation Methods 0.000 claims 1
- 230000005540 biological transmission Effects 0.000 description 2
- 230000000737 periodic effect Effects 0.000 description 2
- YXIWHUQXZSMYRE-UHFFFAOYSA-N 1,3-benzothiazole-2-thiol Chemical compound C1=CC=C2SC(S)=NC2=C1 YXIWHUQXZSMYRE-UHFFFAOYSA-N 0.000 description 1
- 235000014443 Pyrus communis Nutrition 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 230000002045 lasting effect Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Buluş; temel ve birincil kullanım alanı insansız hava araçları olmakla birlikte, her tür vasıtada, jeneratörlerde, kompresörlerde ve pompalarda kullanılan içten yanmalı patlamalı motor ile ilgilidir. Buluş içten yanmalı patlamalı motor olup; değişken açısal hız ile motor gövde bloğunun (1) dairesel hacminde dönen, ikişer adet kanada sahip, arka kapağa (6) dış bileziğinden yataklanmış olan 1.tek yönlü rulmanın (10) iç bileziğinden yataklanan, çıkış mili (17) üzerindeki yüke göre bağımsız hareket ederek otonom güç ayarlaması yapan 1. rotor (3), değişken açısal hız ile motor gövde bloğunun (1) dairesel hacminde dönen, ikişer adet kanada sahip, ön kapağa (5) dış bileziğinden yataklanmış 2.tek yönlü rulmanın (11) iç bileziğinden yataklanan, çıkış mili (17) üzerindeki yüke göre bağımsız hareket ederek otonom güç ayarlaması yapan 2. rotor (4), 1.rotor (3) ile 2.rotor (4) arasında bulunan, 1.rotor (3) ve 2.rotorun (4) birbiri üzerinde dönmesine ve yataklanmasına olanak sağlayan rulman (9), 1.rotor (3) ile arka kapak (6) arasında bulunan, 1.rotor (3) ve 2.rotorun (4) farklı zamanlarda farklı miktarlarda dönmesine olanak sağlayan 1. tek yönlü rulman (10), 2.rotorun (4) dönme hareketlerini çıkış miline (17) aktaran ve 2.rotorun (4) iç bileziğine yataklandığı 3. tek yönlü rulman (18), 1.rotorun (3) dönme hareketlerini çıkış miline (17) aktaran ve 1.rotorun (3) iç bileziğine yataklandığı 4. tek yönlü rulman (19) içermesi ile karakterize edilmektedir.Meet; Although its primary and primary use is unmanned aerial vehicles, it is related to the internal combustion combustion engine used in all types of vehicles, generators, compressors and pumps. The invention is an internal combustion explosion engine; Independent movement according to the load on the output shaft (17), which is housed from the inner ring of the 1st one-way roller bearing (10), which rotates in the circular volume of the motor body block (1) with variable angular speed, has two blades, and is housed on the outer ring of the rear cover (6). The 1st rotor (3), which performs autonomous power adjustment, has two blades, rotating in the circular volume of the motor body block (1) with variable angular speed, and is housed from the inner ring of the second one-way bearing (11), which is supported by the outer ring of the front cover (5). The 2nd rotor (4), which acts independently according to the load on the output shaft (17) and makes autonomous power adjustment, is located between the 1st rotor (3) and the 2nd rotor (4), the 1st rotor (3) and the 2nd rotor ( 4) The bearing (9), which enables the rotation and bearing on each other, is located between the 1.rotor (3) and the rear cover (6), allowing the 1.rotor (3) and the 2.rotor (4) to rotate in different amounts at different times. . one-way bearing (10) transfers the rotational movements of the 2nd rotor (4) to the output shaft (17) and the 2nd rotor (4) The 3rd one-way bearing (18), which is mounted on the three ring, is characterized by the fact that it contains the 4th one-way bearing (19) that transfers the rotation movements of the 1st rotor (3) to the output shaft (17) and where it is housed in the inner ring of the 1st rotor (3).
Description
TARIFNAME IÇTEN YANMALI DÖNER PISTONLU TEK YÖNLÜ RULMANLI Teknik Alan Bulus; temel ve birincil kullanim alani insansiz hava araçlari olmakla birlikte, her tür vasitada, jeneratörlerde, kompresörlerde ve pompalarda kullanilan içten yanmali patlamali motor ile ilgilidir. DESCRIPTION INTERNAL COMBUSTION ROTATING PISTON ONE WAY BEARING Technical Area Meet; Although the main and primary usage area is unmanned aerial vehicles, every internally used in all types of vehicles, generators, compressors and pumps. relates to the combustion explosion engine.
Bulus daha özel olarak, çift rotorlu döner pistonlu motor sisteminde, iki rotorun tek yönlü rulman ile yataklanmasi ile eksantrikligi saglayan disli çifti sistemini ortadan kaldiran ve millerin es merkezli olarak çalismasina olanak saglayan bir içten yanmali patlamali motor ile ilgilidir. Önceki Teknik Klasik içten patlamali motorlar agir ve verimsiz çalisirlar ve insansiz hava araçlarinda istenen düsük agirlik/yüksek güç, kompakt yapi, düsük yakit tüketimi kriterlerini tam olarak karsilayamazlar. Ancak daha uzun ömürlüdürler. More specifically, the invention is concerned with the dual rotor rotary piston motor system, where the two rotors are Gear pair system that provides eccentricity with one-way bearing a system that eliminates the relates to the internal combustion engine. Prior Art Conventional internal combustion engines are heavy and inefficient, and unmanned aerial vehicles low weight/high power, compact structure, low fuel consumption do not fully meet the criteria. However, they are longer lasting.
Karsilikli piston hareketi ile çalisan motorlarla (klasik motor) hava araçlarinin isterlerini karsilamaya çalisilmistir. Buna örnek olarak Rotax motoru verilebilir. Air vehicles with engines working with reciprocating piston movement (classical engine) tried to meet their demands. An example of this is the Rotax engine.
Daha küçük ve verimli motorlara örnek olarak ise döner motorlar verilebilir. Bu döner motorlar ailesinin ilk örnegi Wankel motorlardir ve bu motorlar üçgen- armudi yapiya sahiptir. Bu motorlarin en büyük sorunu ise vibrasyon olup, yüksek yakit tüketimi ve kisa ömür sakincalari vardir. Buna ragmen halen endüstride basariyla kullanilmaktadir. An example of smaller and more efficient motors is rotary motors. This Wankel motors are the first example of rotary motors family and these motors are triangular- It has a pear shape. The biggest problem of these motors is vibration. There are fuel consumption and short life drawbacks. Despite this, it is still in the industry is used with success.
Bu eksantrik milleri, ayrica pistonlara önceden belirlenmis peryodik bir mekanik hareket biçimi saglar sadece yakit-hava karisimi ve atesleme degisimiyle pistonlarin dönme hizi degisir. Çikis mili üzerindeki yükten etkilenerek gücünü kendiliginden ayarlayan herhangi bir motor yoktur. These camshafts also give the pistons a predetermined periodic mechanical Provides movement only with fuel-air mixture and ignition change the rotational speed of the pistons changes. Its strength is affected by the load on the output shaft. There is no motor that adjusts itself.
Teknikte döner motorlarla ilgili çesitli gelistirmeler yapilmistir. patent dokümaninda, sürtünmesiz döner pistonlu makas hareketli motordan bahsedilmektedir. Bulusta, gövde silindirini iki çift hava odasi içine simetrik olarak ayiran iki döner makas-hareketli piston elemani kullanmaktadir. Iki hava girisi ve hava egzozu iki hava bölmesine stratejik olarak konumlandirilmistir. hareketi kontrol etmek için rotorlara baglanmistir. Bulusta, iki pistonlu rotor yüzeyinin yariklari arasina yerlestirilen bir yatak halkasi vardir. Döner pistonun agirligini desteklemek için rotorun her aksinda bir rulman bulunmaktadir. Gövde ile piston elemanlari arasinda fiziksel temas olmamasi, sürtünmesiz bir tasarima ortaya çikarmaktadir. Bu durum döner piston elemanlarinin türbin kanatlari gibi yüksek hizda dönmesini saglar ve yüksek verimlilik elde edilir. patent dokümaninda döner makas hareketli makinelerden bahsedilmistir. Birinci disli ile tutturulmus olan bir reaksiyon dislisi, birinci disliyi dönen mile göre döndürür. Birinci ve ikinci baglanti çubuklari eksensel birinci disli ile baglanir. Various improvements have been made in the art regarding rotary motors. In the patent document, it is a frictionless rotary piston scissor-action motor. is mentioned. In the invention, the body cylinder is symmetrically enclosed in two pairs of air chambers. It uses two rotating scissor-moving piston elements that separate two weather The inlet and air exhaust are strategically located in the two air chambers. It is connected to the rotors to control the movement. In the invention, a two-piston rotor It has a bearing ring placed between the slots of its surface. rotary piston There is a bearing on each axis of the rotor to support its weight. Body The absence of physical contact between the piston and the piston elements, resulting in a frictionless design. is revealing. In this case, the rotating piston elements are like turbine blades. It provides high speed rotation and high efficiency is obtained. In the patent document, rotary scissors moving machines are mentioned. First A reaction gear, which is attached with a gear, rotates the first gear relative to the rotating shaft. returns. The first and second connecting rods are connected with the axial first gear.
Birinci ve ikinci krank kollari eksensel birinci karsilik gelen ve ikinci baglanti çubuklari ile baglanir. Birinci ve ikinci es eksenli saftlar, birinci ve ikinci birinci krank kollari ile baglanir. Birinci mil, en az bir ön çalisma elemaniyla baglantilidir. ikinci mil, en azindan bir geriye dogru çalisma elemaniyla baglantilidir. Kanat ise saftin hareketi ile dönmektedir. First and second crank arms axially corresponding to the first and second link fastened with rods. First and second coaxial shafts, first and second first connected by crank arms. First shaft, with at least one pre-running element is connected. second shaft, with at least one backward running element is connected. The wing rotates with the movement of the shaft.
Teknigin bilinen durumunda yer alan U86886527 numarali Birlesik Devletler patent dokümaninda, içten yanmali döner motordan bahsedilmektedir. Bulusa göre döner kanat tipi motor, bir çift ön kanatçiklara sahip olan birinci dönen eleman ve ikinci döner eleman içermektedir. Kanatlar silindirik bir odacik içinde döner ve silindirik odacik bir emme girisi ve egzoz deligi içerir. Kanatlar bir tahrik mili tarafindan tahrik edilmektedir Iki tahrik mili bir tahrik treniyle baglidir. United States numbered U86886527 in the state of the art In the patent document, the internal combustion rotary engine is mentioned. find it The rotary vane type engine is the first rotating blade having a pair of front blades. element and a second rotating element. Wings in a cylindrical chamber The rotating and cylindrical chamber contains an intake inlet and an exhaust port. wings one driven by the drive shaft The two drive shafts are connected by a drive train.
Tahrik milleri, kanatlar merkezi dönme ekseni etrafinda döndügünde ve yanma döngüsünün asamalarini tanimlarken, arka kanadin iliskili ön kanala dogru ve ondan uzaktaki göreli hareketini belirler. When the drive shafts rotate about the central axis of rotation of the blades and the combustion when describing the phases of the cycle of the rear wing, toward the associated front wing and determines its relative motion away from it.
Teknigin bilinen durumunda yer alan USZOO3138337 numarali Birlesik Devletler patent dokümaninda içten yanmali motordan bahsedilmektedir. Motor, giris ve egzoz portlarina sahip silindirik bir çalisma odasini tanimlayan bir mahfaza, çalisma odasinda pistonlardan olusan ve çapraz olarak yerlestirilmis birinci ve ikinci birbirine disli pistonlu düzenekler mevcuttur. United States numbered USZOO3138337 in the state of the art The patent document mentions the internal combustion engine. engine, inlet and an enclosure defining a cylindrical work chamber with exhaust ports, The first and diagonally placed first and Second, threaded piston assemblies are available.
Ancak örnek gösterilen dokümanlarda, motorlarin yanma bölümü üzerinde bulunan piston kanatlarinin hareketi, pistonlarin baglandigi eksantrik milinin hareketine baglidir. Çift rotorlu motorlarda, rotorlarin birbiri ile göreceli hareket etmesi sebebiyle kanatlarda olusan zit yönlü kuvvetler dogruca eksantrik kaçikligi olusturan iç ve dis disli çiftine etki eder. Döner pistonlu motorlarda bulunan eksantrik miller, yapisi geregi hareket esnasinda olusacak titresimi dengeleyecek karsi agirlik yerlesimine izin vermez. Bu sebeple titresim saft boyunca aktarilir ve zamanla eksantrikligi saglayan dislinin dis dislisinde yorulma görülür. Bu durum hem yüksek vibrasyon olusturur hem de parça ömrü kisalir. However, in the exemplary documents, on the combustion section of the engines The movement of the piston blades located in the it depends on the movement. In double rotor motors, the relative motion of the rotors with each other due to the opposing forces on the wings, the eccentric It acts on the inner and outer gear pair. found in rotary piston engines eccentric shafts will balance the vibration that will occur during movement due to its structure. does not allow counterweight placement. Therefore vibration is transmitted along the shaft and Over time, fatigue is seen in the tooth gear of the gear that provides eccentricity. This situation It creates both high vibration and shortens the life of the part.
Bu eksantrik milleri ayrica pistonlara belirlenmis hareket biçimi saglar sadece yakit-hava karisimi ve atesleme degisimiylc pistonlarin dönme hizi degisir.Ana mil üzerindeki yüktcn etkilenerek gücünü kendiliginden ayarlayan herhangi bir motor yoktur. These camshafts also provide the pistons with a defined movement pattern. The rotation speed of the pistons changes with the fuel-air mixture and ignition change. any device that automatically adjusts its power by affecting the load on the shaft. there is no engine.
Eksantrikligi saglayan disli çifti sistemini ortadan kaldiran ve millerin es merkezli olarak çalismasina olanak saglayan bir motorun olmamasi, bulus konusu içten yanmali döner pistonlu tek yönlü rulmanli motorun gelistirilmesi ihtiyacini dogurmustur. It eliminates the gear pair system that provides eccentricity and the concentricity of the shafts. The fact that there is no engine that allows it to work as a The need for the development of a combustion rotary piston one-way bearing engine has given birth.
Bulusun Amaçlari ve Kisa Açiklamasi Bu bulusun amaci, iki rotorun tek yönlü rulmanlar ile yataklanmasi ile eksantrikligi saglayan disli çifti sistemini ortadan kaldiran ve millerin es merkezli olarak çalismasina olanak saglayan bir içten yanmali patlamali motorun gerçeklestirilmesidir. Objectives and Brief Description of the Invention The aim of this invention is to use two rotors with one-way bearings. It eliminates the gear pair system providing eccentricity and the concentricity of the shafts. an internal combustion explosion engine that allows it to work as is realization.
Bu bulusun amaci, Vibrasyon, saft ve disli yorulmasi gibi sorunlari, tek yönlü rulmanin sagladigi es merkezli güç iletimi baglantisi ile çözen bir içten yanmali patlamali motorun gerçeklestirilmesidir. The aim of this invention is to solve problems such as vibration, shaft and gear fatigue, one-way It is an internal combustion engine that solves the concentric power transmission connection provided by the bearing. realization of the explosion engine.
Bu bulusun bir baska amaci, motorun mili üzerindeki yüke oranla gücü otonom olarak ayarlayan ve güç artisi saglayan bir içten yanmali patlamali motorun gerçeklestirilmesi, bu sekilde mekanik güç aktarma organlarinin basitlestirilmesi ve hafifletilmesidir. Another object of this invention is to make the power autonomous in proportion to the load on the shaft of the motor. of an internal combustion explosion engine that adjusts the realization, thereby simplifying mechanical power transmission and alleviation.
Bu Bulusun bir baska amaci Çikis mili üzerindeki yüke göre hava-yakit karisimini sikistirmasi degisen pistonlarin, çikis mili üzerinde herhangi bir nedenle (veya ariza sonucu) yükün çok fazla artmasi nedeniyle pistonlarin birbirine yapismasini engelleyecek sekilde asimetrik yapida (bir tarafi düz, diger tarafi konveks veya konkav) yapilarak motorda olusabilecek kalici hasarlari önlemesidir. Another object of this Invention is the air-fuel mixture according to the load on the output shaft. pistons whose compression has changed, on the output shaft for any reason (or the pistons sticking to each other due to excessive load. asymmetrical structure (one side is flat, the other side is convex or concave) to prevent permanent damages that may occur in the engine.
Bu bulusun bir baska amaci, basit yapida, hafif aiicak yüksek güç saglayan bir içten yanmali patlamali motorun gerçeklestirilmesidir. Another object of the present invention is a simple construction, light-weight high-power realization of the internal combustion explosion engine.
Bulusta, Vane motoru türü motorlarda bulunan eksantrik inilin hareketini ileten ve döner piston zamanlamasini saglayan mafsallar yerine tek yönlü rulmanlar kullanilmistir. Tek yönlü rulmanlar ile rotorlar motor gövdesine yataklanmistir. In the invention, the eccentric shaft in Vane engine type engines transmits the movement and one-way bearings instead of joints that provide rotary piston timing used. Rotors are mounted on the motor body with one-way bearings.
Kanatlarin olusturdugu degisken hacme sahip odalarda yanma gerçeklestigi anda kanatlardan sadece biri çikis milinin dönme yönünde digeri ise tersi yönde dönmek isteyecektir. Tek yönlü rulmanlar sadece çikis milinin dönme yönündeki harekete izin vermektedir. Bu sebeple bir rotor sabit dururken diger rotor çikis milini döndürecek yönde hareket eder. Iki rotor farkli motor zamanlarinda durur, çikis miline zit dönme yönünde döner veya iki rotorda birlikte döner. Rotorlarin bu sekilde dönmesi, dört zamanli motorlardaki emme, sikistirma, yaiima ve egzoz zamanlarina denk gelen krank mili zamanlamalarinin benzerini gerçeklestiren, periyodik olarak döner pistonlari (rotorlari) döndüren bir yapi olusturur. Çikis milinde bulunan iki veya daha fazla tek yönlü rulman rotorlar ile yataklanmistir. As soon as combustion takes place in the rooms with variable volume formed by the wings Only one of the blades is in the direction of rotation of the output shaft and the other in the opposite direction. will want to return. One-way bearings are only in the direction of rotation of the output shaft. allows movement. For this reason, while one rotor is stationary, the other rotor exits. moves in the direction to rotate the shaft. The two rotors stop at different engine times, rotates in the opposite direction of rotation to the output shaft, or the two rotors rotate together. your rotors This way it rotates, the intake, compression, combustion and exhaust systems in four-stroke engines. simulating the crankshaft timings corresponding to the timings, it creates a structure that periodically rotates the rotating pistons (rotors). Exit Two or more one-way bearings on the shaft are supported by rotors.
Bu rulmanlar iki rotoru birbirine yataklayan tek yönlü rulmanlar ile zit yönde dönmeye izin verecek sekilde yataklanmistir. Bu sayede rotorlar dönünce çikis mili ve hareketli rotor kilitlenir ve güç aktarilir. These bearings are in opposite directions with one-way bearings that hold the two rotors together. It is bedded to allow rotation. In this way, when the rotors turn, the output shaft and movable rotor are locked and power is transmitted.
Bulusun Ayrintili Açiklamasi Bu bulusun amacina ulasmak için gerçeklestirilen içten yanmali patlamali motor ekli sekillerde gösterilmistir. Detailed Description of the Invention To achieve the aim of this invention, the internal combustion explosion engine shown in the attached figures.
Bu sekiller; Sekil 1: Bulus konusu içten yanmali patlamali motorun kesit görünümüdür. These figures are; Figure 1: The subject of the invention is the cross-sectional view of the internal combustion explosion engine.
Sekil 2: Bulus konusu içten yanmali patlamali motorda, rotor kanatlarinin sikistirilmis olan yakit-hava karisiminin yanma evresindeki konumunun görünümüdür. Figure 2: In the internal combustion explosion engine, the subject of the invention, the rotor blades position of the compressed fuel-air mixture in the combustion phase. is the view.
Sekil 3: Bulus konusu içten yanmali patlamali motorda, rotorlarin birlikte saat yönünde döndügü fazin görünümüdür. Figure 3: In the internal combustion explosion engine, the subject of the invention, the rotors are clocked together. It is the view of the phase in which it rotates in the direction of.
Sekil 4: Rotorlarin bir tarafi düz diger tarafi konkav olan rotorlarin temas yüzeyini minimuma indiren yapisinin rotorlarin ayrik konumlarinin görünümüdür. Figure 4: The contact of the rotors with one side flat and the other side concave It is the view of the separate positions of the rotors of the structure that minimizes the surface.
Sekil 5: Rotorlarin bir tarafi düz diger tarafi konkav olan rotorlarin temas yüzeyini minimuma indiren yapisinin rotorlarin patlama öncesi konumlarinin görünümüdür. Figure 5: The contact of the rotors with one side flat and the other side concave The pre-explosion position of the rotors of the structure that minimizes the surface is the view.
Sekil 6: Bulus konusu içten yanmali patlamali motorda yer alan, her rotor üzerinde dört adet bulunan yag ve basinç segmanlarinin görünümüdür. Figure 6: Each rotor in the internal combustion explosion engine, which is the subject of the invention It is the appearance of the four oil and pressure rings on it.
Sekil 7: Bulus konusu içten yanmali patlamali motorda yer alan basinç segmaninin perspektif görünümüdür. Figure 7: Pressure in the internal combustion explosion engine of the invention is the perspective view of the segment.
Sekil 8: Bulus konusu içten yanmali patlamali motorda yer alan rotor ve rotor yapisinin görünümüdür. Figure 8: Rotor and rotor in the internal combustion explosion engine which is the subject of the invention is the view of the structure.
Sekil 9: Bulus konusu içten yanmali patlamali motorda yer alan yaglama sübap bilyasinin rotor içindeki konumunun görünümüdür. Figure 9: The lubrication valve in the internal combustion explosion engine, which is the subject of the invention is the view of the position of the ball in the rotor.
Sekil 10: Yaglama subap bilyasinin rotorlar ve motor blogu arasinda yaglama islemi devam ederken bulundugu konumun görünümüdür. Figure 10: Lubrication valve ball between rotors and engine block It is the view of the location where the process is in progress.
Sekillerde yer alan parçalar tek tek numaralandirilmis olup, bu numaralarin karsiliklari asagida verilmistir. The parts in the figures are numbered one by one. the responses are given below.
Motor gövde blogu 2. Rotor Rulman ön kapagi Rulman arka kapagi Rulman . 1. Tek yönlü rulman . 2. Tek yönlü rulman . Tahliye borusu . l. Sizdirmazlik elemani . 2. Sizdirmazlik elemani 16. 3. Sizdirmazlik elemani 17. Çikis mili 18. 3. Tek yönü rulman 4. Tek yönlü rulman Basinç segmani Yag segmani Yaglama sübap bilyasi Yag tahliye deligi Rotor yapisi Bulus, içten yanmali patlamali motor olup; motorun yanma, sikistirma, emme ve egzoz zamanlarinin olustugu degisken hacimlerin bulundugu dairesel bir bos hacme sahip, disinda ön kapak (5) ve arka kapak (6) parçalarinin civatalar ile baglandigi ara yüze sahip bir motor gövde blogu (1), yakit-hava karisiminin yanmasini saglayan, motor gövde blogu (1) üzerine baglanan bir buji (2), degisken açisal hiz ile motor gövde blogunun (l) dairesel hacminde dönen, ikiser adet kanada sahip, arka kapaga (6) dis bileziginden yataklanmis olan 1. tek yönlü rulmanin (10) iç bileziginden yataklanan 1. rotor (3), degisken açisal hiz ile motor gövde blogunun (1) dairesel hacminde dönen, ikiser adet kanada sahip, ön kapaga (5) dis bileziginden yataklanmis, 1.rotor (3) ve 2.rotorun (4) farkli zamanlarda farkli miktarlarda dönmesine olanak saglayan 2. tek yönlü rulmanin (11) iç bileziginden yataklanan 2. l.rotor (3) ile 2.rotor (4) arasinda bulunan, l.rotor (3) ve 2.rotorun (4) yataklanmasini saglayan ve dönmesine olanak saglayan rulman (9), 1.rotor (3) ile arka kapak (6) arasinda bulunan, 1.rotor (3) ve 2.rotorun (4) farkli zamanlarda farkli miktarlarda dönmesine olanak saglayan 1. tek yönlü rulman (10), 2.rotor (4) ile ön kapak (5) arasinda bulunan, 1.rotor (3) ve 2.rotorun (4) farkli zamanlarda farkli miktarlarda dönmesine olanak saglayan 2. tek yönlü rulman (11), egzoz gazlarini tahliye eden ve motor gövde blogu (1) üzerine baglanan bir egzoz tahliye borusu (12), yakit-hava karisimini yanma odalarina besleyen bir yakit hava karisimi farkli açisal hizlarda ve farkli periyotlarda dönen l.rotor (3) ve 2.rotor (4) hareketlerinin tek mil üzerinde toplayan çikis mili (17), 2.rotorun (4) dönme hareketlerini çikis miline (17) aktaran ve 2.rotorun (4) iç bilezigine yataklandigi 3. tek yönlü rulman (18), l.rotorun (3) dönme hareketlerini çikis miline (17) aktaran ve l.rotorun (3) iç bilezigine yataklandigi 4. tek yönlü rulman (19), l.rotor (3) ve 2.rotorun (4) üzerinde bulunan, isi ile genlesen, yaglamayi saglayan en az bir adet U seklindeki basinç segmanlari (20) ve yag segmanlari (21), motorun çalisma esnasinda yaglamayi saglayan yaglama sübap bilyasi (22), motor gövde blogunu (l) sogutmasi ve yaglamasi için kullandigi müsterek yagi motor gövde blogunun (l) gömleginin yani sira l.rotor (3) ve 2.rotor (4) içinde de dolastirmasi ve l.rotor (3) ve 2.rotorlarin (4) dönüs hiziyla orantili yeterli miktardaki yag ile motor yaglamasi yapan yag tahliye deligi (23), çikis mili (17) üzerindeki yükün çok fazla olmasi durumunda l.rotor (3) ve 2.rotorun (4) birbiriyle yapismasini engelleyen asimetrik olan, bir tarafi düz, diger tarafi konkav veya konveks rotor yapisi (24), içermektedir. engine body block 2. Rotor Bearing front cover Bearing back cover Roller . 1. One way bearing . 2. One-way bearing . drain pipe . l. sealing element . 2. Sealing element 16. 3. Sealing element 17. Output shaft 18. 3. One-way bearing 4. One-way bearing pressure ring oil ring lubrication valve ball oil drain hole rotor structure The invention is an internal combustion explosion engine; combustion, compression, intake and exhaust times of the engine It has a circular empty volume with variable volumes, with the exception of the front to the interface where the cover (5) and the rear cover (6) parts are connected with bolts. an engine body block (1), on the engine body block (1), which allows the fuel-air mixture to burn. a connected spark plug (2), rotating in the circular volume of the engine body block (l) with variable angular velocity, having two wings each, mounted on the back cover (6) from the outer ring The 1st rotor (3), which is supported by the inner ring of the 1st one-way bearing (10), rotating in the circular volume of the engine body block (1) with variable angular velocity, it has two wings, the front cover (5) is supported by the outer ring, 1st rotor (3) and 2nd rotor (4) rotate at different times at different amounts. 2 bearing from the inner ring of the 2nd one-way bearing (11) that allows Between the 1st rotor (3) and the 2nd rotor (4), the 1st rotor (3) and the 2nd rotor (4) bearing (9), which provides the bedding and allows it to rotate, 1st rotor (3) and 2nd rotor (4) located between the 1st rotor (3) and the rear cover (6) 1. single that allows it to rotate in different amounts at different times directional bearing (10), 1st rotor (3) and 2nd rotor (4) located between the 2nd rotor (4) and the front cover (5) 2nd single one that allows it to rotate in different amounts at different times directional bearing (11), a system that evacuates the exhaust gases and is connected to the engine body block (1). exhaust discharge pipe (12), a fuel-air mixture that feeds the fuel-air mixture into the combustion chambers 1st rotor (3) and 2nd rotor (4) rotating at different angular speeds and different periods the output shaft (17), which collects the movements on a single shaft, Transferring the rotational movements of the 2nd rotor (4) to the output shaft (17) and (4) the 3rd one-way bearing (18), in which it is mounted in the inner ring, Transferring the rotational movements of the l.rotor (3) to the output shaft (17) and of the l.rotor (3) 4th one-way bearing (19), which is mounted on the inner ring The lubrication, which expands with the heat, is located on the 1st rotor (3) and the 2nd rotor (4). at least one U-shaped pressure ring (20) and oil segments (21) lubricating valve ball that provides lubrication during engine operation (22) common engine used for cooling and lubrication of the engine body block (l). oil of the engine body block (l), as well as the liner of the l.rotor (3) and the 2nd rotor (4) and the rotation speed of the 1st rotor (3) and 2nd rotors (4). Oil drain hole that lubricates the engine with a proportionally sufficient amount of oil (23) In case the load on the output shaft (17) is too high, the rotor (3) and Asymmetric one side, which prevents the 2nd rotor (4) from sticking to each other flat, concave on the other side or convex rotor structure (24), contains.
Bulus bir içten yanmali patlamali motor olup; ön kapak (5) ve arka kapak (6) arasinda disaridan ve içeriden sizdirmazligi saglamak kullanilan 1.sizdirmazlik elemani (13) içermektedir. The invention is an internal combustion explosion engine; front cover (5) and back cover (6) 1. sealing used to provide sealing from outside and inside between includes element (13).
Bulus bir içten yanmali patlamali motor olup; l.rotor (3) ile 2.rotor (4) arasinda sürtünmeyi azaltmak ve disaridan ya da içeriden yabanci madde, yakit girisini veya çikisini engellemek amaci ile kullanilan 2. sizdirmazlik elemani (14) içermektedir. The invention is an internal combustion explosion engine; Between 1st rotor (3) and 2nd rotor (4) to reduce friction and prevent foreign matter, fuel intake from the outside or inside. or the 2nd sealing element (14) used to prevent its exit. contains.
Bulus bir içten yanmali patlamali motor olup; l.rotor (3) ve 2.rotorun (4) kanatlari üzerinde bulunan, düsük sürtünme katsayisi ile sizdirmazligi saglayan 3. sizdirmazlik elemani (16) içermektedir. The invention is an internal combustion explosion engine; The blades of the 1st rotor (3) and the 2nd rotor (4) 3, which provides sealing with its low coefficient of friction. contains a sealing element (16).
Motor gövde blogu (1) motorun yanma, sikistirma, emme ve egzoz zamanlarinin olustugu degisken hacimlerin bulundugu dairesel bir bos hacme sahip, disinda ön kapak (5) ve arka kapak (6) parçalarinin civatalar ile baglandigi ara yüze sahip parçadir. Buji (2), yakit hava borusu (15) ve tahliye borusu (12) motor gövde blogu (l) üzerine baglanmistir. l. rotor (3) ve 2. rotor (4) motor gövde blogunun (l) dairesel hacminde bulunmaktadir. 1. rotor (3) ve 2. rotorun (4) kanatlari ile ön kapak (5) arka kapak (6) arasinda sizdirmazlik döner pistonlu motorlarda yaygin olarak kullanilan 1. sizdirmazlik elemani (13) ve 2. sizdirrnazlik elemani (14) ile saglanmistir. l. rotor (3) arka kapaga (6) dis bileziginden yataklanmis olan 1. tek yönlü rulmanin (10) iç bileziginden yataklanmistir. 2. rotor (4) ise ön kapaga (5) dis bileziginden yataklanmis 2. tek yönlü rulinanin (11) iç bileziginden yataklanmistir. 1.tek yönlü rulman (10) ve 2.tek yönlü rulman (1 l), 1. rotor (3) ve 2. rotorun (4) es merkezli olmasini saglamaktadirlar. The engine body block (1) is used to measure the combustion, compression, intake and exhaust times of the engine. It has a circular empty volume in which variable volumes are formed, except for the front It has an interface where the cover (5) and the rear cover (6) parts are connected with bolts. is a piece. Spark plug (2), fuel air pipe (15) and discharge pipe (12) engine body The blog is linked on (l). l. rotor (3) and 2nd rotor (4) in the circular volume of the motor body block (l) are available. Front cover (5) with blades of 1st rotor (3) and 2nd rotor (4) rear cover (6) widely used in sealing rotary piston motors 1. It is provided with sealing element (13) and 2nd sealing element (14). l. 1st unidirectional rotor (3), which is mounted on the rear cover (6) from the outer ring. It is supported from the inner ring of the bearing (10). The 2nd rotor (4) is connected to the front cover (5). from the inner ring of the 2nd one-way roller bearing (11) is bedded. 1st one-way bearing (10) and 2nd one-way bearing (1 l), 1st rotor (3) and They ensure that the 2nd rotor (4) is concentric.
Rulman ön kapagi (7) 1.tek yönlü rulmanin (10), rulman arka kapagi (8) ise 2.tek yönlü rulmanin (1 l) dis bileziklerine basarak 1.tek yönlü rulmanin (10) ve 2.tek yönlü rulmanin (ll) eksenel olarak hareket etmesini engellerler. Rulman ön kapagi (7) ve rulman arka kapagi (8) , ön kapak (5) ve arka kapaga (6) hassas toleransa sahip çapta bir çikinti ile merkezlenmistir. l. rotor (3) ve 2. rotor (4) yataklanmasini saglayan 1. tek yönlü rulman (10) ve 2. tek yönlü rulman (11) , 1. rotor (3) ve 2. rotorun (4) dönüs yönünü ve sirasini belirler. 1. tek yönlü rulmanin (10) ve 2. tek yönlü rulmanin (11) belirlenmis mil dönüs hizinin üstünde dönmemesi, mekanik olarak bozulmamasi için oldukça önemlidir. 2. rotorun (4) dönme hareketlerini çikis miline (17) aktaran ve 2. rotorun (4) iç bilezigine yataklandigi 3. tek yönlü rulman (18) ve 1.r0t0run (3) dönme hareketlerini çikis miline (17) aktaran ve 1.r0t0run (3) iç bilezigine yataklandigi 4. tek yönlü rulman (19) bulunmaktadir. 2. rotor (4) saat yönünde döndügünde, 2. rotora (4) yataklanmis olan 3. tek yönlü rulman (18) kitlenir ve çikis milini (17) saat yönünde döndürür. 1. rotor (3) ise 4. tek yönlü rulmanin (19) iç bilezigi ile sabit haldeyken 4. tek yönlü rulmanin (19) dis bilezigi çikis mili (17) ile birlikte saat yönünde döner. Bu sayede periyodik hareketlerle dönen l. rotor (3) ve 2. rotorun (4) hareketi, çikis milinde (17) sürekli bir harekete dönüsmüs olmaktadir. Bearing front cover (7) of the 1st one-way bearing (10), bearing rear cover (8) of the 2nd single Press the disc rings of the 1 directional bearing (1 l) and the 1st one-way bearing (10) and the 2nd one They prevent the directional bearing (II) from moving axially. bearing front sensitive to the cover (7) and the bearing rear cover (8), the front cover (5) and the rear cover (6) It is centered with a protrusion of diameter with tolerance. l. 1. one-way bearing (10) and 2. one-way bearing (11), the direction and order of rotation of the 1st rotor (3) and the 2nd rotor (4). determines. Designated shaft of 1st one-way bearing (10) and 2nd one-way bearing (11) It is very important not to rotate above the rotation speed and not to break down mechanically. is important. It transfers the rotational movements of the 2nd rotor (4) to the output shaft (17) and the inner part of the 2nd rotor (4). 3. one-way bearing (18) and 1.r0t0run (3) rotation 4, which transfers its movements to the output shaft (17) and is mounted on the inner ring of the 1.r0t0run (3). There is a one-way bearing (19). When the 2nd rotor (4) rotates clockwise, 2. The 3rd one-way bearing (18) mounted on the rotor (4) is locked and the output shaft (17) rotates clockwise. The 1st rotor (3) is connected to the inner ring of the 4th one-way bearing (19). when stationary, the outer ring of the 4th one-way bearing (19) together with the output shaft (17) rotates clockwise. In this way, rotating with periodic movements l. rotor (3) and 2. the movement of the rotor (4) turns into a continuous movement on the output shaft (17).
Yani çikis milinde bulunan 3. tek yönlü rulman (18) ve 4. tek yönlü rulman (19), l. rotor (3) ve 2. rotor (4) ile yataklanmistir. 3. tek yönlü rulman (18) ve 4. tek yönlü rulman (19) 1. rotor (3) ve 2. rotoru (4) yataklayan 1. tek yönlü rulman (10) ve 2. tek yönlü rulman (11) ile zit yönde dönmeye izin verecek sekilde yataklanmistir. Yani, 1. rotor (3) ve 2. rotoru (4) yataklayan 1. tek yönlü rulman (10) ve 2. tek yönlü rulman (11) 1. rotor (3) ve 2. rotor (4) ile ayni yönlü dönmeye izin verirken, çikis mili (17) ile l.rotor (3) ve 2. rotoru (4) yataklayan 3. tek yönlü rulman (18) ve 4. tek yönlü rulman (19) ise 1.rotor (3) ve 2. rotorun (4) dönme yönüne zit yönlü dönmeye izin verir. Bu sayede 1. rotor (3) ve 2. rotor (4) dönünce çikis mili (17) ve hareketli olan rotor kilitlenir ve güç aktarilir. 1. rotor (3) ve 2. rotor (4) kanatlarinin sikistirilmis olan yakit-hava karisiminin yanma evresindeki konumunda (Sekil 2); motor gövde blogunda (1) ikiser adet simetrik hacim olusmustur. Bujinin (2) bulundugu hacimdeki sikismis olan yakit- hava karisimi yaninca ortaya çikan patlama kuvveti ile sag tarafta bulunan kanatin bulundugu 2. rotor (4) saat yönünde döner. Diger 1. rotor (3) ise sabit kalir. That is, the 3rd one-way bearing (18) and the 4th one-way bearing (19) on the output shaft, l. rotor (3) and second rotor (4). 3rd one-way bearing (18) and 4th one-way bearing one-way bearing (19) 1st one-way bearing (10) which supports the 1st rotor (3) and the 2nd rotor (4) and the 2nd one-way bearing (11) to allow rotation in the opposite direction. is bedded. That is, the 1st one-way roller bearing the 1st rotor (3) and the 2nd rotor (4) (10) and 2nd one-way bearing (11) in the same direction as 1st rotor (3) and 2nd rotor (4) while allowing the rotation, the output shaft (17) and the 3rd rotor (3) and the 2nd rotor (4) bearing. the one-way bearing (18) and the 4th one-way bearing (19) the 1st rotor (3) and the 2nd rotor (4). It allows rotation in the opposite direction to the direction of rotation. In this way, the 1st rotor (3) and the 2nd rotor (4) When it turns, the output shaft (17) and the movable rotor are locked and power is transmitted. The compressed fuel-air mixture of the 1st rotor (3) and 2nd rotor (4) blades in its position in the combustion phase (Figure 2); two each in the engine body block (1) symmetrical volume is formed. The compressed fuel in the volume where the spark plug (2) is located. With the explosion force that occurs when the air mixture burns, the wing on the right The 2nd rotor (4), in which it is located, rotates clockwise. The other 1st rotor (3) remains fixed.
Hareketli olan 2. rotor (4) degisken açisal hizli hareketini tamamlarken diger hacimde bulunan egzoz gazlarinin tahliye borusunda (12) atilmasini saglayacak sekilde bu hacmi sikistirir. Bu hacmin simetrik tarafinda ise yakit-hava karisimi While the 2nd movable rotor (4) completes its variable angular speed, the other It will ensure that the exhaust gases in the volume are discharged in the discharge pipe (12). This way it compresses the volume. On the symmetrical side of this volume, the fuel-air mixture
Claims (4)
Priority Applications (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TR2017/05836A TR201705836A2 (en) | 2017-04-20 | 2017-04-20 | INSIDE COMBUSTION ROTATING PISTON ONE-WAY BEARING MOTOR |
| PCT/TR2018/050177 WO2019027400A2 (en) | 2017-04-20 | 2018-04-19 | Internal combustion engine with a rotating piston and uni-directional rolling bear |
| US16/469,154 US10890110B2 (en) | 2017-04-20 | 2018-04-19 | Internal combustion engine with a rotating piston and uni-directional rolling bear |
| EP18840517.9A EP3510248A4 (en) | 2017-04-20 | 2018-04-19 | Internal combustion engine with a rotating piston and uni-directional rolling bear |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| TR2017/05836A TR201705836A2 (en) | 2017-04-20 | 2017-04-20 | INSIDE COMBUSTION ROTATING PISTON ONE-WAY BEARING MOTOR |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| TR201705836A2 true TR201705836A2 (en) | 2017-09-21 |
Family
ID=67902050
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| TR2017/05836A TR201705836A2 (en) | 2017-04-20 | 2017-04-20 | INSIDE COMBUSTION ROTATING PISTON ONE-WAY BEARING MOTOR |
Country Status (1)
| Country | Link |
|---|---|
| TR (1) | TR201705836A2 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11535375B2 (en) | 2017-07-06 | 2022-12-27 | Istanbul Teknik Universitesi | Autonomous unmanned aerial vehicle |
-
2017
- 2017-04-20 TR TR2017/05836A patent/TR201705836A2/en unknown
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US11535375B2 (en) | 2017-07-06 | 2022-12-27 | Istanbul Teknik Universitesi | Autonomous unmanned aerial vehicle |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| RU2439333C1 (en) | Rotary piston machine of volumetric expansion | |
| EP2066889B1 (en) | Improved opposed piston combustion engine | |
| KR20170080606A (en) | Power unit | |
| US20070062469A1 (en) | Rotary radial internal combustion piston engine | |
| US9103333B2 (en) | Axial piston machines | |
| TR201705836A2 (en) | INSIDE COMBUSTION ROTATING PISTON ONE-WAY BEARING MOTOR | |
| US10890110B2 (en) | Internal combustion engine with a rotating piston and uni-directional rolling bear | |
| JP4521785B1 (en) | Rotating piston machine | |
| US8230836B2 (en) | Multi-cylinder reciprocating rotary engine | |
| JP2010523885A (en) | Rotary engine | |
| US4799870A (en) | Fluid power transfer device | |
| RU2496998C2 (en) | Rotary-vane ice | |
| PL180814B1 (en) | Work performing machine in particular a cat-and-mouse engine | |
| WO2015159083A1 (en) | Opposed piston machine with rectilinear drive mechanisms | |
| CN109630203A (en) | A kind of 8-cylinder hot-air engine opposed type transmission system and its crankshaft | |
| RU2565940C1 (en) | Rotary-vane internal combustion engine | |
| RU2013597C1 (en) | Power plant | |
| JPH10196396A (en) | Variable stroke device for miller cycle engine | |
| RU2080453C1 (en) | Internal combustion engine | |
| RU2374454C2 (en) | Design of piston machine and method of designing its working chamber for thermodynamic cycle | |
| RU2664725C1 (en) | Rotary piston engine | |
| RU2397326C1 (en) | Rotary machine | |
| US8684714B2 (en) | Internal orbital engine | |
| WO2012166080A1 (en) | Multy-cylinder reciprocating rotary engine | |
| KR101285095B1 (en) | Rotary Engine |