TR201603532A2 - LOW WEIGHT CENTERED WING STRUCTURE - Google Patents
LOW WEIGHT CENTERED WING STRUCTURE Download PDFInfo
- Publication number
- TR201603532A2 TR201603532A2 TR2016/03532A TR201603532A TR201603532A2 TR 201603532 A2 TR201603532 A2 TR 201603532A2 TR 2016/03532 A TR2016/03532 A TR 2016/03532A TR 201603532 A TR201603532 A TR 201603532A TR 201603532 A2 TR201603532 A2 TR 201603532A2
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- Turkey
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- wing
- vehicle
- chassis
- directly
- elements
- Prior art date
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- 230000005484 gravity Effects 0.000 claims abstract description 10
- 230000001105 regulatory effect Effects 0.000 claims abstract description 6
- 238000003466 welding Methods 0.000 claims description 2
- 230000000694 effects Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 2
- 230000001133 acceleration Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B62—LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
- B62D—MOTOR VEHICLES; TRAILERS
- B62D35/00—Vehicle bodies characterised by streamlining
- B62D35/007—Rear spoilers
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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
- Y02T10/80—Technologies aiming to reduce greenhouse gasses emissions common to all road transportation technologies
- Y02T10/82—Elements for improving aerodynamics
Abstract
Araçlarda (20) istenilmeyen hava akışını düzenleyerek yol tutuşunu artıran kanat (11) unsuru haiz düşük ağırlık merkezli kanat yapılanması (10) olup, özelliği; bahsedilen kanadın (11) araç (20) üzerinde diğer unsurlara temas etmeden doğrudan şasesine (23) bağlantısını sağlayan en az bir bağlantı elemanı (12) içermesidir. Böylece kanat yapılanması (10) aracın (20) diğer unsurları ile temas etmeden doğrudan şaseye (23) bağlantısı sağlanmakta ve hem kendi ağırlığını hem de hızdan oluşan ters kuvveti doğrudan şaseye (23) aktararak ağırlık merkezini zemine yaklaştırması mümkün kılınmaktadır.Low weight centered wing configuration (10) having wing element (11) which improves road holding by regulating unwanted air flow in vehicles (20). said vane (11) comprises at least one connecting element (12) which directly connects to the chassis (23) without contacting the other elements on the vehicle (20). Thus, the wing configuration 10 is directly connected to the frame 23 without contacting the other elements of the vehicle 20, and it is made possible to bring the center of gravity closer to the ground by transferring both its own weight and the inverse force of speed directly to the frame 23.
Description
Tarifname Düsük Agirlik Merkezli Kanat Yapilanmasi Teknik Alan Bulus, araçlarda hava akisini düzenleyen ve kontrol eden bir kanat yapilanmasi ile ilgilidir. specification Low Weight Center Wing Configuration Technical Area The invention relates to a wing configuration that regulates and controls air flow in vehicles.
Bulus özellikle, aracin diger unsurlari ile temas etmeden dogrudan saseye baglanan ve bu sekilde hem kendi agirligini hem de hizdan olusan ters kuvveti dogrudan saseye aktararak agirlik merkezini zemine yaklastiran kanatlar ile ilgilidir. In particular, the invention is connected directly to the chassis without coming into contact with the other elements of the vehicle and in this way. weight by transferring both its own weight and the reverse force consisting of speed directly to the chassis. It is related to the wings that bring the center closer to the ground.
Teknigin Bilinen Durumu Araçlarda istenmeyen hava akimlarini düzenlemek adina kanatlar gelistirilmistir. Genel olarak kanat formunda olusturulan kanatlar, hava akimini düzenleyerek aerodinamigi iyilestirmesinin yani sira çogu durumda ters uçak kanadi etkisi olusturarak hizlanma aninda asagi dogru kuvvet uygulayarak yol tutusunu da artirmaktadirlar. Daha çok yüksek performansli ve spor araçlarda tercih edilen kanatlar günümüzde siradan binek araçlarda da kullanim alani bulabilmektedir. State of the Art Wings have been developed in order to regulate unwanted air flows in vehicles. Generally The wings, which are formed in the form of wings, improve the aerodynamics by regulating the air flow, that is, the in most cases, the downward force at the moment of acceleration creating a reverse airplane wing effect They also increase road holding by applying it. More on high performance and sports vehicles The wings, which are preferred today, can also find use in ordinary passenger cars.
Kanatlar, farkli uygulama alanlari bulunmakla birlikte çogunlukla araç arka kisminin üst tarafina ya da arka çamurluklara gelecek sekilde monte edilmektedirler. CN103342137 numarali ve 'Hava akimini ayarlayan türde araba kuyruk kanadi baslikli Çinli patent dokümaninda araç arka bagaj kapagi üzerine sabitlenen türde bir kanadi ortaya koymaktadir. Bu tür yapilanmalarda kanadin kendi agirliginin yani sira artan hiz ile dogru orantili sekilde asagi yönde olusan baski kuvvetin araca olan etkisi üst kisimdan oldugu için agirlik merkezi yukari çekilmektedir. Aerodinamik olarak artan yere bastirma agirligi aracin hizli viraj kabiliyetini arttirsa da bastirma agirligini üstten uyguladigi için agirlik merkezini ister istemez yerden uzaklastirarak kazanilan bu kabiliyet savrulma seklinde kaybedilmektedir. Bu sebeple bu tür araçlarin genel olarak alçak tasarlanmasi yönünde çözüme kavusturulmaktadir. Mevcut yapilanmalarda kanadin agirligi ile rüzgar basinci ile olusan kuvvetin dogruda saseye aktarilabilecegi bir sistem bulunmamaktadir. Wings, although they have different application areas, are mostly placed on the upper part of the rear of the vehicle. They are also mounted to the rear fenders. CN103342137 and 'Air The type of car tail wing that adjusts the current in the Chinese patent document, the vehicle rear trunk it reveals a wing of the type that is fixed on its cover. In such configurations, the wing In addition to its own weight, the pressure force that occurs in the downward direction in direct proportion to the increasing speed Since the effect on the vehicle is from the upper part, the center of gravity is pulled up. aerodynamically Although the increased downforce increases the vehicle's fast cornering ability, lower the downforce from the top. This ability, which is gained by moving the center of gravity away from the ground involuntarily because it applies is lost in the form of throwing. For this reason, such vehicles are generally designed low. is being resolved accordingly. In current configurations, the weight of the wing and the wind pressure There is no system in which the resulting force can be transferred directly to the chassis.
Sonuç olarak, aracin diger unsurlari ile temas etmeden dogrudan saseye baglanan ve bu sekilde hem kendi agirligini hem de hizdan olusan ters kuvveti dogrudan saseye aktararak agirlik merkezini zemine yaklastiran kanatlara olan gereksinimin varligi ve mevcut çözümlerin yetersizligi ilgili teknik alanda bir gelistirme yapmayi zorunlu kilmistir. As a result, it is connected directly to the chassis without contacting the other elements of the vehicle and is thus weight by transferring both its own weight and the reverse force consisting of speed directly to the chassis. the existence of the need for wings that bring the center closer to the ground and the inadequacy of the existing solutions has made it necessary to make a development in the relevant technical field.
Bulusun Amaci Mevcut bulus, yukarida bahsedilen gereksinimleri karsilayan, tüm dezavantajlari ortadan kaldiran ve ilave bazi avantajlar getiren kanatlar ile ilgilidir. Purpose of the Invention The present invention is one that meets the above-mentioned requirements, eliminates all the disadvantages. and wings that bring some additional advantages.
Bulusa konu olan kanadin ana amaci; kanadin aracin diger hiçbir unsuruna temas etmeden baglanti elemanlari araciligi ile dogrudan sasesine baglanmasi ile hem kendi agirliginin hem de rüzgâr basincindan dogan kuvvetin dogrudan saseye aktarilmasidir. Bu sekilde agirlik merkezi zemine yaklastirilarak aracin savrulmasina olumsuz etkide bulunmasi engellenmektedir. En büyük avantaji keskin virajlarda yol tutusunda kayip yasanmamasi olarak degerlendirilmektedir. The main purpose of the wing, which is the subject of the invention; without touching any other element of the vehicle. By connecting it directly to the chassis via the fasteners, both its own weight and It is the direct transfer of the force arising from the wind pressure to the chassis. In this way the center of gravity It is prevented from having a negative effect on the vehicle's skidding by being brought closer to the ground. The biggest The advantage is that there is no loss of road holding in sharp bends.
Bulusun baska bir amaci; araç gövdesi üzerinde olusturulan delikler sayesinde baglanti elemanlarinin temassiz sekilde saseye ulasmasinin saglanmasidir. Böylece baglanti elemanlari için farkli ve agirligi artiracak tasarimlara ihtiyaç duyulmamakta ve en kisa yoldan saseye ulasilmasi saglanmaktadir. Another object of the invention is; connection thanks to the holes formed on the vehicle body It is to ensure that the elements reach the chassis without contact. Thus, the fasteners There is no need for different and weight-increasing designs and the shortest way is to the chassis. access is provided.
Yukarida bahsedilen amaçlara en genel haliyle ulasilmasi için aracin diger unsurlari ile temas etmeden dogrudan saseye baglanan ve bu sekilde hem kendi agirligini hem de hizdan olusan ters kuvveti dogrudan saseye aktararak agirlik merkezini zemine yaklastiran kanat gelistirilmistir. In order to achieve the above-mentioned purposes in the most general form, contact with other elements of the vehicle directly connected to the chassis and in this way, both its own weight and speed A wing has been developed that brings the center of gravity closer to the ground by transferring the force directly to the chassis.
Gelistirilen kanat; araçlarda istenilmeyen hava akisini düzenleyerek yol tutusunu artiran kanat ve kanadin araç üzerinde diger unsurlara temas etmeden dogrudan sasesine baglantisini saglayan en az bir baglanti elemani içermektedir. Developed wing; wing and wing that increase road holding by regulating the undesired air flow in vehicles and It provides direct connection of the wing to the chassis without contacting other elements on the vehicle. contains at least one connecting element.
Bulusun yapisal ve karakteristik özellikleri ve tüm avantajlari asagida verilen sekiller ve bu sekillere atiflar yapilmak suretiyle yazilan detayli açiklama sayesinde daha net olarak anlasilacaktir ve bu nedenle degerlendirmenin de bu sekiller ve detayli açiklama göz Önüne alinarak yapilmasi gerekmektedir. Structural and characteristic features and all advantages of the invention are given in the following figures and these figures. It will be understood more clearly thanks to the detailed explanation written with references and this For this reason, the evaluation should be made by taking these figures and detailed explanation into consideration. required.
Bulusun Anlasilmasina Yardimci Olacak Sekiller Mevcut bulusun yapilanmasi ve ek elemanlarla birlikte avantajlarinin en iyi sekilde anlasilabilmesi için asagida açiklamasi yapilan sekiller ile birlikte degerlendirilmesi gerekir. Figures to Help Understand the Invention The structuring of the present invention and the best understanding of its advantages with additional elements should be evaluated together with the figures explained below.
Sekil- 1: Bulusa konu olan kanadin araca takili halde genel görünümüdür. Figure- 1: The general view of the wing, which is the subject of the invention, when it is attached to the vehicle.
Sekil- 2: Bulusa konu olan kanadin araca takili halde iken yakindan izomerik görünümüdür. Figure- 2: A close isomeric view of the wing, which is the subject of the invention, when it is attached to the vehicle.
Parça Referanslari Kanat yapilanmasi 1 1 Kanat 12 Baglanti elemani Araç 21 Gövde 22 Delik 23 Sase Bulusun Detayli Açiklamasi Araçlarda (20) kullanilmak üzere gelistirilen düsük agirlik merkezli kanat yapilanmasi (10), temel olarak; istenilmeyen hava akisini düzenleyerek yol tutusunu artiran kanat (11) ve kanadin (11) araç (20) üzerinde diger unsurlara temas etmeden dogrudan sasesine (23) baglantisini saglayan baglanti elemani (12) içermektedir. Sekil 1'de bulusa konu olan kanat yapilanmasi (10) araca (20) takili halde genel görünümü bulunmaktadir. Sayisi degisebilmekle birlikte tercihen edilen yapilanmadan kanat (11) araca (20) iki adet baglanti eleman (12) ilismektedir Baglanti elemanlari (12) Sekil 2'deki kanat yapilanmasinin (10) araca (20) takili halde iken yakindan izomerik görünümünde gösterildigi gibi aracin (20) gövdesi (21) üzerinde olusturulan deliklerden (22) geçerek sase (23) ile irtibat saglamaktadirlar. Bu sekilde baglanti elemaninin (12) kaput, döseme, vb. gibi gövde (21) unsurlarindan temassiz sekilde geçisi mümkün kilinmaktadir. Part References Wing construction 1 1 Wing 12 connectors Vehicle 21 Body 22 Holes 23 Sass Detailed Description of the Invention The low center of gravity wing configuration (10) developed for use in vehicles (20) aspect; The wing (11) and the wing (11), which increase the road holding by regulating the undesired air flow, (20) is directly connected to its chassis (23) without touching other elements. connection element (12). In Figure 1, the wing configuration (10) which is the subject of the invention is compared to the vehicle (20) It has a general view attached. Although the number may vary, the preferred Before the wing (11) is configured, two connection elements (12) are attached to the vehicle (20). With the fasteners (12) attached to the vehicle (20), the wing configuration (10) in Figure 2 formed on the body (21) of the vehicle (20) as shown in its closely isomeric view. they pass through the holes (22) and provide contact with the chassis (23). In this way, the connector (12) hood, trim, etc. It is possible to pass through the body (21) elements such as the body without contact.
Dolayisiyla kanat yapilanmasinin(10) agirliginin ve kanat (11) üzerinde rüzgâr basinci ile olusan baski kuvvettin dagilmadan dogrudan saseye (23) verilmesi amaçlanmistir. Tüm kuvvetlerin sasede (23) odaklanmasi ile agirlik merkezi de zemine yaklastirilmakta ve yol tutusu artirilmaktadir. Söz konusu baglanti elemaninin (12) direk araç (20) sasesine (23) sabitlenmesi kaynak veya farkli sabitleme teknikleri ile saglanmaktadir. Bununla birlikte ayrica Civata, somu gibi farkli sabitleme elemanlariyla da sabitleme isleminin gerçeklestirilmesi imkan dahilindedir. Therefore, the weight of the wing structure (10) and the wind pressure on the wing (11) It is aimed to give the pressure force directly to the chassis (23) without dispersion. of all forces By focusing on the chassis (23), the center of gravity is also brought closer to the ground and the road holding is being increased. Fixing the said fastener (12) directly to the vehicle (20) chassis (23) It is provided by welding or different fixing techniques. However, there are also Bolts, Nuts etc. It is also possible to perform the fixing process with different fixing elements.
Düsük Agirlik Merkezli Kanat Yapilanmasi Araçlarda (20) istenilmeyen hava akisini düzenleyerek yol tutusunu artiran kanat (11) unsuru haiz düsük agirlik merkezli kanat yapilanmasi (10) olup, özelligi; bahsedilen kanadin (11) araç (20) üzerinde diger unsurlara temas etmeden dogrudan sasesine (23) baglantisini saglayan en az bir baglanti elemani (12) içermesidir. Böylece kanat yapilanmasi (10) aracin (20) diger unsurlari ile temas etmeden dogrudan saseye (23) baglantisi saglanmakta ve hem kendi agirligini hem de hizdan olusan ters kuvveti dogrudan saseye (23) aktararak agirlik merkezini zemine yaklastirmasi mümkün kilinmaktadir. Low Weight Center Wing Configuration Vehicles (20) have a wing (11) element that increases road holding by regulating the undesired air flow. Low center of gravity wing structure (10), its feature is; said wing (11) vehicle (20) at least one that provides direct connection to the chassis (23) without contacting other elements. connection element (12). Thus, the wing configuration (10) is combined with the other elements of the vehicle (20). It is directly connected to the chassis (23) without contacting, and both its own weight and It brings the center of gravity closer to the ground by transferring the reverse force consisting of speed directly to the chassis (23). is made possible.
Claims (1)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
TR2016/03532A TR201603532A2 (en) | 2016-03-18 | 2016-03-18 | LOW WEIGHT CENTERED WING STRUCTURE |
PCT/TR2016/050301 WO2017160247A1 (en) | 2016-03-18 | 2016-08-22 | Spoiler wing embodiment with low center of gravity |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
TR2016/03532A TR201603532A2 (en) | 2016-03-18 | 2016-03-18 | LOW WEIGHT CENTERED WING STRUCTURE |
Publications (1)
Publication Number | Publication Date |
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TR201603532A2 true TR201603532A2 (en) | 2016-06-21 |
Family
ID=57145014
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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TR2016/03532A TR201603532A2 (en) | 2016-03-18 | 2016-03-18 | LOW WEIGHT CENTERED WING STRUCTURE |
Country Status (2)
Country | Link |
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TR (1) | TR201603532A2 (en) |
WO (1) | WO2017160247A1 (en) |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS60163772A (en) * | 1984-02-03 | 1985-08-26 | Mitsubishi Motors Corp | Rear spoiler for car |
US6712424B2 (en) * | 2002-04-29 | 2004-03-30 | Daniel B. Swain | Hitch receiver mounted spoiler |
DE102008005194B4 (en) * | 2008-01-18 | 2011-03-17 | Hs Genion Gmbh | Air guiding device of a vehicle |
GB2473293A (en) * | 2009-09-08 | 2011-03-09 | Trysome Ltd | A variable aerodynamic device for a motor vehicle |
CN103342137B (en) | 2013-07-09 | 2015-06-03 | 大连理工大学 | Air flow adjustment type car tail spoiler |
-
2016
- 2016-03-18 TR TR2016/03532A patent/TR201603532A2/en unknown
- 2016-08-22 WO PCT/TR2016/050301 patent/WO2017160247A1/en active Application Filing
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Publication number | Publication date |
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WO2017160247A1 (en) | 2017-09-21 |
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