KR200160693Y1 - Flange connection structure of propeller shaft - Google Patents
Flange connection structure of propeller shaft Download PDFInfo
- Publication number
- KR200160693Y1 KR200160693Y1 KR2019960057102U KR19960057102U KR200160693Y1 KR 200160693 Y1 KR200160693 Y1 KR 200160693Y1 KR 2019960057102 U KR2019960057102 U KR 2019960057102U KR 19960057102 U KR19960057102 U KR 19960057102U KR 200160693 Y1 KR200160693 Y1 KR 200160693Y1
- Authority
- KR
- South Korea
- Prior art keywords
- propeller shaft
- flange
- steel flange
- steel
- fastening
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K17/00—Arrangement or mounting of transmissions in vehicles
- B60K17/22—Arrangement or mounting of transmissions in vehicles characterised by arrangement, location, or type of main drive shafting, e.g. cardan shaft
- B60K17/24—Arrangements of mountings for shafting
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2208/00—Plastics; Synthetic resins, e.g. rubbers
- F16C2208/80—Thermosetting resins
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2326/00—Articles relating to transporting
- F16C2326/01—Parts of vehicles in general
- F16C2326/06—Drive shafts
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C3/00—Shafts; Axles; Cranks; Eccentrics
- F16C3/02—Shafts; Axles
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
Abstract
본 고안은 프로펠러 샤프트 플랜지의 구조를 개량하여 체결력을 증대시킨 프로펠러 샤프트 플랜지 체결 구조에 관한 것으로, 스틸 플랜지(10)의 외주면(11)을 각형으로 형성하고, 상기 스틸 플랜지(10)의 내경(12)에 삽입되어지게 형성된 프로펠러 샤프트(20)의 접속부(21)가 체결되며, 스틸 플랜지(10)와 프로펠러 샤프트(20)의 외주면에 보강튜브(30)가 필라멘트 와인딩공법에 의해 체결되어서 구성된 것이다.The present invention relates to a propeller shaft flange fastening structure in which the fastening force is increased by improving the structure of the propeller shaft flange. The connection portion 21 of the propeller shaft 20 formed to be inserted into the fastening is fastened, and the reinforcing tube 30 is fastened to the outer circumferential surface of the steel flange 10 and the propeller shaft 20 by a filament winding method.
Description
본 고안은 프로펠러 샤프트 플랜지에 관한 것으로, 특히 스틸 플랜지의 구조를 개량하여 체결력을 증대시킨 프로펠러 샤프트 플랜지 체결 구조에 관한 것이다.The present invention relates to a propeller shaft flange, and more particularly, to a propeller shaft flange fastening structure that improves the fastening force by improving the structure of the steel flange.
프로펠러 샤프트는, FR자동차에서 트랜스미션과 디퍼렌셜 기어를 연결하여 동력을 전달하는 추진축, 중공(中空)의 탄소강관을 사용하는 것이 보통이지만 양 끝에 유니버설 조인트가 장착되어 있다.The propeller shaft generally uses propulsion shafts and hollow carbon steel pipes that transmit power by connecting transmission and differential gears in FR vehicles, but universal joints are mounted at both ends.
끊임없이 비틀림 토크를 받으면서 고속 회전하기 때문에 길이가 긴 프로펠러 샤프트는 진동이 발생되어 파손되기 쉬우므로 조인트를 2개 또는 3개를 사용한 분할식이 많다.Because of the high speed rotation under constant torsional torque, long propeller shafts are easy to break due to vibrations, so there are many split types using two or three joints.
상기 복합재료인 프로펠러 샤프트에 스틸 플랜지를 체결하기 쉽지 않았으며, 프로펠러 샤프트에 스틸 플랜지를 체결하기 위한 체결 구조의 개발이 지속되어 왔다.It was not easy to fasten the steel flange to the propeller shaft of the composite material, the development of a fastening structure for fastening the steel flange to the propeller shaft has been continued.
본 고안의 기술적 과제는, 복합재료인 프로펠러 샤프트의 가공방법으로 인하여 스틸 플랜지의 체결 구조를 개선하는데 제약이 있었으며, 이로 인하여 프로펠러 샤프트와 스틸 플랜지의 체결력 증대에 한계가 있었으며, 체결력을 증대하기 위해서는 그 구조가 복잡해지는 문제점을 해결하기 위한 것이다.The technical problem of the present invention has been a limitation in improving the fastening structure of the steel flanges due to the processing method of the propeller shaft, which is a composite material. As a result, there is a limit in increasing the fastening force of the propeller shaft and the steel flange. This is to solve the problem of complicated structure.
제1도는 본 고안에 의한 프로펠러 샤프트 플랜지 체결부위를 발췌한 분리 구성도.Figure 1 is an exploded configuration diagram extracting the propeller shaft flange fastening portion according to the present invention.
제2도는 본 고안에 의한 프로펠러 샤프트 플랜지 체결부위를 결합 단면 구성도.Figure 2 is a cross-sectional configuration of the coupling portion of the propeller shaft flange fastening according to the present invention.
＜도면의 주요부분에 대한 부호의 설명＞<Description of the code | symbol about the principal part of drawing>
10 : 스틸 플랜지 11 : 외주면10 steel flange 11 outer peripheral surface
12 : 내경 20 : 프로펠러 샤프트12: inner diameter 20: propeller shaft
21 : 접속부 30 : 보강튜브21: connection part 30: reinforcement tube
이하 첨부도면에 의거, 본 고안의 바람직한 실시예를 설명한다.Hereinafter, preferred embodiments of the present invention will be described based on the accompanying drawings.
도1은 본 고안에 의한 프로펠러 샤프트 플랜지 체결 구조를 발췌한 분리 구성도이고, 도2은 본 고안에 의한 프로펠러 샤프트 플랜지 체결 구조의 결합 단면 구성도이다.Figure 1 is a separate configuration of the propeller shaft flange fastening structure according to the present invention, Figure 2 is a coupling cross-sectional view of the propeller shaft flange fastening structure according to the present invention.
본 고안의 프로펠러 샤프트 플랜지 체결 구조는, 스틸 플랜지(10)의 외주면(11)을 각형으로 형성하고, 상기 스틸 플랜지(10)의 내경(12)에 삽입되어지게 형성된 프로펠러 샤프트(20)의 접속부(21)가 체결되며, 스틸 플랜지(10)와 프로펠러 샤프트(20)의 외주면에 보강튜브(30)가 필라멘트 와인딩공법에 의해 체결되어서 구성된 것이다.The propeller shaft flange fastening structure of the present invention, the outer peripheral surface 11 of the steel flange 10 is formed in a square, the connection portion of the propeller shaft 20 formed to be inserted into the inner diameter 12 of the steel flange 10 ( 21 is fastened, and the reinforcement tube 30 is fastened to the outer circumferential surface of the steel flange 10 and the propeller shaft 20 by the filament winding method.
상기 스틸 플랜지(10)의 외주면(11)은 육각형 또는 팔각형으로 형성된 것이다.The outer circumferential surface 11 of the steel flange 10 is formed in a hexagonal or octagonal shape.
본 고안의 작용을 설명하면 다음과 같다.Referring to the operation of the present invention is as follows.
먼저, 스틸 플랜지(10)의 내경으로 복합재료인 프로펠러 샤프트(20)의 접속부(21)를 끼워 체결한다.First, the connection part 21 of the propeller shaft 20 which is a composite material is inserted and fastened to the inner diameter of the steel flange 10.
상기한 상태에서 스틸 플랜지(10)와 프로펠러 샤프트(20)에 걸쳐 위치하도록 보강튜브(30)를 체결하다.In the above state, the reinforcing tube 30 is fastened to be positioned over the steel flange 10 and the propeller shaft 20.
상기한 보강튜브(30)의 체결은 FRP의 연속 필라멘트를 스틸 플랜지와 프로펠러 샤프트의 표면에 장력을 가해서 감아붙여 열경화시켜 접착 형성시킨다.The fastening of the reinforcing tube 30 is applied to the surface of the steel filament and the propeller shaft by applying the tension of the continuous filament of the FRP and heat-cured to form an adhesive.
상기한 보강튜브(30)는 스틸 플랜지(10)의 외주면(11)이 각을 이루며 형성되어 있어 많은 면이 면접촉되어 진다.The reinforcement tube 30 is formed in the outer circumferential surface 11 of the steel flange 10 at an angle, so that many surfaces are in surface contact.
이상 설명된 본 고안의 프로펠러 샤프트 플랜지 체결 구조는, 외주면이 각을 이룬 스틸 플랜지의 내주면으로 복합재료로된 프로펠러 샤프트의 접속부를 끼워 체결하고 스틸 플랜지와 복합재료로된 프로펠러 샤프트에 걸쳐 보강튜브를 필라멘트 와인딩공법에 의해 형성한 것으로써, 그 구조가 단순하면서도 접촉면이 증가되어 스틸 플랜지와 복합재료로된 프로펠러 샤프트의 체결력을 증대시킴과 동시에 제품의 신뢰성을 향상시킬 수 있는 효과를 나타낸다.The propeller shaft flange fastening structure of the present invention described above is fastened by fitting the connection part of the propeller shaft made of composite material to the inner circumferential surface of the steel flange having an outer circumferential surface and filamenting the reinforcing tube over the steel flange and the propeller shaft made of the composite material. Formed by the winding method, the structure is simple, but the contact surface is increased to increase the fastening force of the propeller shaft made of steel flange and composite material, and at the same time improve the reliability of the product.
본 고안은, 외주면이 각을 이룬 스틸 플랜지의 내주면으로 복합재료로된 프로펠러 샤프트의 접속부를 끼워 체결하고 스틸 플랜지와 복합재료로된 프로펠러 샤프트에 걸쳐 보강튜브를 필라멘트 와인딩공법에 의해 형성한 것으로써, 그 구조가 단순하면서도 접촉면이 증가되어 스틸 플랜지와 복합재료로된 프로펠러 샤프트의 체결력을 증대시킴과 동시에 제품의 신뢰성을 향상시킬 수 있는 프로펠러 샤프트 플랜지 체결구조를 제공하는 것에 그 목적을 둔다.The present invention is to fasten the connection portion of the propeller shaft made of composite material to the inner circumferential surface of the steel flange with an outer circumferential surface, and to form a reinforcement tube by the filament winding method over the steel flange and the propeller shaft made of the composite material, The object of the present invention is to provide a propeller shaft flange fastening structure capable of improving the reliability of the product while increasing the fastening force of the propeller shaft made of the steel flange and the composite material by increasing the contact surface with a simple structure.
Claims (2)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| KR2019960057102U KR200160693Y1 (en) | 1996-12-26 | 1996-12-26 | Flange connection structure of propeller shaft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| KR2019960057102U KR200160693Y1 (en) | 1996-12-26 | 1996-12-26 | Flange connection structure of propeller shaft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| KR19980043977U KR19980043977U (en) | 1998-09-25 |
| KR200160693Y1 true KR200160693Y1 (en) | 1999-11-15 |
Family
ID=19483407
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| KR2019960057102U KR200160693Y1 (en) | 1996-12-26 | 1996-12-26 | Flange connection structure of propeller shaft |
Country Status (1)
| Country | Link |
|---|---|
| KR (1) | KR200160693Y1 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR101588846B1 (en) * | 2014-07-03 | 2016-01-27 | 효림산업 주식회사 | A propeller shaft for automobiles, and a manufacturing method of the product |
-
1996
- 1996-12-26 KR KR2019960057102U patent/KR200160693Y1/en not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| KR19980043977U (en) | 1998-09-25 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4932924A (en) | Torque transmitting assembly | |
| US5851152A (en) | Drive shaft with reinforced plastic tube and a joint-connecting body connected nonrotatably endwise | |
| JPH0554567B2 (en) | ||
| US4892433A (en) | Process for producing a joint between a metallic inner sleeve and a tube of fiber-reinforced plastic material and the resulting joint produced thereby | |
| JPS61142241A (en) | Tensile compression stay having fiber reinforced synthetic resin pillar | |
| KR200160693Y1 (en) | Flange connection structure of propeller shaft | |
| CN200978896Y (en) | Sleeve diaphragm coupler | |
| CN209724991U (en) | A kind of automobile-used waveform composite material transmission shaft assembly | |
| EP1129301A4 (en) | Improved elastomer coupling having cylindrical surface hubs | |
| US5868626A (en) | Universal joint yoke having axially-extending grooves | |
| CN214661588U (en) | Polygonal deformation expansion structure | |
| KR100410781B1 (en) | Structure for bonding steel yoke into tube for propeller shaft | |
| JPH0755384Y2 (en) | Resin power transmission shaft | |
| KR19980064609U (en) | Propulsion shaft assembly of vehicle | |
| JPS63199914A (en) | Joint joining method for fiber reinforced plastics-made propeller shaft | |
| KR20190031710A (en) | Cfrp propeller shafts for vehicle | |
| JP3292351B2 (en) | FRP cylinder | |
| KR19980040342U (en) | Automotive Propulsion Shaft Flange Yoke Joint for Shock Absorption | |
| KR20220138678A (en) | Stub shaft and shaft connection structure including the same | |
| KR100190327B1 (en) | Transmission shaft | |
| KR19990039281U (en) | Joint structure of low vibration composite propulsion shaft | |
| KR19980013112U (en) | Anti-vibration damper on propeller shaft | |
| KR200279000Y1 (en) | Joint structure of composite transmission shaft | |
| JPH02236013A (en) | Driving shaft made of fiber reinforced plastic | |
| KR20000016341U (en) | Universal joint of steering apparatus for vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A201 | Request for examination | ||
| E701 | Decision to grant or registration of patent right | ||
| REGI | Registration of establishment | ||
| FPAY | Annual fee payment |
Payment date: 20050817 Year of fee payment: 7 |
|
| LAPS | Lapse due to unpaid annual fee |