Coupling body using Z-pin
10184212 ยท 2019-01-22
Assignee
Inventors
- Ik Hyeon Choi (Daejeon, KR)
- Ho Sung Lee (Daejeon, KR)
- Gi Hyuk Choi (Daejeon, KR)
- In Hee Hwang (Daejeon, KR)
Cpc classification
B29C66/7212
PERFORMING OPERATIONS; TRANSPORTING
B29C70/86
PERFORMING OPERATIONS; TRANSPORTING
B29C66/534
PERFORMING OPERATIONS; TRANSPORTING
B29C65/02
PERFORMING OPERATIONS; TRANSPORTING
F16C2326/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29L2031/30
PERFORMING OPERATIONS; TRANSPORTING
B29C66/7212
PERFORMING OPERATIONS; TRANSPORTING
B29C65/564
PERFORMING OPERATIONS; TRANSPORTING
F16D1/064
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16C3/026
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29C70/222
PERFORMING OPERATIONS; TRANSPORTING
B29C66/72141
PERFORMING OPERATIONS; TRANSPORTING
B29C66/131
PERFORMING OPERATIONS; TRANSPORTING
Y10T403/472
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
B29L2031/737
PERFORMING OPERATIONS; TRANSPORTING
B29C70/24
PERFORMING OPERATIONS; TRANSPORTING
D07B1/02
TEXTILES; PAPER
Y10T29/49947
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
International classification
D07B9/00
TEXTILES; PAPER
B29C65/00
PERFORMING OPERATIONS; TRANSPORTING
B29C65/56
PERFORMING OPERATIONS; TRANSPORTING
B29C70/86
PERFORMING OPERATIONS; TRANSPORTING
F16C3/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16D1/064
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B29C70/24
PERFORMING OPERATIONS; TRANSPORTING
B29C65/02
PERFORMING OPERATIONS; TRANSPORTING
D07B1/02
TEXTILES; PAPER
Abstract
Coupling body devices, including methods of making the same, are provided and described. A method of manufacturing a coupling body, for example, can include forming a tube by braiding nonmetal fibers, forming a flange by rolling inwards an end of the tube, providing a metallic connector, inserting at least one Z-pin in an end portion of the connector, and coupling the tube and the connector by inserting the Z-pin in the flange and performing a composite material forming process.
Claims
1. A coupling body, comprising: a tube formed by a plurality of nonmetal fibers being braided with one another, and of which an end portion comprises a flange; a metallic connector comprising an end portion corresponding to the flange, and at least one Z-pin fixed to the end portion of the connector, wherein the connector and the tube are coupled with the at least one Z-pin extending into the flange end portion of the tube.
2. The coupling body of claim 1, wherein the nonmetal fibers comprise a carbon fiber.
3. The coupling body of claim 1, wherein the end portion of the connector comprises at least one Z-pin accommodating groove into which the at least one Z-pin is inserted.
4. The coupling body of claim 1, wherein the Z-pin is fixed to the end portion of the connector through welding.
5. The coupling body of claim 1, wherein the flange is formed by rolling inwards an end of the tube and spreading outwards the inwardly rolled end of the tube.
6. The coupling body of claim 1, further comprising a metal skin covering an outer side of the tube and the connector in a coupled state.
7. The coupling body of claim 1, further comprising a surface protection agent coated on the tube, where the surface protection agent is applied after the tube and the connector are coupled.
8. The coupling body of claim 1, wherein the end portion of the connector is a flange.
9. A method of manufacturing a coupling body, comprising: forming a tube by braiding a plurality of nonmetal fibers; forming a flange by rolling inwards an end of the tube and spreading outwards the inwardly rolled end of the tube; providing a metallic connector; fixing at least one Z-pin to an end portion of the connector; and coupling the tube and the connector by inserting the Z-pin in the flange and performing a composite material forming process.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) These and/or other aspects, features, and advantages of the invention will become apparent and more readily appreciated from the following description of embodiments, taken in conjunction with the accompanying drawings of which:
(2)
(3)
(4)
(5)
(6)
(7)
DETAILED DESCRIPTION
(8) Hereinafter, example embodiments are described with reference to the accompanying drawings, wherein like reference numerals refer to the like elements throughout. Also, it is noted that the disclosures in the claims are not limited by the example embodiments to be described below, and the configuration described in the example embodiments is not required for solving the example embodiments.
(9)
(10) The coupling body 100 includes the tube 120 including a flange 122 formed by nonmetal fibers braided with one another, and the connector 110 of a metal material including an end portion corresponding to the flange 122. At least one Z-pin 111 is inserted in the end portion of the connector 110, and the connector 110 is coupled with the tube 120 through the Z-pin 111 being inserted in the flange 122 of the tube 120 and through a composite material forming process. The composite material forming process indicates a process in which parts of different types are coupled and closely attached to one other through thermal treatment performed at a high temperature.
(11) At an initial operation of forming the tube 120, an end portion of the tube 120 is not formed to be a smooth surface and includes a curved portion, and thus portions of the tube 120 and the connector 110 to come in contact may not be closely attached although the tube 120 of a nonmetal material is coupled with the connector 110 through the Z-pin 111.
(12) Thus, after the connector 110 is coupled with the tube 120 by the Z-pin 111 being inserted in the end portion of the tube 120, the tube 120 is heated at a high temperature through the composite material forming process to allow an end surface of the tube 120 to be closely attached to a corresponding surface of the connector 110 and to allow the Z-pin 111 to be more strongly attached to the nonmetal fibers of the tube 120.
(13) The connector 110 is provided in a state in which the Z-pin 111 is inserted in advance, and the Z-pin 111 is densely inserted along a circumferential direction of the end portion of the connector 110. The number of Z-pins to be used may be determined to allow coupling of the connector 110 and the flange 122 of the tube 120 to be maximal.
(14) A length of the Z-pin 111 extended from the connector 110 needs not to exceed a thickness of the flange 122 of the tube 120.
(15) The Z-pin 111 may be inserted along a circumference of the flange 122 of the tube 120, and the Z-pin 111 may not be inserted in a central portion of the connector 110 which corresponds to the portion connected to the internal hollow space in the end portion of the flange 122 of the tube 120.
(16)
(17) Although the connector 110 of a metal material may be engaged with the tube 120 using a bolt, the Z-pins 111 may be fixed to the metallic connector 110 through welding and such, and the Z-pins 111 may be inserted in the flange 122 to form the connection.
(18) Referring to
(19) The end portion 112 of the connector 110 includes Z-pin accommodating grooves 113 to indicate respective locations in which the Z-pins 111 are to be inserted and to facilitate the insertion. The grooves 113 are formed in a shape of end surfaces of the Z-pins 111 for the Z-pins 111 to be smoothly inserted.
(20) Referring to
(21) Here, the Z-pins 111 may not be smoothly inserted if the tube 120 is formed with a metal material as in the connector 110. However, when the braided tube 120 is formed with a carbon fiber material, the Z-pins 111 may be inserted in gaps in the carbon fiber material because the fiber has gaps therein. In addition, since a carbon fiber is elastic, the inserted Z-pins 111 are surrounded by the carbon fiber and receive pressure therefrom. Thus, once the Z-pins 111 are inserted in the tube 120, the Z-pins 111 may not fall out.
(22) The flange 122 is formed by rolling inwards an end of the tube 120 and spreading outwards the rolled end.
(23) According to an example embodiment, in manufacturing a composite material tube, a tube may be formed using a forming method of inserting resin in a woven carbon fiber which is braided in a tube form, instead of using a filament winding method. In detail, a portion to be connected to a connector may be secured by overlapping inwards opposite end portions of the fiber and spreading outwards the portions to be in a flange form.
(24) To prevent damage to the composite material tube 120, a metal skin 127 is provided to cover an outer side of the tube 120 after the tube 120 is coupled with the connector 110 to 20 reinforce impact resistance, or a surface protection agent 129 is provided to coat the tube 120 to reinforce impact resistance.
(25) The nonmetal fibers may include a carbon fiber. The carbon fiber may be obtained by thermally processing an organic fiber in an inert gas at an appropriate temperature and carbonizing and crystallizing the fiber. The carbon fiber, as a graphite carbon, has a suitable mechanical property such as high strength and high stiffness. In addition, the carbon fiber may be manufactured by carbonizing an acrylic fiber as a raw material at a temperature of 1,000 to 1,500 C. in an inert state in which a chemical reaction such as oxidation does not occur.
(26) The carbon fiber may be used as a fiber for a composite material, for example, as a reinforced fiber for a plastic material, due to properties such as high strength and high elasticity. When the carbon fiber is used as a reinforced material, the carbon fiber may be utilized as a carbon fiber-reinforced plastic. The carbon fiber may be used for sports goods such as tennis rackets and golf shafts. In addition, the carbon fiber may be used as a material for a gas structure of a space shuttle due to high heat resistance.
(27)
(28) The method of manufacturing the coupling body includes operation 125 of forming a tube by braiding nonmetal fibers, operation 126 of forming a flange by rolling inwards an end of the tube, operation 130 of providing a metallic connector, operation 150 of inserting at least one Z-pin in an end portion of the connector, operation 160 of matching a center of the tube to a center of the connector, and operation 170 of coupling the tube and the connector by inserting the Z-pin in the flange.
(29) Referring to
(30) To arrange, to be smooth, an outer surface of a portion of the flange in which the tube and the connector are coupled, an end surface of the flange and an end surface of the connector may need to have matching profiles.
(31) When the end surface of the flange and the end surface of the connector have matching profiles, matching the center of the tube to the center of the connector may be more readily performed.
(32) Subsequent to the operation 130 of providing the metallic connector, the method further includes operation 140 of forming a Z-pin accommodating groove to indicate locations of an end portion of the metallic connector in which Z-pins are to be inserted and to facilitate the insertion.
(33) In manufacturing the connector, when using a casting process, a cast may be manufactured to provide the Z-pin accommodating groove in the cast in advance. When using a forging process, the connector may be formed in advance and the Z-pin accommodating groove may be cut therefrom through drilling or milling. Alternatively, a basic form of the connector may be first manufactured and the Z-pins may be welded directly into a surface of the connector.
(34)
(35) Referring to
(36) According to example embodiments, a coupling body may be highly productive compared to invested costs for equipment, because braided woven fibers are used to manufacture a composite material tube portion, instead of using a filament winding method.
(37) In addition, structural safety may be improved because stress concentration may not occur in a certain portion of a flange and cutting of a reinforced fiber due to a bolt hole may not occur by using Z-pins, in lieu of a bolt, in a portion connected to the flange and a connector.
(38) Further, a load may be evenly transferred to the portion connected to the flange, and thus weight lightening of the flange portion may be enabled.
(39) According to example embodiments described herein, a coupling body may be used to reduce costs of investment in equipment by using a braided woven product without using a filament winding method to manufacture a composite material tube portion.
(40) In the coupling body, a Z-pin may be used without using a bolt in a portion connected to a flange.
(41) In the coupling body, stress concentration that may be generated in a portion of the flange may be eliminated and cutting of a reinforced fiber due to a bolt hole may be prevented.
(42) In the coupling body, a load may be evenly transferred to the portion connected to the flange, and thus a weight of the flange portion may be reduced
(43) Although a few embodiments of the present invention have been shown and described, the present invention is not limited to the described embodiments. Instead, it would be appreciated by those skilled in the art that changes may be made to these embodiments without departing from the principles and spirit of the invention, the scope of which is defined by the claims and their equivalents.