GB2228693A - Small thick-walled composite metal tubing - Google Patents
Small thick-walled composite metal tubing Download PDFInfo
- Publication number
- GB2228693A GB2228693A GB9002613A GB9002613A GB2228693A GB 2228693 A GB2228693 A GB 2228693A GB 9002613 A GB9002613 A GB 9002613A GB 9002613 A GB9002613 A GB 9002613A GB 2228693 A GB2228693 A GB 2228693A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuel injection
- composite metal
- injection tubing
- metal fuel
- steel pipe
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D51/00—Making hollow objects
- B21D51/02—Making hollow objects characterised by the structure of the objects
- B21D51/06—Making hollow objects characterised by the structure of the objects folded objects
-
- 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
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L9/00—Rigid pipes
- F16L9/02—Rigid pipes of metal
- F16L9/04—Reinforced pipes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02M—SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
- F02M55/00—Fuel-injection apparatus characterised by their fuel conduits or their venting means; Arrangements of conduits between fuel tank and pump F02M37/00
- F02M55/02—Conduits between injection pumps and injectors, e.g. conduits between pump and common-rail or conduits between common-rail and injectors
-
- 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
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L9/00—Rigid pipes
- F16L9/18—Double-walled pipes; Multi-channel pipes or pipe assemblies
-
- 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
- F02B3/00—Engines characterised by air compression and subsequent fuel addition
- F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Fuel-Injection Apparatus (AREA)
- Pressure Welding/Diffusion-Bonding (AREA)
- Rigid Pipes And Flexible Pipes (AREA)
Description
B&S No C9U/4 SMALL THICK-WALLED COMPOSITE METAL TUBING AND PROCESS OF
PRODUCING THE SAME This invention relates to a high pressure fuel injection pipe for a fuel supply passage of a diesel engine and to a process of producing the small thick-walled metal fuel i.njection tubing.
Generally, in a high pressure fuel injection pine of the described type such as f or a diesel engine, high pressure fuel flows inside the injection pine under the conditions, i.e. an injection tire cf about 5 nil!4Lseconds, a flow speed of at most abcu,;L-. 15 n/sec and an internal pressure of 200 - 600 kg/c::.2 (peak pressure); either flow speed or internal pressure fluctuates frequently and sharply.
As can be seen in, for example, a tubing fcr a high pressure fuel pipe, this type of cor.,ncsite netal 1 tubing has heretofore been formed by a procedure which comprises the press-fitting of large and small diameter high pressure piping carbon steel pipes (JIS G 3455 STS 38), each having a copper plating film preliminarily provided around the circumferential mating surface thereof, and subsequent heat-treating of them to effect mutual brazing with the copper plating films as the filler which are present around the circumferential mating surfaces, or by a simple procedure which comprises inserting one of two pipes having mutually different diameters' into the other and mutually press-fitting then by solid drawing or the like.
However, according to the former of these conventional procedures, complicated steps are needed because copper plating must be applied around the inner surface and the outer surface of the pipes. If the brazing is inadequate, the mutually press-fitted mating circumferential surfaces undergoes a relaxation phenomenon to create a gap from which portion a possible breakage due to fatigue tends to progress. Yet if the brazing is adequate, only a limited degree of proofness against vibration can be obtained as the base metal becomes soft due to the heat during brazing. Therefore an excellent composite fuel injection tubing cannot be achieved.
4 3 - According to the latter conventional procedure, because the resulting configuration has the mating faces simply subjected to press-fitting, the mating circumferential interface disadvantageously undergoes a relaxation_ phenomenon leading to reduction of the mechanical strength when the composite tubing is used as a fuel injection pipe. Coupled with vibration during rotation of an engine, this often gives rise to cracking or breakage.
As countermeasures have been made in recent years in increasing the power as well as in reducing NOx and minimizing black smoke, the tendency of highly pressurizing fuel is particularly on the rise. A high pressure fuel injection tubing has thus been demanded which can be used under the conditions, e.g. an injection time of 1 - 2 milliseconds, a flow speed of at most about 50 m/sec and an internal pressure of 600 1,000 kg/cm2 (peak pressure). Consequently, under such severe conditions, a high pressure fuel injection pipe most highly requires (1) durability against fatigue due to the repeated high pressure loading, (2) resistance to cavitation erosion, and (3) proofness against vibration from the vehicle body. So safety measures against cracxing and breakage of the injection pipe hdve been very significant.
To this end, as attempted measures to deal with the severe conditions, it has been proposed that a small diameter thick-walled pipe having a wall thickness of 25 - 40% of its outside diameter is used for the inner tubular member of a high pressure fuel injection pipe, that the inner wall surface of the inner tubular member has no irregular wavy swells which would be a cause for development of fuel eddy resistance, and that there is eliminated a gap, between the thick-walled inner tubular member and the outer tubular member, which would cause a breakage of the inner tubular member and/or fel leak. Further, this increased eddy resistance creates cavitation which leads cavitation erosion in the inner wall surface of the inner tubular member, thus resulting in a breakage of the inner tubular member.
Despite this, a fuel injection pipe for diesel engine usable in safety under the above-mentioned severe conditions has not yet been developed for the present.
It is therefore an object of this invention to provide a small thickwalled composite fuel injection tubing, for diesel engines in particular, which is excellent in resistance to cavitation and in proofness against pressure even under severe conditions.
According to a first aspect of this invention, 1 - 5 there is provided a small thick-walled composite metal fuel injection tubing comprising: an outer carbon steel pipe; and an inner stainless steel pipe pressfitted in said large diameter carbon steel pipe by drawing, the press-fitted mating surfaces of said inner and outer pipes being netallurgically and integrally bonded together, at least an inside wall surface of said inner stainless steel pipe having a diffused layer of at least one kind of metal, or an alloy of two or more kinds of metals in combination, said metals being selected from Ni, Cr, Mo, Co, Al and Cu.
According to a second aspect of this invention, there is provided a process of producing a small thick-walled composite metal fuel injection tubing, comprising the steps of: press-fitting an inner stainless steel pipe in an outer carbon steel pipe by drawing, the inner stainless steel pipe having a coating layer of at least one kind of metal, or an alloy of two or more kinds of metals in combination, said metals being selected from Ni, Cr, Mo, Co, Al and Cu; and thereafter heat-treating the resulting press-fitted inner and outer pipes in a furnace in non- oxidizing atmosphere or a vacuum furnace to effect diffusion bonding of the mating surfaces of said.inner and outer pipes to form a diffused layer of said metal or alloy 6 on at least an inner wall surface of said inner pipe.
As a result of the invention one can obtain a small thickwalled metal fuel injection tubing having an outside diameter of at most about 30 mm and having its outer and inner tubular members metallurgically press- fitted on each other, which shows excellent resistance to cavitation, erosion and pressure.
The above and other advantages, features and additional objects of this invention will be manifest to those versed in the art upon making reference to the following detailed description and the accompanying drawings in which a preferred embodiment incorporating the principles of this invention is shown by way of illustrative example.
Fig. 1 is a fragmentary plan view of a small thick-walled fuel injection tubing according to this invention; Fig. 2 is an enlarged view, partially broken away, of Fig.1; and Fig. 3 is a cross-sectional view taken along line A-A of Fig. 2.
The principles of this invention are particularly useful when embodied in a small thick-walled composite fuel injection tubing (hereinafter called "composite injection tubing") such as shown in Figs 1, 2 and 3 generally designated by the numeral 1.
7 - Referring to Figs 2 and 3, the composite injection tubing 1 is a double metal pipe composed of an outer tubular member 11 and an inner tubular member 12 inserted in and through the outer tubular member 11, the inner tubular member 12 having over its inner wall surface a dif fused layer 13. Alternatively, the diffused layer may be disposed over the outer peripheral surface of the inner tubular member 12, namely, at the boundary interface contacting the mating outer and inner tubular members 11, 12.
In this invention, a carbon steel pipe (e.U., aIS G 3455 STS 38 and JIS G3455 STS 42) is used as the outer tubular member 11 particularly for proofness against pressure, while a stainless steel pipe (e.g., JIS 3459 SUS 304TP, SUS 304LTP) is used as the inner tubular member 12 for resistance to cavitation erosion.
The chemical compositions of the above-mentioned carbon steel and stainless steel are shown in Table 1.
TABLE 1 (Chemical Composition of outer and Inner Pipes) Material chemical Composition c si Mn p S Ni Cr STS 38 at most 0.10- 0.30- at most at most 0.25 0.35 1.10 0.035 0.035 SUS304 at most at most at most at most at most 8.00- 18.00 TP 0.08 1.00 2.00 0.04 0.03 11.00 20.00 1, 1 1 1 00 1 t For passage of high pressure fuel in safety, the composite injection tubing 1 in the form of a double metal pipe has preferably an outside diameter of at most 30 mn and preferably a wall thickness of- 25-40% of the outside diameter. The outside diameter and thickness-are easily determined from those widely used in the art, and may be determined each to apredetermined value as desired.
In the 'manufacture of a high pressure fuel injection tubing 1, it is important that any gap should not be created between the outer and inner tubular members and also that any wavy swell or undulations should not be created on the inner wall surface 14 of the inDection tubing, namely, any passage resistance should not be created on the fuel passaqe wall surface to the utmost in view of resistance to cavitation erosion.
From the view point of manufacturing process of the composite injection tubing as a double metal pipe, a gap between the outer and inner tubular members and irregular swells or waves on the inner wall surface 14 of the injection tubing are created when the outer and inner tubular members are press-fitted by drawing to reduce their diameters and particularly when the press-fitted outer and inner tubular members are reformed by reforming rollers after heat-treating (practically, a double metal pipe would be deformed sharply when heat-treated). Keeping the actual condi- tions of such manufacturing process in mind, the present inventors found that it is important to restrict the thickness of the inner.tubular member 12 so as not to create any gap between the outer and inner tubular members and any irregular swells on the inner wall surface of the injection pipe. For the composite injection tubing 1 of this invention, the thickness of a stainless steel pipe as the inner tubular member 12 should be preferably 1.5% - 8.5% of the outside diameter of the entire double metal pipe.
This figure has been determined for the following reason. If the thickness of the inner tubular member 12 exceeds 8.5%, the tendency of creating a large gap between the outer and inner tubular members increases sharply with the plastic deformation toward the axis of the outer tubular member 11 due to the reforming during the press-fitting after the drawing and before diffusion by heat treatment. If the thickness of the inner tubular member 12 does not exceed 1.5%, the tendency of creating irregular or wavy swells on the inner wall surface 14 of the flow passage of the inner tubular member increases sharply due to the roller traces during the reforming.
For the most significant feature of this invention, at least the inner wall surface of the inner 1 - 11 tubular member 12 has a diffused layer of at least one kind of metal, or an alloy of two or more kinds of me±als in combination, selected from Ni, Cr, Mo, Co,.Al and Cu. In addition, the diffused layer may be disposed on the outer wall surface of the inner tubular member 12, i.e., at the mutual boundary interface between the mating outer and inner tubular members 11, 12, in which case the metal or alloy is diffused around the boundary surface between the outer and inner tubular members 11, 12, thus serving to assist in joining the two tubular members together with increased firmness.
For forming a diffused layer of the abovementioned metal or alloy, a coating of the metal or alloy is fornred over the inner wall surface 14 of the inner tubular member 12 beforehand such as by plating, whereupon the outer and inner tubular members 11, 12 are press-fitted and then heattreated. Alternatively, using a stainless hoop or band steel (for forming the inner tubular member) coated beforehand with the above-mentioned metal or alloy by plating or cladding, the inner tubular member is produced, and the inner tubular member is then heat-treated to form a diffused layer of the metal or alloy. The method of forming a diffused layer should by no means be limited to the illustrated examples.
Forming a coating of the above-mentioned metal or alloy over the inner wall surface of the inner tubular member 12 or over both the inner and outer wall surfaces thereof may be accomplished by chemical plating. Further, the thickness of the coating may be usually 1 - 20 pm and should by no means be limited to this figure.
In this invention, the outer and inner tubular members 11, 12 are pressfitted, whereupon the outer and inner tubular members 11, 12 are heattreated in a vacuum furnace, or a furnace in non-oxidizing or reducing atmosphere, as the mating boundary surfaces of the outer and inner tubular members 11, 12 are bonded together metallurgically and integrally. By the heat treatment at that time, the diffusion layer also is formed.
The heat treating conditions in a vacuum furnace, or a furnace in reducing atmosphere, after the above-mentioned press-fitting, may be sufficient if they enable to metallurgically unify the mating boundary surfaces of the outer and inner tubular members; they may be conducted usually at 700 1,2000C for 1 - 30 minutes.
The small thick-walled composite fuel injection tubing of this invention causes the following results:
(i) since a diffused layer of Ni is formed t 1 around the inner wall surface of the inner tubular member, a high- hardness inner wall surface can be obtained so that resistance to cavitation erosion and proofness against pressure.is improved.
(ii) Since the press-fitted mating surfaces of the outer tubular member (carbon steel pipe) and the inner tubular member (stainless steel pipe) are bonded together with increased firmness by diffusion, these two tubular members can hardly be separated during bending and pressing. In general, if a gap is created between the outer and inner tubular members, the inner tubular member will be broken for a short time due to a sudden fluctuation of pressure of high pressure fuel; according to this invention, however, no such gap cannot be created.
(iii) Generally, in the manufacture of this kind of composite fuel injection tubing, wavy and irregular swells are created on the inner wall surface of the inner tubular member due to the shaping force, particularly the shaping pressure applied during the reforming at the final stage of the process, thus lowering resistance to cavitation erosion. With the arrangement of this invention, however, since occurrence of any irregular swell on the inner wall surface of the inner tubular member can be prevented by restricting the thickness of the inner tubular member, it is pos- sible to improve resistance to cavitation erosion and proofness against pressure.
This invention is-now described with.reference to the Examples- but this invention is not limited to these specific Examples. Example 1 A carbon steel pipe of STS 38 (outside diameter of 10 mn, inside diameter of 5 mn) was used as the outer tubular member. A stainless steel pipe of SUS 304 (outside diameter of 5 mm, thickness of 0.5 mm) having on its inner wall surface an Ni-plating layer of 7 pm thickness was used as the inner tubular member.
After having cleaned the outer and inner tubular members, and particularly after having removed pollutants such as oils, carbon scales from the inner circumferential surface of the outer tubular member and the outer circumferential surface of the inner tubular member, the inner tubular member was inserted in and through the outer tubular member. Then, by drawing with a drawing bench, the outer and inner tubular members were mutually fitted to provide a double metal pipe having an outside diameter of 6.35 mm and an inside diameter of 2.0 mm.
Subsequently, the double metal pipe was heat- 1 3 S 1 - is - treated at 1,1000C for 5 minutes in a continuously operating furnace in non-oxidizing atmosphere to join the mating surfaces of the outer and inner tubular members together metallurgically and integrally, and also to form an Ni-rich, excellent-fatigue-strength, high-hardness diffused layer in which an Ni-plating layer was diffused around the inner wall surface of the inner tubular member. The resulting double metal pipe was subjected to desired subsequent processes, such as forming a head for connection. As a result, a high pressure composite fuel injection tubing suitable for a diesel engine was obtained, which tubing was excellent in resistance to cavitation erosion as-well as in proofness against pressure, compared with the conventional tubings. Specifically, in a single-member injection tubing (conventional art) made of annealed STS 38 and having the above-mentioned outside diameter and thickness, a cavitation erosion test was conducted under such an injecting condition that the pressure waveform in the tubing creates cavitation erosion was at most 0.6 mm. As a result, no cavitaion erosion was created at all on the inner wall surface of the single-layer injection tubing. Further, a characteristic of fatigue-proofness with repeated-high-pressure increased to 2.4 times as compared the conventional tubing. In a bending fatigue test regarded as a so- - 16 called 115.8 bending fatigue test" of JA SOM 104 "brake tube test method", vibration-proofness increased by 15%.
Example 2
A double metal pipe was obtained in exactly the same manner as Example 1, except that the stainless pipe as the inner tubular member was manufactured from a stainless hool (band steel). Specifically, the inner tubular member was obtained by forming an Niplating layer of 1 pm thickness and then a Cr-plating layer of 6 pm thickness on the stainless hop, then shaping the-plated stainless hoop into a tube, and finally plugdrawing the tube. Also, the inner tubular member was tried to obtain from a clad band steel having an Ni layer of the same thickness. A high pressure composite fuel injection tubing was obtained from the resulting double metal pipe, which tubing was excellent in resistant to cavitation erosion and in proofness against pressure, like the tubing of Example 1.
11 1 i
Claims (12)
1. A small thick-walled composite metal fuel injection tubing comprising:
(a) an outer carbon steel pipe; and (b) an inner stainless steel pipe press-fitted in said large diameter carbon steel pipe by drawing, the press-fitted mating surfaces of said inner and outer pipes being metallurgically and integrally bonded together, at least an inside wall surface of said inner stainless steel pipe having a diffused layer of at least one kind of metal, or an alloy of two or more kinds of metals in combination, said metals being selected from Ni, Cr, Mo, Co, Al and Cu.
2. A composite metal fuel injection tubing according to claim 1, wherein said composite metal fuel injection tubing has an outside diameter smaller than 30 mn.
3. A composite metal fuel injection tubing according to either of claims 1 and 2 wherein said composite metal fuel injection tubing has a thickness which is 25% to 40% of the outside diameter of said composite metal fuel injection tubing.
4. A composite metal fuel injection tubing according to any one of the preceding claims, wherein said inner stainlesssteel pipe has a thickness which is 1.5% to 8.5% of the out- - 18 side diameter of said composite metal fuel injection tubing.
5. A process f or- producing a small thick-walled composite metal fuel injection tubing, comprising the steps of:
(a) press-fitting an inner stainless steel pipe in an outer carbon steel pipe by drawing. the inner stainless steel pipe having a coating layer of at least one kind of metal, or an alloy of two or more kinds of metals in combination, said metals being selected fror, ni, Cr, Mo, Co, Al and Cu; and (b) thereafter heat treating the resulting pressfitted inner and outer pipes in a furnace in nonoxidizing atmosphere or a vacuum furnace to effect diffusion bonding of the mating surfaces of said inner and outer pipes to form a diffused layer of said metal or alloy on at least an inner wall surface of said inner pipe.
6. A process according to claim 5, wherein said heating treatment in said furnace in non-oxidizing atmosphere or said vacuum furnace is performed at 700 to 1, 2 0 WC.
7. A process according to either of claims 5 and 6 wherein said composite metal fuel injection tubing.has an outside diameter smaller than 30 mm.
8. A process according to any one of claims 5 to 7 wherein said k 1 - 19 composite metal fuel injection tubing has a thickness which is 25% to 40% of the outside diameter of said composite metal fuel injection tubing.
9. A process according to any one of claims 5 to 8, wherein said inner stainless steel pipe has a thickness which is 1.5% to 8.5% of the outside diameter of said composite metal fuel injection tubing.
10. A process for producing a small thick-walled composite metal fuel injection tubing according to claim 5 as hereinbefore described with reference to the Examples.
11. A small thick-walled composite metal fuel injection tubing whenever prepared by the process according to any one of claims 5 to 10.
12. A small thick-walled composite metal fuel injection tubing according to claim 1 substantially as hereinbefore described with reference to the drawings.
Published 1990 at The Patent Ofrice, State House. 6671 High Holbom. London WC1R4TP. Further copies mkvbe obuLinedfr:)rr, The Patent Oflics Sales Branch, St Mary Cray. Orpington. Kent BR5 3RD- Printed by Multiplex techniques ltd. St Mary Cray, Kent. Con. 1187
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1026719A JP2796551B2 (en) | 1989-02-07 | 1989-02-07 | Thick and small-diameter fuel injection pipe and method of manufacturing the same |
Publications (3)
Publication Number | Publication Date |
---|---|
GB9002613D0 GB9002613D0 (en) | 1990-04-04 |
GB2228693A true GB2228693A (en) | 1990-09-05 |
GB2228693B GB2228693B (en) | 1993-03-03 |
Family
ID=12201151
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9002613A Expired - Fee Related GB2228693B (en) | 1989-02-07 | 1990-02-06 | Small thick-walled composite metal tubing and process of producing the same |
Country Status (5)
Country | Link |
---|---|
JP (1) | JP2796551B2 (en) |
KR (1) | KR940011851B1 (en) |
DE (2) | DE9001286U1 (en) |
GB (1) | GB2228693B (en) |
SE (1) | SE502469C2 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2262059A (en) * | 1991-12-02 | 1993-06-09 | Usui Kokusai Sangyo Kk | Manufacturing small diameter pipes |
GB2335018A (en) * | 1998-03-04 | 1999-09-08 | Usui Kokusai Sangyo Kk | Multilayer steel tube |
CN100372621C (en) * | 2006-04-24 | 2008-03-05 | 江苏兴荣高新科技股份有限公司 | Method for manufacturing copper aluminium composite tubing and copper aluminium tubing produced thereby |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4105701A1 (en) * | 1990-03-08 | 1991-09-12 | Mannesmann Ag | METHOD FOR PRODUCING A METAL, THICK-WALLED HIGH-PRESSURE PIPE |
GB2265961B (en) * | 1992-04-09 | 1995-12-20 | Usui Kokusai Sangyo Kk | High pressure fuel injection pipe |
JP3841372B2 (en) * | 1997-02-26 | 2006-11-01 | 臼井国際産業株式会社 | High pressure fuel injection pipe and manufacturing method thereof |
JP2001280218A (en) * | 2000-01-26 | 2001-10-10 | Usui Internatl Ind Co Ltd | Common rail for diesel engine |
WO2002060683A1 (en) * | 2001-01-31 | 2002-08-08 | E.I. Dupont De Nemours And Company | Metallurgically bonded layered article having a curved surface |
DE10023890C2 (en) * | 2000-05-17 | 2002-05-29 | Karl Weinhold | High pressure pipe for water or hydraulic fluid, especially for underground use |
DE10140057B4 (en) * | 2001-08-16 | 2007-08-30 | Robert Bosch Gmbh | High-pressure fuel storage |
JP2006000897A (en) | 2004-06-17 | 2006-01-05 | Usui Kokusai Sangyo Kaisha Ltd | High pressure fuel injection pipe |
JP4640992B2 (en) * | 2006-02-02 | 2011-03-02 | 臼井国際産業株式会社 | Ultra-high pressure fuel pipe and method for manufacturing the same |
DE102007019511B3 (en) * | 2007-04-25 | 2008-11-13 | Benteler Automobiltechnik Gmbh | Device for hydraulic-interior high pressure transformation of composite metal tube into bottom die and upper die, has forming tool, where medium, between individual tube wall, is escaped during interior high pressure reforming process |
DE102007061220A1 (en) | 2007-12-19 | 2008-10-16 | Daimler Ag | Fuel-injected motor vehicle has fuel line comprising inner pipe made of metal and surrounded by fiber-reinforcement |
CN104019289A (en) * | 2014-06-23 | 2014-09-03 | 谢志树 | Composite stainless steel pipe and manufacturing method for same |
KR20190000232A (en) * | 2017-06-22 | 2019-01-02 | 주식회사 협성이엔지 | Leakage checking hole for gas leakage of the underground buried gas-pipelines |
KR101985482B1 (en) * | 2017-12-19 | 2019-06-03 | 주식회사 협성이엔지 | Leakage checking hole for gas leakage of the underground buried gas-pipelines |
KR101985487B1 (en) * | 2017-12-19 | 2019-06-03 | 주식회사 협성이엔지 | Leakage checking hole for gas leakage of the underground buried gas-pipelines |
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GB958267A (en) * | 1961-10-17 | 1964-05-21 | Talbot Stead Tube Company Ltd | Improvements relating to methods of making neutron-absorbing devices |
GB1045427A (en) * | 1964-04-07 | 1966-10-12 | Revere Copper & Brass Inc | Improvements in metallurgically bonded composite metal structures |
GB2085330A (en) * | 1980-10-20 | 1982-04-28 | Sumitomo Metal Ind | Method of preparing clad steels |
GB2180182A (en) * | 1985-07-25 | 1987-03-25 | Usui Kokusai Sangyo Kk | Thick-walled composite metal tubing |
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JPS5662614A (en) * | 1979-10-24 | 1981-05-28 | Usui Internatl Ind Co Ltd | Thick-walled small-diameter superposed metal pipe material |
JPS57152320U (en) * | 1982-02-26 | 1982-09-24 | ||
JPS58177677U (en) * | 1982-05-24 | 1983-11-28 | 臼井国際産業株式会社 | Fuel injection pipe in diesel internal combustion engine |
JPS5952170U (en) * | 1982-09-30 | 1984-04-05 | 株式会社新潟鐵工所 | Structure of fuel oil injection pipe for internal combustion engine |
JPS6037483A (en) * | 1983-08-09 | 1985-02-26 | マルヤス工業株式会社 | High-pressure fuel injecting pipe with surface cured layer |
JPS62184291A (en) * | 1986-09-09 | 1987-08-12 | 臼井国際産業株式会社 | Double metallic pipe |
-
1989
- 1989-02-07 JP JP1026719A patent/JP2796551B2/en not_active Expired - Fee Related
-
1990
- 1990-01-31 SE SE9000339A patent/SE502469C2/en not_active IP Right Cessation
- 1990-02-01 KR KR1019900001196A patent/KR940011851B1/en not_active IP Right Cessation
- 1990-02-05 DE DE9001286U patent/DE9001286U1/en not_active Expired - Lifetime
- 1990-02-05 DE DE4003384A patent/DE4003384C2/en not_active Expired - Fee Related
- 1990-02-06 GB GB9002613A patent/GB2228693B/en not_active Expired - Fee Related
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
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GB958267A (en) * | 1961-10-17 | 1964-05-21 | Talbot Stead Tube Company Ltd | Improvements relating to methods of making neutron-absorbing devices |
GB1045427A (en) * | 1964-04-07 | 1966-10-12 | Revere Copper & Brass Inc | Improvements in metallurgically bonded composite metal structures |
GB2085330A (en) * | 1980-10-20 | 1982-04-28 | Sumitomo Metal Ind | Method of preparing clad steels |
GB2180182A (en) * | 1985-07-25 | 1987-03-25 | Usui Kokusai Sangyo Kk | Thick-walled composite metal tubing |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2262059A (en) * | 1991-12-02 | 1993-06-09 | Usui Kokusai Sangyo Kk | Manufacturing small diameter pipes |
GB2262059B (en) * | 1991-12-02 | 1994-08-17 | Usui Kokusai Sangyo Kk | Method of manufacturing thick-walled small diameter pipe |
GB2335018A (en) * | 1998-03-04 | 1999-09-08 | Usui Kokusai Sangyo Kk | Multilayer steel tube |
GB2335018B (en) * | 1998-03-04 | 2002-11-06 | Usui Kokusai Sangyo Kk | Lapped steel tube |
CN100372621C (en) * | 2006-04-24 | 2008-03-05 | 江苏兴荣高新科技股份有限公司 | Method for manufacturing copper aluminium composite tubing and copper aluminium tubing produced thereby |
Also Published As
Publication number | Publication date |
---|---|
DE9001286U1 (en) | 1990-06-28 |
GB9002613D0 (en) | 1990-04-04 |
KR940011851B1 (en) | 1994-12-27 |
GB2228693B (en) | 1993-03-03 |
DE4003384A1 (en) | 1990-08-09 |
SE502469C2 (en) | 1995-10-23 |
JPH02247085A (en) | 1990-10-02 |
JP2796551B2 (en) | 1998-09-10 |
SE9000339D0 (en) | 1990-01-31 |
DE4003384C2 (en) | 1998-05-20 |
SE9000339L (en) | 1990-08-08 |
KR900012694A (en) | 1990-09-01 |
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Legal Events
Date | Code | Title | Description |
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PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20080206 |