GB625005A - Improvements in or relating to pipe joints or couplings - Google Patents
Improvements in or relating to pipe joints or couplingsInfo
- Publication number
- GB625005A GB625005A GB755843A GB755843A GB625005A GB 625005 A GB625005 A GB 625005A GB 755843 A GB755843 A GB 755843A GB 755843 A GB755843 A GB 755843A GB 625005 A GB625005 A GB 625005A
- Authority
- GB
- United Kingdom
- Prior art keywords
- members
- pipe
- flange
- gripped
- slidable
- 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.)
- Expired
Links
Classifications
-
- 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
- F16L27/00—Adjustable joints, Joints allowing movement
- F16L27/10—Adjustable joints, Joints allowing movement comprising a flexible connection only, e.g. for damping vibrations
- F16L27/1004—Adjustable joints, Joints allowing movement comprising a flexible connection only, e.g. for damping vibrations introduced in exhaust pipes for hot gases
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Exhaust Silencers (AREA)
- Quick-Acting Or Multi-Walled Pipe Joints (AREA)
Abstract
625,005. Pipe couplings. TICKNER, A., (Mercier, P. E.). May 12, 1943, No. 7558. [Class 99(i)] A pipe 1, Fig. 1, for exhaust gases &c. is coupled to another member in a line by a collar 2 flared outwardly to form an arcuate annulus resiliently gripped between a pair of arcuate metallic members 3, 4, at least one of the members and/or the annulus having different arcuate curvatures and at least the outer of the members 3, 4 terminating in a flange 8 secured to the other member in the line. In Fig. 1, the member 4 has a flange 9, a flanged ring 5 is interposed between the flanges 8, 9 and a plate 6 drilled for bolts whereby the pipe 1 is coupled to a pipe 7 and the three flanges are connected by spot welding. In Fig. 3, pipes 11, 11a have collars gripped between a single inner member 14 and two outer members 13, 13a spot welded at 16. In Fig. 5, the joint assembly is slidable, a collar 12 having an extension slidable between extensions on a flange 21 and on a plate 6. The joint itself is a modification of that of Fig. 3, the member 14 being replaced by a member 19 recessed at 20 and having a rim 19a gripped between the members 13, 13a. In Fig. 6, (not shown), an exhaust manifold is connected to a three-cylinder head by a central rigid joint and two slidable joints as shown in Fig. 5.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB755843A GB625005A (en) | 1943-05-12 | 1943-05-12 | Improvements in or relating to pipe joints or couplings |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB755843A GB625005A (en) | 1943-05-12 | 1943-05-12 | Improvements in or relating to pipe joints or couplings |
Publications (1)
Publication Number | Publication Date |
---|---|
GB625005A true GB625005A (en) | 1949-06-21 |
Family
ID=9835421
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB755843A Expired GB625005A (en) | 1943-05-12 | 1943-05-12 | Improvements in or relating to pipe joints or couplings |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB625005A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3302885A (en) * | 1962-06-22 | 1967-02-07 | Lockheed Aircraft Corp | Swinveled rocket motor nozzle |
-
1943
- 1943-05-12 GB GB755843A patent/GB625005A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3302885A (en) * | 1962-06-22 | 1967-02-07 | Lockheed Aircraft Corp | Swinveled rocket motor nozzle |
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