GB153021A - Improvements in machines for bolting up and tightening plates and the like - Google Patents
Improvements in machines for bolting up and tightening plates and the likeInfo
- Publication number
- GB153021A GB153021A GB30286/20A GB3028620A GB153021A GB 153021 A GB153021 A GB 153021A GB 30286/20 A GB30286/20 A GB 30286/20A GB 3028620 A GB3028620 A GB 3028620A GB 153021 A GB153021 A GB 153021A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rod
- piston
- stem
- screwed
- plates
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25B—TOOLS OR BENCH DEVICES NOT OTHERWISE PROVIDED FOR, FOR FASTENING, CONNECTING, DISENGAGING OR HOLDING
- B25B31/00—Hand tools for applying fasteners
- B25B31/005—Hand tools for applying fasteners for temporarily connecting sheets before or during assembly operations
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Clamps And Clips (AREA)
Abstract
153,021. McBride, J. P. Aug. 20, 1919, [Convention date]. Clamps.-In an apparatus for tightening and bolting up plates or like members, prior to riveting, the clamping stem is carried by the rod of an hydraulic piston which has an extension rod on its other side passing through the cylinder head and provided with means tu hold the piston in a position partly or completely pumped up. The piston-rod 6 which is screwed to the piston 3 passes through a gland 7 into a housing 8 and has screwed to its end a pulling stem 9 which, in order to permit of angularity between the stem and plates, passes through a spherical washer 15 mounted in the end of the housing, through the plates 13, 14 and through a concaved washer 17 supported by a spherical washer 16 screwed to the stem. An extension piston-rod 18 of the same diameter as the rod 6 is used so as to maintain a constant volume of fluid in the cylinder. The end of this rod 18 passes through the cylinder head and is fitted with a nut 19 for holding the piston in position, thus preventing backward movement due to leakage, or it may be used to pull the stem positively outwards and hold it in position. A pump plunger 21, Fig. 4, operated by a hand-lever 22 slides in a casing 20 screwed to the cylinder head and operates in connexion with a direct pressure spring valve 25, a similar back pressure valve, and a hand adjusted plug valve 28, which may be set so that pressure may be supplied either to the top or bottom of the cylinder. Specification 155,206 is referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US153021XA | 1919-08-20 | 1919-08-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB153021A true GB153021A (en) | 1922-01-26 |
Family
ID=21770647
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB30286/20A Expired GB153021A (en) | 1919-08-20 | 1920-10-26 | Improvements in machines for bolting up and tightening plates and the like |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB153021A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2919691A1 (en) * | 2007-08-03 | 2009-02-06 | Lisi Aerospace Soc Par Actions | Anchoring screw fastener for temporary fixation of drilling grid on wings of airplane, has assembly of rod and half clamps in form of circle, whose diameter is identical to internal diameter of orifices for longitudinal sliding of assembly |
-
1920
- 1920-10-26 GB GB30286/20A patent/GB153021A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2919691A1 (en) * | 2007-08-03 | 2009-02-06 | Lisi Aerospace Soc Par Actions | Anchoring screw fastener for temporary fixation of drilling grid on wings of airplane, has assembly of rod and half clamps in form of circle, whose diameter is identical to internal diameter of orifices for longitudinal sliding of assembly |
WO2009047405A2 (en) * | 2007-08-03 | 2009-04-16 | Lisi Aerospace | Riveting screw tack and use thereof for temporarily fixing a boring grid to elements to be assembled |
WO2009047405A3 (en) * | 2007-08-03 | 2009-07-30 | Lisi Aerospace | Riveting screw tack and use thereof for temporarily fixing a boring grid to elements to be assembled |
US8448929B2 (en) | 2007-08-03 | 2013-05-28 | Lisi Aerospace | Riveting screw tack and use thereof for temporarily fixing a boring grid to elements to be assembled |
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