GB116984A - Improvements in Attachment Devices for Tension Members, Wires or Stays, particularly applicable to Aircraft. - Google Patents
Improvements in Attachment Devices for Tension Members, Wires or Stays, particularly applicable to Aircraft.Info
- Publication number
- GB116984A GB116984A GB13301/17A GB1330117A GB116984A GB 116984 A GB116984 A GB 116984A GB 13301/17 A GB13301/17 A GB 13301/17A GB 1330117 A GB1330117 A GB 1330117A GB 116984 A GB116984 A GB 116984A
- Authority
- GB
- United Kingdom
- Prior art keywords
- trunnion
- slots
- aircraft
- wires
- stays
- 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
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Insertion, Bundling And Securing Of Wires For Electric Apparatuses (AREA)
Abstract
116,984. Blackburn Aeroplane & Motor Co., and Copley. J. W. Sept. 17, 1917. Framework.-Adevice for the attachment of bracing-wires, particularly in aircraft, comprises a sheet-metal blank bent to form two approximately parallel limbs 1, 2 in which slots 5, 6 are formed to take a trunnion 7 to which the bracing-wire is secured, preferably by screwing through a hole at right-angles to the axis of the trunnion. The trunnion has grooves 8, 9 engaging the outer ends of the slots to prevent splaying of the limbs 1, 2 and to prevent axial movement of the trunnion which is introduced through enlarged portions of the slots near the bent portion 3 and slid into position. The bent portion 3 may be made cylindrical and placed astride a pin 4 on the structure as shown in Fig. 8, or it may be flat and secured by bolts. More than one pair of slots may be made in a single bent plate to take additional trunnions.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB13301/17A GB116984A (en) | 1917-09-17 | 1917-09-17 | Improvements in Attachment Devices for Tension Members, Wires or Stays, particularly applicable to Aircraft. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB13301/17A GB116984A (en) | 1917-09-17 | 1917-09-17 | Improvements in Attachment Devices for Tension Members, Wires or Stays, particularly applicable to Aircraft. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB116984A true GB116984A (en) | 1918-07-04 |
Family
ID=32671861
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB13301/17A Expired GB116984A (en) | 1917-09-17 | 1917-09-17 | Improvements in Attachment Devices for Tension Members, Wires or Stays, particularly applicable to Aircraft. |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB116984A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102483087A (en) * | 2009-03-03 | 2012-05-30 | 哈特马特.弗莱格 | Safety screw, screw connection and method for producing safety screw |
-
1917
- 1917-09-17 GB GB13301/17A patent/GB116984A/en not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102483087A (en) * | 2009-03-03 | 2012-05-30 | 哈特马特.弗莱格 | Safety screw, screw connection and method for producing safety screw |
| EP2511542A1 (en) | 2009-03-03 | 2012-10-17 | Flaig, Hartmut | Safety screw, screw connection and method for producing a safety screw |
| EP2628965A1 (en) | 2009-03-03 | 2013-08-21 | Flaig, Hartmut | Retaining screw, screw connection and method for producing a retaining screw |
| CN102483087B (en) * | 2009-03-03 | 2014-05-28 | 哈特马特.弗莱格 | Safety screw, screw connection and method for producing safety screw |
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