GB641432A - Improved assembling device and applications thereof, in particular to the structuresof aircraft - Google Patents
Improved assembling device and applications thereof, in particular to the structuresof aircraftInfo
- Publication number
- GB641432A GB641432A GB11495/47A GB1149547A GB641432A GB 641432 A GB641432 A GB 641432A GB 11495/47 A GB11495/47 A GB 11495/47A GB 1149547 A GB1149547 A GB 1149547A GB 641432 A GB641432 A GB 641432A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rods
- ribs
- bolts
- diameters
- modification
- 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
- 230000004048 modification Effects 0.000 abstract 3
- 238000012986 modification Methods 0.000 abstract 3
- 230000008878 coupling Effects 0.000 abstract 1
- 238000010168 coupling process Methods 0.000 abstract 1
- 238000005859 coupling reaction Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Geophysics And Detection Of Objects (AREA)
- Bridges Or Land Bridges (AREA)
- Pivots And Pivotal Connections (AREA)
Abstract
641,432. Rod couplings. SOC. NATIONALE DE CONSTRUCTIONS AERONAUTIQUES DU NORD. April 29, 1947, No. 11495. Convention date, Jan. 17. [Class 99(i)] '[Also in Groups XXII and XXXIII] Two members, such as rods 1, 1', Fig. 2, forming the bottom flanges of aircraft spars, are connected together by means of parallel ribs on the contacting faces of the rods, or on jaws 8, 9 between which the ends of the rods are clamped, assembling bolts 12 being passed through holes in the rods, and through the shoes 8, 9 where used, the, diameters of the holes in one of the parts being equal to the diameters of the bolts while, in the other part the diameters are greater than those of the bolts, and the clearance being at least equal to the pitch of the ribs whereby relative adjustment of the members may be effected in two directions or angularly. The ribs may be in zones a, b, c, Fig. 7, the ribs b allowing lateral adjustment and the ribs a, c longitudinal adjustment. In a modification, one rod is made in two parts clamped together by a bolt and formed with eyes to receive a pivot pin. Fig. 11, shows a modification in which two rods 27, 28 are connected by tapered keys 32 driven into coacting keyways in the two parts, assembling bolts 12 being provided as before. In a modification of this form a separate grooved member may be interposed between the two ends of the rods to be joined. The ribs may be semi-circular to provide angular adjustment.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR641432X | 1947-01-17 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB641432A true GB641432A (en) | 1950-08-09 |
Family
ID=8998145
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB11495/47A Expired GB641432A (en) | 1947-01-17 | 1947-04-29 | Improved assembling device and applications thereof, in particular to the structuresof aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB641432A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2920498A (en) * | 1954-03-17 | 1960-01-12 | Schenck Gmbh Carl | Linking device for movable parts |
| US3174781A (en) * | 1962-09-06 | 1965-03-23 | Everett J Eastman | Separable coupling |
| DE3510543A1 (en) * | 1984-03-28 | 1985-10-10 | Composit System S.r.l., Cesano Boscone, Mailand/Milano | NODE CONNECTION FOR NETWORK STRUCTURES |
| US4579475A (en) * | 1984-01-23 | 1986-04-01 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Optimized bolted joint |
| JP2015078551A (en) * | 2013-10-18 | 2015-04-23 | 株式会社コンステック | Joint structure |
| EP3028940A1 (en) * | 2014-12-02 | 2016-06-08 | The Boeing Company | Splice assembly for joining structural components |
-
1947
- 1947-04-29 GB GB11495/47A patent/GB641432A/en not_active Expired
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2920498A (en) * | 1954-03-17 | 1960-01-12 | Schenck Gmbh Carl | Linking device for movable parts |
| US3174781A (en) * | 1962-09-06 | 1965-03-23 | Everett J Eastman | Separable coupling |
| US4579475A (en) * | 1984-01-23 | 1986-04-01 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Optimized bolted joint |
| DE3510543A1 (en) * | 1984-03-28 | 1985-10-10 | Composit System S.r.l., Cesano Boscone, Mailand/Milano | NODE CONNECTION FOR NETWORK STRUCTURES |
| GB2157388A (en) * | 1984-03-28 | 1985-10-23 | Composit System Srl | Space frame nodal joint |
| JP2015078551A (en) * | 2013-10-18 | 2015-04-23 | 株式会社コンステック | Joint structure |
| EP3028940A1 (en) * | 2014-12-02 | 2016-06-08 | The Boeing Company | Splice assembly for joining structural components |
| CN105644766A (en) * | 2014-12-02 | 2016-06-08 | 波音公司 | Splice assembly for joining structural components |
| US9586667B2 (en) | 2014-12-02 | 2017-03-07 | The Boeing Company | Splice assembly for joining structural components |
| EP3388330A1 (en) * | 2014-12-02 | 2018-10-17 | The Boeing Company | Splice assembly for joining structural components |
| CN105644766B (en) * | 2014-12-02 | 2019-12-20 | 波音公司 | Lap assembly for joining structural members |
| CN110844041A (en) * | 2014-12-02 | 2020-02-28 | 波音公司 | Lap assembly for joining structural members |
| EP3659905A1 (en) * | 2014-12-02 | 2020-06-03 | The Boeing Company | Splice assembly for joining structural components |
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