GB394289A - Improvements in and relating to the manufacture of forcetransmitting constructional parts for aircraft more particularly for aeroplanes - Google Patents
Improvements in and relating to the manufacture of forcetransmitting constructional parts for aircraft more particularly for aeroplanesInfo
- Publication number
- GB394289A GB394289A GB561333A GB561333A GB394289A GB 394289 A GB394289 A GB 394289A GB 561333 A GB561333 A GB 561333A GB 561333 A GB561333 A GB 561333A GB 394289 A GB394289 A GB 394289A
- Authority
- GB
- United Kingdom
- Prior art keywords
- soldered
- thin
- ribs
- edges
- spar
- 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
- 238000004519 manufacturing process Methods 0.000 title 1
- 229910052751 metal Inorganic materials 0.000 abstract 2
- 238000005476 soldering Methods 0.000 abstract 2
- 229910000906 Bronze Inorganic materials 0.000 abstract 1
- 229910000831 Steel Inorganic materials 0.000 abstract 1
- 239000010974 bronze Substances 0.000 abstract 1
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 abstract 1
- 239000000463 material Substances 0.000 abstract 1
- 239000002184 metal Substances 0.000 abstract 1
- 229910000679 solder Inorganic materials 0.000 abstract 1
- 239000010959 steel Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
-
- 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
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
Abstract
394,289. Soldering. SHEVLIN, J. T., 15, South Street, London.-(Sambraus, A.; 57, Bismarck-Strasse, Charlottenburg, Berlin.) Feb. 23, 1933, No. 5613. [Classes 83 (ii) and 83 (iv).] Aircraft parts comprising thin tough metal elements such as highly alloyed steel or bronze are secured together by soft soldered joints, and where a number of parts have to be secured together successively the later operations are effected with solders of successively lower melting-points. Fig. 3 shows a joint between the front spar, ribs and skin of an aeroplane wing, the spar comprising a thin metal web 9 and flanges 7 connected together by angle strips 8 soldered to both elements. Holes 15 may be formed in the strips 8 for the introduction of soldering material. The web is strengthened at intervals by profiled pieces 10 soldered on. The skin 11, 11<1> is lap jointed and connected to a plate 14 and is strengthened by ribs 12, 12<1>. Gusset plates 13, 13<1> connect the spar and ribs and the edges of the gusset plates have thin flanges 17 soldered on. To secure flexibility at joints in thin sheets the edges are toothed and tapered in thickness. When a sheet is to remain in tension it is heated by rollers prior to having its edges soldered.. Very thin sheets may be temporarily supported by cementing them to cardboard.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB561333A GB394289A (en) | 1933-02-23 | 1933-02-23 | Improvements in and relating to the manufacture of forcetransmitting constructional parts for aircraft more particularly for aeroplanes |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB561333A GB394289A (en) | 1933-02-23 | 1933-02-23 | Improvements in and relating to the manufacture of forcetransmitting constructional parts for aircraft more particularly for aeroplanes |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB394289A true GB394289A (en) | 1933-06-22 |
Family
ID=9799380
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB561333A Expired GB394289A (en) | 1933-02-23 | 1933-02-23 | Improvements in and relating to the manufacture of forcetransmitting constructional parts for aircraft more particularly for aeroplanes |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB394289A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2157248A (en) * | 1984-04-13 | 1985-10-23 | Metal Fax Ltd | A beam structure |
| CN1990149B (en) * | 2005-12-30 | 2010-10-27 | 航天材料及工艺研究所 | Welding method of titanium alloy skeleton and skin with variable cross-section |
| CN103318402A (en) * | 2012-03-22 | 2013-09-25 | 空中客车运营有限公司 | Seal assembly for an aircraft wing |
| EP2316726A3 (en) * | 2009-10-27 | 2016-01-13 | Airbus Operations Limited | Cover trailing edge profile |
| CN109677586A (en) * | 2019-01-18 | 2019-04-26 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | A kind of web, aircraft wing and aircraft |
-
1933
- 1933-02-23 GB GB561333A patent/GB394289A/en not_active Expired
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2157248A (en) * | 1984-04-13 | 1985-10-23 | Metal Fax Ltd | A beam structure |
| CN1990149B (en) * | 2005-12-30 | 2010-10-27 | 航天材料及工艺研究所 | Welding method of titanium alloy skeleton and skin with variable cross-section |
| EP2316726A3 (en) * | 2009-10-27 | 2016-01-13 | Airbus Operations Limited | Cover trailing edge profile |
| CN103318402A (en) * | 2012-03-22 | 2013-09-25 | 空中客车运营有限公司 | Seal assembly for an aircraft wing |
| EP2641830A3 (en) * | 2012-03-22 | 2015-06-03 | Airbus Operations Limited | Seal assembly for an aircraft wing |
| CN109677586A (en) * | 2019-01-18 | 2019-04-26 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | A kind of web, aircraft wing and aircraft |
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