GB129673A - Improvements in or relating to Spars for Aircraft. - Google Patents
Improvements in or relating to Spars for Aircraft.Info
- Publication number
- GB129673A GB129673A GB17121/17A GB1712117A GB129673A GB 129673 A GB129673 A GB 129673A GB 17121/17 A GB17121/17 A GB 17121/17A GB 1712117 A GB1712117 A GB 1712117A GB 129673 A GB129673 A GB 129673A
- Authority
- GB
- United Kingdom
- Prior art keywords
- web
- aircraft
- spars
- junctionpiece
- struts
- 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 1
- 238000012986 modification 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
- B64C1/065—Spars
-
- 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
- B64C2001/0063—Fuselage structures substantially made from particular materials from wood
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Plates (AREA)
Abstract
129,673. Highgate Aircraft Co., and Hellers, F. Nov. 20, 1917. Framework.-Spars for aircraft are made up of upper and lower flanges a, b screwed, glued, or otherwise fixed to a web c, the flanges being formed with interrupted grooves e, Fig. 5, for engaging the web, which is formed with recesses g, Fig. 7, corresponding to the interruptions of the grooves e. The web may be in two or more lengths connected by junction-pieces d, Fig. 6, and bolts k. The centre part m of the junctionpiece may support fittings for the attachment of stays or struts. In a modification, the junctionpiece is elongated, its centre portion being formed as a web and its ends serving for attachment of struts &c.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB17121/17A GB129673A (en) | 1917-11-20 | 1917-11-20 | Improvements in or relating to Spars for Aircraft. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB17121/17A GB129673A (en) | 1917-11-20 | 1917-11-20 | Improvements in or relating to Spars for Aircraft. |
Publications (1)
Publication Number | Publication Date |
---|---|
GB129673A true GB129673A (en) | 1919-07-24 |
Family
ID=32347447
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB17121/17A Expired GB129673A (en) | 1917-11-20 | 1917-11-20 | Improvements in or relating to Spars for Aircraft. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB129673A (en) |
-
1917
- 1917-11-20 GB GB17121/17A patent/GB129673A/en not_active Expired
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