GB127402A - Improvements in and relating to Aeroplanes. - Google Patents
Improvements in and relating to Aeroplanes.Info
- Publication number
- GB127402A GB127402A GB8888/18A GB888818A GB127402A GB 127402 A GB127402 A GB 127402A GB 8888/18 A GB8888/18 A GB 8888/18A GB 888818 A GB888818 A GB 888818A GB 127402 A GB127402 A GB 127402A
- Authority
- GB
- United Kingdom
- Prior art keywords
- planes
- spars
- fuselage
- christmas
- bracing
- 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
- B64C39/00—Aircraft not otherwise provided for
- B64C39/08—Aircraft not otherwise provided for having multiple wings
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Rod-Shaped Construction Members (AREA)
Abstract
127,402. Christmas, W. W., and Christmas Aeroplane Co. May 29, 1918. Planes, construction and arrangement of.-The lower planes of a biplane are made only “ to ¢ the area of the upper planes, the trailing edges of the upper and lower planes being in vertical alinement. The construction of the planes is such as to render interplane struts and bracing unnecessary. Figs. 1 and 4 show upper catahedral planes 25 and lower dihedral planes 26 detachably mounted on the fuselage by passing the spars 29 through brackets 31, Fig. 9, on, or grooves in, the longerons 2, the inner ends of the spars being connected bv sleeves 32. The spars are secured in the brackets 31 and sleeves 32 by means of pins 33 locked by catches 35. The upper plane is arranged below the line of vision of the pilot. The spars 29 comprise steel bars or strips arranged edgewise, and they are connected by bracing 30. Cars and cabins.-The upper surface of the fuselage is made to conform to the curvature of the crest of the upper plane. Framework.-The fuselage framework may be composed of metal tubing of rectangular crosssection jointed by welding.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8888/18A GB127402A (en) | 1918-05-29 | 1918-05-29 | Improvements in and relating to Aeroplanes. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8888/18A GB127402A (en) | 1918-05-29 | 1918-05-29 | Improvements in and relating to Aeroplanes. |
Publications (1)
Publication Number | Publication Date |
---|---|
GB127402A true GB127402A (en) | 1919-05-29 |
Family
ID=32343528
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8888/18A Expired GB127402A (en) | 1918-05-29 | 1918-05-29 | Improvements in and relating to Aeroplanes. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB127402A (en) |
-
1918
- 1918-05-29 GB GB8888/18A patent/GB127402A/en not_active Expired
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