GB306410A - Improvements in and relating to flying machines - Google Patents
Improvements in and relating to flying machinesInfo
- Publication number
- GB306410A GB306410A GB5411/29A GB541129A GB306410A GB 306410 A GB306410 A GB 306410A GB 5411/29 A GB5411/29 A GB 5411/29A GB 541129 A GB541129 A GB 541129A GB 306410 A GB306410 A GB 306410A
- Authority
- GB
- United Kingdom
- Prior art keywords
- spaces
- wings
- protective
- fuselages
- machine
- 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
- 230000001681 protective effect Effects 0.000 abstract 5
- 238000010276 construction Methods 0.000 abstract 2
- 230000035939 shock Effects 0.000 abstract 2
- 230000015572 biosynthetic process Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
306,410. Junkers, H. Feb. 17, 1928, [Convention date]. Aeroplanes ; planes, construction of ; cars and cabins.-In a flying machine of the type having hollow wings arranged to accommodate passengers and loads, additional hollow spaces are provided which extend downwardly beneath the wings in such a manner that they are the first portions of the machine to come into contact with the ground in the event of undercarriage breakage thus absorbing the shock and affording protection to the loads carried in the wings ; these spaces are utilized to carry the less valuable inert loads. These protective spaces may extend beyond the leading edge of the wings to take the shock of the machine pitching on its nose. In the construction shown the fuselage is formed with downwardly extending hollow spaces 7 which form the protective space desired; these spaces are continued forwardly to form a nose 8. Further protective spaces are arranged on the leading edge of the wings and serve as housings for the propellers. In the case of a double fuselage machine both fuselages are designed in this manner whilst when there are more than two fuselages all or only some are employed for the formation of protective spaces. Similar spaces may be provided between the leading and trailing edges of the wings to serve as protection ir the event of failure of one side of the undercarriage only. These last-mentioned spaces only are provided on flying machines having no fuselage; in machines with fuselages the fuselages may then also be designed as protective spaces or not.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE306410X | 1928-02-17 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB306410A true GB306410A (en) | 1929-11-07 |
Family
ID=6121103
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5411/29A Expired GB306410A (en) | 1928-02-17 | 1929-02-18 | Improvements in and relating to flying machines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB306410A (en) |
-
1929
- 1929-02-18 GB GB5411/29A patent/GB306410A/en not_active Expired
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