GB357099A - Improvements in aircraft - Google Patents
Improvements in aircraftInfo
- Publication number
- GB357099A GB357099A GB7323/30A GB732330A GB357099A GB 357099 A GB357099 A GB 357099A GB 7323/30 A GB7323/30 A GB 7323/30A GB 732330 A GB732330 A GB 732330A GB 357099 A GB357099 A GB 357099A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- augsburg
- longerons
- germany
- march
- 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
- 239000011800 void material Substances 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
-
- 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)
- Tires In General (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Transmission Devices (AREA)
Abstract
357,099. Aircraft wings. MESSER. SCHMITT, W., 118A, Haunstetterstrasse, Augsburg, Germany.-(Assignees of Bayerische Flugzeugwerke Akt.-Ges. ; Augsburg, Germany.) March 6, 1930, No. 7323. Convention date, March 7, 1929. Void [Published under Sect. 91 of the Acts]. [Class 4.] The continuous main spar or spars of a wing are arranged to pass directly over or under the aeroplane fuselage and are connected. to an outer longeron in such a manner that the strain is directly transmitted from one to the other. Fig. 5 shows a wing mounted directly on a fuselage by means of connections A, B to transverse frames S. The wing is also connected at points B to longerons R disposed tangentially to the upper side of wing spar H. According to a modification, Fig. 6, the wing is connected at points A, C, so that the connections at B only transmit the strain in the longerons R. The Specification does not permit of satisfactory abridgment.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE357099X | 1929-03-07 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB357099A true GB357099A (en) | 1931-09-14 |
Family
ID=6290476
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB7323/30A Expired GB357099A (en) | 1929-03-07 | 1930-03-06 | Improvements in aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB357099A (en) |
-
1930
- 1930-03-06 GB GB7323/30A patent/GB357099A/en not_active Expired
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