GB396025A - Improvements in airplane fusilages - Google Patents
Improvements in airplane fusilagesInfo
- Publication number
- GB396025A GB396025A GB29104/31A GB2910431A GB396025A GB 396025 A GB396025 A GB 396025A GB 29104/31 A GB29104/31 A GB 29104/31A GB 2910431 A GB2910431 A GB 2910431A GB 396025 A GB396025 A GB 396025A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuselage
- aeroplane
- bifurcated
- fusilages
- airplane
- 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
- NIOPZPCMRQGZCE-WEVVVXLNSA-N 2,4-dinitro-6-(octan-2-yl)phenyl (E)-but-2-enoate Chemical compound CCCCCCC(C)C1=CC([N+]([O-])=O)=CC([N+]([O-])=O)=C1OC(=O)\C=C\C NIOPZPCMRQGZCE-WEVVVXLNSA-N 0.000 abstract 1
- 239000011800 void material Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWERÂ PLANTSÂ OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D7/00—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
- B64D7/02—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft the armaments being firearms
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
Abstract
396,025. Aeroplane fuselages fitted with guns. RUMBOWICZ, W., Mokotow Lotnisko, Warsaw. Oct. 20, 1931, No. 29104. Convention date, March 11. Void [Published under Sect. 91 of the Acts]. [Class 4.] To enable a gun to be fired rearwards and downwards as well as upwards and to both sides, the fuselage of an aeroplane is bifurcated immediately behind the gunner's station, the rudder planes being mounted on the bifurcated part. The two bifurcations a are formed integral with or separately secured to the main part b of the fuselage.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PL396025X | 1931-03-11 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB396025A true GB396025A (en) | 1933-07-27 |
Family
ID=19936310
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB29104/31A Expired GB396025A (en) | 1931-03-11 | 1931-10-20 | Improvements in airplane fusilages |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB396025A (en) |
-
1931
- 1931-10-20 GB GB29104/31A patent/GB396025A/en not_active Expired
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