GB946762A - Improvements in aircraft - Google Patents
Improvements in aircraftInfo
- Publication number
- GB946762A GB946762A GB2601/60A GB260160A GB946762A GB 946762 A GB946762 A GB 946762A GB 2601/60 A GB2601/60 A GB 2601/60A GB 260160 A GB260160 A GB 260160A GB 946762 A GB946762 A GB 946762A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- cabin
- jan
- roof
- floor
- 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
- 238000010276 construction Methods 0.000 abstract 1
- 239000007787 solid 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
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Body Structure For Vehicles (AREA)
Abstract
946,762. Aircraft construction. MINISTER OF AVIATION. Jan. 19, 1961 [Jan 25, 1960], No. 2601/60. Heading B7W. The roof and floor of a pressurized cabin A, B, B<SP>1</SP> of an aircraft 10, comprise skins 14, 15, 14a, 15a filled with square section tubes 16, 16a, the skins 14, 15a forming part of the aircraft skin; the tubes 16, 16a may be replaced by a corrugated filling, Fig. 2a, not shown. The cabin side walls are thin sheets of circular arc section. Equispaced ribs cd, ef, gh, &c. secured to the roof and floor and comprising a solid web 18 and an open mesh structure 17 divide the cabin into sections; corridors a, a<SP>1</SP>, b, b<SP>1</SP> and B, B<SP>1</SP> are also provided. Regions W and B, B<SP>1</SP>, F, F<SP>1</SP> of the aircraft constitute storage compartments.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2601/60A GB946762A (en) | 1960-01-25 | 1960-01-25 | Improvements in aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2601/60A GB946762A (en) | 1960-01-25 | 1960-01-25 | Improvements in aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB946762A true GB946762A (en) | 1964-01-15 |
Family
ID=9742445
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2601/60A Expired GB946762A (en) | 1960-01-25 | 1960-01-25 | Improvements in aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB946762A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2646494A1 (en) * | 1989-04-26 | 1990-11-02 | Atomic Energy Authority Uk | LIGHT MATERIAL FOR AEROSPATIAL STRUCTURES |
GB2428417A (en) * | 2005-10-27 | 2007-01-31 | Hal Errikos Calamvokis | Aircraft fuselage structure |
EP3018051A1 (en) * | 2014-11-06 | 2016-05-11 | Airbus Operations GmbH | Structural component and method for producing a structural component |
CN113353237A (en) * | 2020-03-02 | 2021-09-07 | 中航西飞民用飞机有限责任公司 | Method for disposing dangerous goods on airplane and disposal cabin structure |
-
1960
- 1960-01-25 GB GB2601/60A patent/GB946762A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2646494A1 (en) * | 1989-04-26 | 1990-11-02 | Atomic Energy Authority Uk | LIGHT MATERIAL FOR AEROSPATIAL STRUCTURES |
GB2428417A (en) * | 2005-10-27 | 2007-01-31 | Hal Errikos Calamvokis | Aircraft fuselage structure |
GB2428417B (en) * | 2005-10-27 | 2007-09-12 | Hal Errikos Calamvokis | Aircraft fuselage structure |
EP3018051A1 (en) * | 2014-11-06 | 2016-05-11 | Airbus Operations GmbH | Structural component and method for producing a structural component |
CN105584618A (en) * | 2014-11-06 | 2016-05-18 | 空中客车运营有限公司 | Structural Component And Method For Producing A Structural Component |
US9988136B2 (en) | 2014-11-06 | 2018-06-05 | Airbus Operations Gmbh | Structural component and method for producing a structural component |
CN113353237A (en) * | 2020-03-02 | 2021-09-07 | 中航西飞民用飞机有限责任公司 | Method for disposing dangerous goods on airplane and disposal cabin structure |
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