ES178645A1 - IMPROVEMENTS IN AIRCRAFT CONSTRUCTION - Google Patents
IMPROVEMENTS IN AIRCRAFT CONSTRUCTIONInfo
- Publication number
- ES178645A1 ES178645A1 ES0178645A ES178645A ES178645A1 ES 178645 A1 ES178645 A1 ES 178645A1 ES 0178645 A ES0178645 A ES 0178645A ES 178645 A ES178645 A ES 178645A ES 178645 A1 ES178645 A1 ES 178645A1
- Authority
- ES
- Spain
- Prior art keywords
- aircraft construction
- spar
- structures
- construction
- keel structure
- 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 title abstract 2
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
- B64C1/12—Construction or attachment of skin panels
-
- 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
- B64C1/061—Frames
-
- 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
- B64C1/065—Spars
-
- 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)
- Laminated Bodies (AREA)
- Moulding By Coating Moulds (AREA)
- Vibration Dampers (AREA)
Abstract
Perfeccionamiento en la construcción de aviones, que incluyen un fuselaje para avión que comprende, por lo menos, un larguero o estructura de quilla longitudinal inferior y, por lo menos, un larguero o estructura de quilla longitudinal superior, interconectándose las estructuras superior e inferior por medios de costillas situadas en planos perpendiculares a los que contienen los largueros o estructuras de quilla.Improvement in the construction of airplanes, including an aircraft fuselage comprising at least one spar or lower longitudinal keel structure and at least one spar or upper longitudinal keel structure, the upper and lower structures interconnecting by rib means located in planes perpendicular to those containing the stringers or keel structures.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2507/47A GB620863A (en) | 1947-01-27 | 1947-01-27 | Improvements in or relating to aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
ES178645A1 true ES178645A1 (en) | 1947-08-16 |
Family
ID=9740774
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES0178645A Expired ES178645A1 (en) | 1947-01-27 | 1947-06-26 | IMPROVEMENTS IN AIRCRAFT CONSTRUCTION |
Country Status (2)
Country | Link |
---|---|
ES (1) | ES178645A1 (en) |
GB (1) | GB620863A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2398287A1 (en) * | 2010-03-29 | 2013-03-15 | Airbus Operations S.L. | Attachment system of aircraft components |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2827251A (en) * | 1952-04-02 | 1958-03-18 | Doman Helicopters Inc | Aircraft frame with large side openings |
DE102006025930B4 (en) * | 2006-06-02 | 2008-09-11 | Airbus Deutschland Gmbh | Hull structure and method of making a hull structure |
DE102010014638B4 (en) * | 2010-04-12 | 2019-08-01 | Airbus Defence and Space GmbH | Aircraft with an integrated energy absorbing deformation structure and aircraft with such a fuselage |
FR2969119B1 (en) * | 2010-12-17 | 2013-02-08 | Airbus Operations Sas | FRONT PART OF AN AIRCRAFT FUSELAGE INTEGRATING A LANDING TRAIN STORAGE BOX |
CN112027053A (en) * | 2020-09-10 | 2020-12-04 | 中国航空工业集团公司沈阳飞机设计研究所 | Framework structure of frame beam of middle fuselage of airplane |
-
1947
- 1947-01-27 GB GB2507/47A patent/GB620863A/en not_active Expired
- 1947-06-26 ES ES0178645A patent/ES178645A1/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2398287A1 (en) * | 2010-03-29 | 2013-03-15 | Airbus Operations S.L. | Attachment system of aircraft components |
US8960603B2 (en) | 2010-03-29 | 2015-02-24 | Airbus Operations S.L. | Impact resistant and damage tolerant aircraft fuselage |
Also Published As
Publication number | Publication date |
---|---|
GB620863A (en) | 1949-03-31 |
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