FR2638708B1 - Perfectionnement a un fuselage - Google Patents
Perfectionnement a un fuselageInfo
- Publication number
- FR2638708B1 FR2638708B1 FR8814714A FR8814714A FR2638708B1 FR 2638708 B1 FR2638708 B1 FR 2638708B1 FR 8814714 A FR8814714 A FR 8814714A FR 8814714 A FR8814714 A FR 8814714A FR 2638708 B1 FR2638708 B1 FR 2638708B1
- Authority
- FR
- France
- Prior art keywords
- fuselage
- improvement
- 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 - Fee Related
Links
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
- B64C1/064—Stringers; Longerons
-
- 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
- B64C1/068—Fuselage sections
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tires In General (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8824723A GB2224000B (en) | 1988-11-10 | 1988-10-21 | Aircraft fuselage or other pressure vessel. |
FR8814714A FR2638708B1 (fr) | 1988-11-10 | 1988-11-10 | Perfectionnement a un fuselage |
DE3900167A DE3900167A1 (de) | 1988-11-10 | 1989-01-05 | Luftfahrzeugrumpf |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8814714A FR2638708B1 (fr) | 1988-11-10 | 1988-11-10 | Perfectionnement a un fuselage |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2638708A1 FR2638708A1 (fr) | 1990-05-11 |
FR2638708B1 true FR2638708B1 (fr) | 1994-05-06 |
Family
ID=9371782
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8814714A Expired - Fee Related FR2638708B1 (fr) | 1988-11-10 | 1988-11-10 | Perfectionnement a un fuselage |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE3900167A1 (fr) |
FR (1) | FR2638708B1 (fr) |
GB (1) | GB2224000B (fr) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2935722B2 (ja) * | 1990-02-28 | 1999-08-16 | 富士重工業株式会社 | 航空機の胴体構造およびその成形方法 |
US5223067A (en) * | 1990-02-28 | 1993-06-29 | Fuji Jukogyo Kabushiki Kaisha | Method of fabricating aircraft fuselage structure |
GB2279930B (en) * | 1993-06-18 | 1997-03-26 | Royal Ordnance Plc | The protection of aircraft structures |
US7527222B2 (en) * | 2004-04-06 | 2009-05-05 | The Boeing Company | Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections |
US7325771B2 (en) | 2004-09-23 | 2008-02-05 | The Boeing Company | Splice joints for composite aircraft fuselages and other structures |
US7503368B2 (en) | 2004-11-24 | 2009-03-17 | The Boeing Company | Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections |
US8388795B2 (en) | 2007-05-17 | 2013-03-05 | The Boeing Company | Nanotube-enhanced interlayers for composite structures |
DE102008012282A1 (de) | 2008-03-03 | 2009-09-17 | Airbus Deutschland Gmbh | Rumpfstruktur für Flugzeug |
DE102010018932B4 (de) * | 2010-04-30 | 2013-06-13 | Airbus Operations Gmbh | Umfangsversteifung für einen Luftfahrzeugrumpf |
US10745104B2 (en) * | 2018-03-02 | 2020-08-18 | The Boeing Company | Stringer transition through a common base charge |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR845332A (fr) * | 1938-10-28 | 1939-08-18 | Henschel Flugzeugwerke Ag | Dispositif pour le raidissage de tôles lisses |
GB534810A (en) * | 1940-02-26 | 1941-03-19 | David Henderson Sandilands | Stressed skin panels |
GB555496A (en) * | 1942-02-20 | 1943-08-25 | Henry Kremer | Improvements in or relating to structures built up of plywood or other light-weight laminated material |
GB559954A (en) * | 1942-09-07 | 1944-03-13 | Vultee Aircraft Inc | Airplane structures |
-
1988
- 1988-10-21 GB GB8824723A patent/GB2224000B/en not_active Expired - Lifetime
- 1988-11-10 FR FR8814714A patent/FR2638708B1/fr not_active Expired - Fee Related
-
1989
- 1989-01-05 DE DE3900167A patent/DE3900167A1/de not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
FR2638708A1 (fr) | 1990-05-11 |
GB2224000B (en) | 1992-05-27 |
GB8824723D0 (en) | 1988-11-30 |
DE3900167A1 (de) | 1990-07-12 |
GB2224000A (en) | 1990-04-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |