ITUB20160979A1 - Complete fuselage protection system for large civil and military aircraft defined in tights - Google Patents
Complete fuselage protection system for large civil and military aircraft defined in tightsInfo
- Publication number
- ITUB20160979A1 ITUB20160979A1 ITUB2016A000979A ITUB20160979A ITUB20160979A1 IT UB20160979 A1 ITUB20160979 A1 IT UB20160979A1 IT UB2016A000979 A ITUB2016A000979 A IT UB2016A000979A IT UB20160979 A ITUB20160979 A IT UB20160979A IT UB20160979 A1 ITUB20160979 A1 IT UB20160979A1
- Authority
- IT
- Italy
- Prior art keywords
- tights
- protection system
- military aircraft
- large civil
- aircraft defined
- Prior art date
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
- B64C1/068—Fuselage sections
- B64C1/069—Joining arrangements therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ITUB2016A000979A ITUB20160979A1 (en) | 2016-02-03 | 2016-02-03 | Complete fuselage protection system for large civil and military aircraft defined in tights |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ITUB2016A000979A ITUB20160979A1 (en) | 2016-02-03 | 2016-02-03 | Complete fuselage protection system for large civil and military aircraft defined in tights |
Publications (1)
Publication Number | Publication Date |
---|---|
ITUB20160979A1 true ITUB20160979A1 (en) | 2017-08-03 |
Family
ID=58670112
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ITUB2016A000979A ITUB20160979A1 (en) | 2016-02-03 | 2016-02-03 | Complete fuselage protection system for large civil and military aircraft defined in tights |
Country Status (1)
Country | Link |
---|---|
IT (1) | ITUB20160979A1 (en) |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB581142A (en) * | 1942-11-18 | 1946-10-02 | Vickers Armstrongs Ltd | Improvements in or connected with pressure cabins for aircraft |
US5031862A (en) * | 1990-01-26 | 1991-07-16 | Rhodes James R | Aircraft with passenger safety net |
US6286785B1 (en) * | 1999-03-11 | 2001-09-11 | Nicholas Donald Kitchen | Reinforcement system for aircraft fuselage frame and aluminum skin |
US20060004499A1 (en) * | 2004-06-30 | 2006-01-05 | Angela Trego | Structural health management architecture using sensor technology |
US20110303791A1 (en) * | 2010-06-11 | 2011-12-15 | Airbus Operations Gmbh | Fuselage Section of an Aircraft and Method for the Production of the Fuselage Section |
-
2016
- 2016-02-03 IT ITUB2016A000979A patent/ITUB20160979A1/en unknown
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB581142A (en) * | 1942-11-18 | 1946-10-02 | Vickers Armstrongs Ltd | Improvements in or connected with pressure cabins for aircraft |
US5031862A (en) * | 1990-01-26 | 1991-07-16 | Rhodes James R | Aircraft with passenger safety net |
US6286785B1 (en) * | 1999-03-11 | 2001-09-11 | Nicholas Donald Kitchen | Reinforcement system for aircraft fuselage frame and aluminum skin |
US20060004499A1 (en) * | 2004-06-30 | 2006-01-05 | Angela Trego | Structural health management architecture using sensor technology |
US20110303791A1 (en) * | 2010-06-11 | 2011-12-15 | Airbus Operations Gmbh | Fuselage Section of an Aircraft and Method for the Production of the Fuselage Section |
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