FR868568A - composite construction elements, working in bending for airplanes, etc., in particular side members or beams - Google Patents
composite construction elements, working in bending for airplanes, etc., in particular side members or beamsInfo
- Publication number
- FR868568A FR868568A FR868568DA FR868568A FR 868568 A FR868568 A FR 868568A FR 868568D A FR868568D A FR 868568DA FR 868568 A FR868568 A FR 868568A
- Authority
- FR
- France
- Prior art keywords
- airplanes
- beams
- bending
- working
- side members
- 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
- 238000005452 bending Methods 0.000 title 1
- 239000002131 composite material Substances 0.000 title 1
- 238000010276 construction Methods 0.000 title 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
- 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
- B64C1/065—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
- B64C2001/0063—Fuselage structures substantially made from particular materials from wood
-
- 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)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR868568T | 1940-03-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
FR868568A true FR868568A (en) | 1942-01-07 |
Family
ID=9346199
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR868568D Expired FR868568A (en) | 1940-03-21 | 1940-03-21 | composite construction elements, working in bending for airplanes, etc., in particular side members or beams |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR868568A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10220935B2 (en) * | 2016-09-13 | 2019-03-05 | The Boeing Company | Open-channel stiffener |
-
1940
- 1940-03-21 FR FR868568D patent/FR868568A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10220935B2 (en) * | 2016-09-13 | 2019-03-05 | The Boeing Company | Open-channel stiffener |
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