GB590511A - Improvements in or relating to aircraft and other hollow bodies - Google Patents
Improvements in or relating to aircraft and other hollow bodiesInfo
- Publication number
- GB590511A GB590511A GB20069/44A GB2006944A GB590511A GB 590511 A GB590511 A GB 590511A GB 20069/44 A GB20069/44 A GB 20069/44A GB 2006944 A GB2006944 A GB 2006944A GB 590511 A GB590511 A GB 590511A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- attachments
- openings
- wing
- side walls
- 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
- 230000002787 reinforcement Effects 0.000 abstract 2
- 230000003014 reinforcing effect Effects 0.000 abstract 2
- 239000000945 filler 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
-
- 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)
Abstract
590,511. Aircraft. BUDD MANUFACTURING CO., E. G. Oct. 17, 1944, No. 20069. Convention date, June 23, 1943. [Class 4] In a hollow body, such as the body 20 of an aircraft shown in Fig. 1 and particularly one with side wall openings 31 giving access to the body cargo space, members, such as the wings 19, span the openings and provide reinforcement to the side walls, which are liable on landing of the aircraft to bulge at the curved parts of the side walls as shown at f in Fig. 3. The primary wing attachments through spars 39, 40 shown in plan, Fig. 4, are constructed in the manner described in Specification 590,510, these attachments being forward of the openings 31 ; the lighter secondary attachments for the trailing wing portions span the door openings 31 to serve as external reinforcements, The wing 19, Fig. 8, with reinforced upper and lower skins 38 is connected by the reinforcing stringers 42 to the curved wall members 35, the skins 38 being connected by filler sections 47<1> to the body skin 33. The two sets of attachments are indicated by shading in Fig. 4 to show the C-shaped reinforcing member formed by them.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US590511XA | 1943-06-23 | 1943-06-23 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB590511A true GB590511A (en) | 1947-07-21 |
Family
ID=22020513
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB20069/44A Expired GB590511A (en) | 1943-06-23 | 1944-10-17 | Improvements in or relating to aircraft and other hollow bodies |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB590511A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2009003870A2 (en) * | 2007-06-29 | 2009-01-08 | Airbus Operations Gmbh | Structural component with rib and cross member element |
CN104015916A (en) * | 2014-06-13 | 2014-09-03 | 韩世宇 | Unmanned plane |
-
1944
- 1944-10-17 GB GB20069/44A patent/GB590511A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2009003870A2 (en) * | 2007-06-29 | 2009-01-08 | Airbus Operations Gmbh | Structural component with rib and cross member element |
WO2009003870A3 (en) * | 2007-06-29 | 2009-03-12 | Airbus Gmbh | Structural component with rib and cross member element |
US8439307B2 (en) | 2007-06-29 | 2013-05-14 | Airbus Operations Gmbh | Structural component with rib and cross member element |
CN104015916A (en) * | 2014-06-13 | 2014-09-03 | 韩世宇 | Unmanned plane |
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