GB210591A - Improvements in girders and the like of box-like or similar section for use upon aircraft - Google Patents
Improvements in girders and the like of box-like or similar section for use upon aircraftInfo
- Publication number
- GB210591A GB210591A GB34567/22A GB3456722A GB210591A GB 210591 A GB210591 A GB 210591A GB 34567/22 A GB34567/22 A GB 34567/22A GB 3456722 A GB3456722 A GB 3456722A GB 210591 A GB210591 A GB 210591A
- Authority
- GB
- United Kingdom
- Prior art keywords
- girder
- stays
- tubes
- attachment
- girders
- 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
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
- B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Body Structure For Vehicles (AREA)
Abstract
210,591. Armstrong Siddeley Motors, Ltd., and Lloyd, J. Dec. 19, 1922. Framework.-A longitudinally-grooved hollow girder is stiffened for attachment of stays, hinges, cross-members, and other fittings by tubular distance-pieces B arranged longitudinally with their sides in the grooves in the side members of the girder. The tubes B may be secured to the girder by bolts C, and stiffening plates D, may be riveted, welded, or brazed to the girder for the attachment of the stays &c. The tubes at one or both ends of the girder may be shaped to provide a hinge connection for a flap or rudder. Struts F may be provided to connect the tubes B with the upper and lower flanges A<4>, A<5> of the girder, and are preferably tubular to receive bolts or the like for the attachment of stays, cross-girders &c.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB34567/22A GB210591A (en) | 1922-12-19 | 1922-12-19 | Improvements in girders and the like of box-like or similar section for use upon aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB34567/22A GB210591A (en) | 1922-12-19 | 1922-12-19 | Improvements in girders and the like of box-like or similar section for use upon aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB210591A true GB210591A (en) | 1924-02-07 |
Family
ID=10367229
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB34567/22A Expired GB210591A (en) | 1922-12-19 | 1922-12-19 | Improvements in girders and the like of box-like or similar section for use upon aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB210591A (en) |
-
1922
- 1922-12-19 GB GB34567/22A patent/GB210591A/en not_active Expired
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB210591A (en) | Improvements in girders and the like of box-like or similar section for use upon aircraft | |
US2407480A (en) | Aircraft fuselage and wing construction | |
US1992560A (en) | Aeroplane wing structure | |
GB329963A (en) | Improvements in and relating to fronts for furnaces | |
GB264626A (en) | Improvements in or relating to light metal structures | |
US2383635A (en) | Airfoil tip construction | |
US1973268A (en) | Aircraft structure | |
GB212993A (en) | Improvements in the construction of supporting planes for flying machines | |
US1883552A (en) | Airplane wing structure and method of making the same | |
GB130825A (en) | Improvements in or relating to the Spars of Aeroplane Wings. | |
GB520249A (en) | Improvements in stressed-skin structures of fuselages, wings and other hollow bodies of aircraft | |
GB382176A (en) | Improvements in or relating to wing structure for flying machines | |
GB339486A (en) | Improvements in the structure of monoplanes with thick wings | |
GB464249A (en) | Improvements relating to metal aeroplane bodies | |
GB213883A (en) | Improvements in or relating to frame components | |
GB325465A (en) | Cantilever spars for aircraft | |
GB151762A (en) | Improvements in metal strut and stay-wire connections for aircraft | |
GB154035A (en) | Improvements in metal construction for aircraft | |
GB360170A (en) | Improvements in metal spars suitable for aircraft | |
GB356129A (en) | Mode of construction of wings for flying apparatus | |
GB431895A (en) | Improvements in or connected with the construction of cantilever wings and other aircraft structures | |
GB487799A (en) | Improvements in or relating to aeroplanes | |
GB391333A (en) | Improvements in or relating to structural elements particularly for aircraft | |
GB136293A (en) | Improvements in Fittings for Aeronautical Machines. | |
GB410405A (en) | Improvements in and connected with aeroplane wings and/or tail sections |