GB124819A - Improvements in the Construction of Car Frame Work of Airships, Aeroplanes and the like. - Google Patents
Improvements in the Construction of Car Frame Work of Airships, Aeroplanes and the like.Info
- Publication number
- GB124819A GB124819A GB585716A GB585716A GB124819A GB 124819 A GB124819 A GB 124819A GB 585716 A GB585716 A GB 585716A GB 585716 A GB585716 A GB 585716A GB 124819 A GB124819 A GB 124819A
- Authority
- GB
- United Kingdom
- Prior art keywords
- joints
- spherical
- booms
- joint
- aeroplanes
- 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
- B64C1/08—Geodetic or other open-frame structures
Abstract
124,819. Day, B. I., and Rolls-Royce, Ltd. April 20, 1916. Wire and rod couplings and joints.- The struts, booms, and stays of the car framework of air-ships, aeroplanes, &c. are connected together by ball-andsocket joints to minimize bending- movements. Fig. 1 shows a car frame comprising booms a, struts b, and stays c connected by ball-and-socket joints, the rigging cables d and the tierods e being also connected to the joints. Fig. 3 shows one of the joints, in which the stay is provided with a two-part spherical end c<2> forming the inner member of the joint; the booms a are formed with part-spherical ends a<2> which engage on opposite sides of the member c<2>, and the strut b is formed with a semi-spherical member b<2> adapted to bear on the members a<2>, the joint being completed bv a semi-spherical part b<3> which is bolted to the part b<2>. The cable d is passed through holes in the members b<2>, a<2>, c<2> and attached by a nut d<2> to a part-spherical bearing-member d' inside the joint. The tie-rods e are attached to flanges e<1>.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB585716A GB124819A (en) | 1916-04-20 | 1916-04-20 | Improvements in the Construction of Car Frame Work of Airships, Aeroplanes and the like. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB585716A GB124819A (en) | 1916-04-20 | 1916-04-20 | Improvements in the Construction of Car Frame Work of Airships, Aeroplanes and the like. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB124819A true GB124819A (en) | 1919-04-10 |
Family
ID=32342328
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB585716A Expired GB124819A (en) | 1916-04-20 | 1916-04-20 | Improvements in the Construction of Car Frame Work of Airships, Aeroplanes and the like. |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB124819A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4543762A (en) * | 1980-10-15 | 1985-10-01 | Scanding Byggkonsult Aktiebolag | Flexible terminal point for lattice work construction |
| GB2448997A (en) * | 2007-05-03 | 2008-11-05 | Boeing Co | Aircraft for carrying containerised cargo |
-
1916
- 1916-04-20 GB GB585716A patent/GB124819A/en not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4543762A (en) * | 1980-10-15 | 1985-10-01 | Scanding Byggkonsult Aktiebolag | Flexible terminal point for lattice work construction |
| GB2448997A (en) * | 2007-05-03 | 2008-11-05 | Boeing Co | Aircraft for carrying containerised cargo |
| GB2448997B (en) * | 2007-05-03 | 2010-02-24 | Boeing Co | Aircraft with space frame fuselage structure for carrying containerised cargo and related method |
| US7891608B2 (en) | 2007-05-03 | 2011-02-22 | The Boeing Company | Space frame fuselage structure and related methods |
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