GB910792A - Improvements in aeroplanes having wings adjustable in sweep - Google Patents
Improvements in aeroplanes having wings adjustable in sweepInfo
- Publication number
- GB910792A GB910792A GB3955559A GB3955559A GB910792A GB 910792 A GB910792 A GB 910792A GB 3955559 A GB3955559 A GB 3955559A GB 3955559 A GB3955559 A GB 3955559A GB 910792 A GB910792 A GB 910792A
- Authority
- GB
- United Kingdom
- Prior art keywords
- root
- sweep
- wing
- annulus
- nov
- 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
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/40—Varying angle of sweep
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Footwear And Its Accessory, Manufacturing Method And Apparatuses (AREA)
- Supports For Plants (AREA)
- Wind Motors (AREA)
Abstract
910,792. Hinges and pivots. VICKERS-ARMSTRONGS (AIRCRAFT) Ltd. Nov. 7, 1960 [Nov. 20, 1959], No. 39555/59. Class 65 (2). [Also in Group XXXIII] In an aeroplane having wings adjustable in sweep, each wing pivot comprises an annulus 10 fixed at points 111, 112 to the aeroplane body 11 and mounted by the wing root 14. The root 14 has hemispherical shoes 15 arranged in opposed pairs to embrace, and slide, on annulus 10, the shoe seating in comformably shaped recesses in root 14. Opposed sets of rollers 16 mounted in root 14 positively locate the wing relative to the pivot axis 12. Specifications 832,760 is referred to.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3955559A GB910792A (en) | 1959-11-20 | 1959-11-20 | Improvements in aeroplanes having wings adjustable in sweep |
ES0262582A ES262582A1 (en) | 1959-11-20 | 1960-11-19 | Improvements in aeroplanes having wings adjustable in sweep |
NL258193A NL110890C (en) | 1959-11-20 | 1960-11-21 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3955559A GB910792A (en) | 1959-11-20 | 1959-11-20 | Improvements in aeroplanes having wings adjustable in sweep |
Publications (1)
Publication Number | Publication Date |
---|---|
GB910792A true GB910792A (en) | 1962-11-21 |
Family
ID=10410182
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3955559A Expired GB910792A (en) | 1959-11-20 | 1959-11-20 | Improvements in aeroplanes having wings adjustable in sweep |
Country Status (3)
Country | Link |
---|---|
ES (1) | ES262582A1 (en) |
GB (1) | GB910792A (en) |
NL (1) | NL110890C (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5337974A (en) * | 1992-04-15 | 1994-08-16 | The Boeing Company | Wing pivot structure |
-
1959
- 1959-11-20 GB GB3955559A patent/GB910792A/en not_active Expired
-
1960
- 1960-11-19 ES ES0262582A patent/ES262582A1/en not_active Expired
- 1960-11-21 NL NL258193A patent/NL110890C/xx active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5337974A (en) * | 1992-04-15 | 1994-08-16 | The Boeing Company | Wing pivot structure |
Also Published As
Publication number | Publication date |
---|---|
NL110890C (en) | 1965-03-15 |
ES262582A1 (en) | 1961-06-01 |
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