GB274534A - Improvements in or relating to planes for aircraft of the helicopter type - Google Patents
Improvements in or relating to planes for aircraft of the helicopter typeInfo
- Publication number
- GB274534A GB274534A GB7286/26A GB728626A GB274534A GB 274534 A GB274534 A GB 274534A GB 7286/26 A GB7286/26 A GB 7286/26A GB 728626 A GB728626 A GB 728626A GB 274534 A GB274534 A GB 274534A
- Authority
- GB
- United Kingdom
- Prior art keywords
- planes
- sections
- wing
- collapsed
- wires
- 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
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
- B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
274,534. Oldfield, W. R. March 16, 1926. Screw propellers.-The wings of a freely rotating wing-system are built up of telescopic sections which may be collapsed or extended longitudinally at the will of the pilot. In the machine described, the wing-system comprises four planes 2 connected by hinge fittings 4 to a freely-rotatable mast 6 mounted in a bearing 9 carried by the fuselage. The planes 2 each consist of a number of telescopic sections 3 of sheet metal covered externally or internally, or both, with fabric, and of progressively increasing thickness and width towards their tips. The outer open end of each section is braced by ribs 26 attached to angle pieces 27 which may be hinged to facilitate removal of the ribs. The sections are of tapering thickness so that when they are extended a wedge action is set up : the joints may be made .airtight by interposing rubber packing. The innermost sections are reinforced by tubular stays 21 braced, if desired, by tie wires. The planes are normally held collapsed by tension wires 12 incorporating springs or elastic cords and connected to the outermost sections, which also carry weights 28. A modification is referred to in which the sections 3 decrease in thickness and width towards the tips. The mast 6 is fitted at its base with a friction clutch 16, 17 operable by a lever 18. Normally this clutch holds the wing-system against rotation at which time the planes 2 are collapsed by the tension wires 12. When the clutch is released, the wing-system is rotated by the air stream and under centrifugal action aided by the weights 28 extends against the tension of the wires 12. If desired the main planes 8 may be made to telescope under the control of the pilot so that they may be collapsed when the rotary wing system is extended.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7286/26A GB274534A (en) | 1926-03-16 | 1926-03-16 | Improvements in or relating to planes for aircraft of the helicopter type |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7286/26A GB274534A (en) | 1926-03-16 | 1926-03-16 | Improvements in or relating to planes for aircraft of the helicopter type |
Publications (1)
Publication Number | Publication Date |
---|---|
GB274534A true GB274534A (en) | 1927-07-18 |
Family
ID=9830170
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB7286/26A Expired GB274534A (en) | 1926-03-16 | 1926-03-16 | Improvements in or relating to planes for aircraft of the helicopter type |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB274534A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2575886A (en) * | 1943-02-27 | 1951-11-20 | Myers George Francis | Helicopter antitorque mechanism |
US4029435A (en) * | 1976-01-29 | 1977-06-14 | Barker Sidney L | Retractable blade for a helicopter rotor |
FR2976912A1 (en) * | 2011-06-24 | 2012-12-28 | Eurocopter France | Aircraft, has half-wing with lower portion arranged in wake of upper portion, where wake is generated by flow of air from rotary wing by impacting suction face from upper portion when aircraft has feed rate lower than preset threshold |
WO2013077718A1 (en) * | 2011-11-21 | 2013-05-30 | Poblette Espinosa Mireles Hector | Retractable rotor blades for rotary-wing aircraft |
-
1926
- 1926-03-16 GB GB7286/26A patent/GB274534A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2575886A (en) * | 1943-02-27 | 1951-11-20 | Myers George Francis | Helicopter antitorque mechanism |
US4029435A (en) * | 1976-01-29 | 1977-06-14 | Barker Sidney L | Retractable blade for a helicopter rotor |
FR2976912A1 (en) * | 2011-06-24 | 2012-12-28 | Eurocopter France | Aircraft, has half-wing with lower portion arranged in wake of upper portion, where wake is generated by flow of air from rotary wing by impacting suction face from upper portion when aircraft has feed rate lower than preset threshold |
US8820673B2 (en) | 2011-06-24 | 2014-09-02 | Airbus Helicopters | Rotary-wing and fixed-wing aircraft |
WO2013077718A1 (en) * | 2011-11-21 | 2013-05-30 | Poblette Espinosa Mireles Hector | Retractable rotor blades for rotary-wing aircraft |
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