GB424140A - Improvements relating to air-craft of the gyroplane type - Google Patents
Improvements relating to air-craft of the gyroplane typeInfo
- Publication number
- GB424140A GB424140A GB23240/33A GB2324033A GB424140A GB 424140 A GB424140 A GB 424140A GB 23240/33 A GB23240/33 A GB 23240/33A GB 2324033 A GB2324033 A GB 2324033A GB 424140 A GB424140 A GB 424140A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wings
- craft
- air
- rotated
- aircraft
- 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
- B64C39/00—Aircraft not otherwise provided for
- B64C39/003—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage
- B64C39/005—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage about a horizontal transversal axis
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Wind Motors (AREA)
Abstract
424,140. Aircraft with rotary wing systems. JONES, T., Cwmbach, Pontyates, Llanelly, Carmarthenshire. Aug. 21, 1933, No. 23240. [Class 4] In an aircraft provided with ordinary means of propulsion and with lifting rotors or wings 3 rotated by the relative wind pressure, the wings 3 are mounted on a shaft 5 adapted to be rotated, during take-off from land wheels 2 through a crossed belt 7 and pulleys 6, 8. Means are provided for disconnecting the land wheels from the wings in flight. The edges of the wings may be deeply recessed, or scalloped or constituted by a series of arcs struck from the longitudinal centre of the blades. The wings may also be built up of a number of spaced apart discs. Specification 402,992 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB23240/33A GB424140A (en) | 1933-08-21 | 1933-08-21 | Improvements relating to air-craft of the gyroplane type |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB23240/33A GB424140A (en) | 1933-08-21 | 1933-08-21 | Improvements relating to air-craft of the gyroplane type |
Publications (1)
Publication Number | Publication Date |
---|---|
GB424140A true GB424140A (en) | 1935-02-15 |
Family
ID=10192431
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB23240/33A Expired GB424140A (en) | 1933-08-21 | 1933-08-21 | Improvements relating to air-craft of the gyroplane type |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB424140A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2681775A (en) * | 1951-05-24 | 1954-06-22 | Orazi Paolo | Convertible airplane having autorotatable sustaining elements |
US3079126A (en) * | 1959-05-05 | 1963-02-26 | Specialized Patents Sales And | Turbine systems |
GB2195308A (en) * | 1986-09-23 | 1988-04-07 | Lawrence Albert Holmes | Rotating wing aircraft |
EP0264529A1 (en) * | 1986-08-19 | 1988-04-27 | Rheinmetall GmbH | Missile with a stabilizing device |
-
1933
- 1933-08-21 GB GB23240/33A patent/GB424140A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2681775A (en) * | 1951-05-24 | 1954-06-22 | Orazi Paolo | Convertible airplane having autorotatable sustaining elements |
US3079126A (en) * | 1959-05-05 | 1963-02-26 | Specialized Patents Sales And | Turbine systems |
EP0264529A1 (en) * | 1986-08-19 | 1988-04-27 | Rheinmetall GmbH | Missile with a stabilizing device |
US4903917A (en) * | 1986-08-19 | 1990-02-27 | Rheinmetall Gmbh | Projectile with rotatable stabilizing device |
GB2195308A (en) * | 1986-09-23 | 1988-04-07 | Lawrence Albert Holmes | Rotating wing aircraft |
GB2195308B (en) * | 1986-09-23 | 1990-09-26 | Lawrence Albert Holmes | An aircraft |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB424140A (en) | Improvements relating to air-craft of the gyroplane type | |
GB516738A (en) | Improvements in landing wheels for aircraft | |
GB408457A (en) | Improvements in or relating to sustaining or propelling surfaces particularly aeroplane wing structures | |
GB1124929A (en) | A folding multi-blade airscrew | |
GB568548A (en) | Improvements in aircraft | |
GB536865A (en) | Improvements in or relating to aircraft | |
GB612304A (en) | Improvements in aeroplane construction | |
GB483043A (en) | Improvements relating to aircraft | |
GB608883A (en) | Improvements relating to aircraft | |
GB577524A (en) | Improvement in airing of anti-torque propeller | |
GB364151A (en) | Aircraft | |
GB663206A (en) | Improvements relating to helicopters | |
GB348528A (en) | Improvements relating to aeroplanes | |
GB536904A (en) | Aeroplanes | |
GB523357A (en) | Improved propulsion for aircraft | |
GB601913A (en) | Improvements in and relating to sustaining or sustaining and propulsive blades for helicopters | |
GB1175073A (en) | Improvements in or relating to Vertical Take-off and Landing Aircraft | |
GB456177A (en) | Improvements in or relating to aircraft provided with rotating wings | |
GB405539A (en) | Improvements in arrangements for starting flight requiring no gliding | |
GB319613A (en) | Improvements in or relating to aircraft | |
GB212547A (en) | Improvements in the driving of flying machines | |
GB372422A (en) | Improvements in flying machines | |
GB516013A (en) | Improvements in or relating to two-motored aircraft, having tractor and pusher airscrews | |
GB477894A (en) | Improvements in lifting means for aircraft | |
GB366603A (en) | Improvements in or relating to rotating wing systems, propellers, or lifting screws for aircraft |