GB213705A - Improvements in and relating to aircraft - Google Patents
Improvements in and relating to aircraftInfo
- Publication number
- GB213705A GB213705A GB154323A GB154323A GB213705A GB 213705 A GB213705 A GB 213705A GB 154323 A GB154323 A GB 154323A GB 154323 A GB154323 A GB 154323A GB 213705 A GB213705 A GB 213705A
- Authority
- GB
- United Kingdom
- Prior art keywords
- planes
- struts
- stepped
- series
- 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
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/006—Paddle wheels
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Pivots And Pivotal Connections (AREA)
Abstract
213,705. McKelvey, A. L. Jan. 17, 1923. Planes, arrangement and disposition of; planes, connecting to machine; framework. -A rigid framework for supporting a stepped series of sustaining planes B, consists of a lattice girder A projecting from which are struts 5 supporting tension wires or bars 6. A complete sustaining unit comprises a number of these stepped series of planes arranged side by side, each series being supported between two lattice girders A. The girders A consist of upper and lower booms 2, formed of angle strips placed back-to-back, and rigidly connected at their ends to vertically-disposed laced struts 1. The stepped planes B are fixed, by means of angle plates 7, to diagonally-arranged bracing strips 4 which are riveted at their ends to the booms 2. Steering, balancing, and regulating altitude. - Elevating planes C are rotatably mounted in bracket-bearings 8 mounted upon the vertical struts 1.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB154323A GB213705A (en) | 1923-01-17 | 1923-01-17 | Improvements in and relating to aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB154323A GB213705A (en) | 1923-01-17 | 1923-01-17 | Improvements in and relating to aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB213705A true GB213705A (en) | 1924-04-10 |
Family
ID=9723787
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB154323A Expired GB213705A (en) | 1923-01-17 | 1923-01-17 | Improvements in and relating to aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB213705A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5661741A (en) * | 1994-06-07 | 1997-08-26 | Mitsubishi Denki Kabushiki Kaisha | Semiconductor light emitting device, laser amplifier, and integrated light amplifier and wavelength variable filter |
-
1923
- 1923-01-17 GB GB154323A patent/GB213705A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5661741A (en) * | 1994-06-07 | 1997-08-26 | Mitsubishi Denki Kabushiki Kaisha | Semiconductor light emitting device, laser amplifier, and integrated light amplifier and wavelength variable filter |
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