GB154970A - Air craft - Google Patents
Air craftInfo
- Publication number
- GB154970A GB154970A GB2110919A GB2110919A GB154970A GB 154970 A GB154970 A GB 154970A GB 2110919 A GB2110919 A GB 2110919A GB 2110919 A GB2110919 A GB 2110919A GB 154970 A GB154970 A GB 154970A
- Authority
- GB
- United Kingdom
- Prior art keywords
- frames
- planes
- aerostat
- frame
- floats
- 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
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Air Bags (AREA)
- Steering Controls (AREA)
Abstract
154,970. McKelvey, A. L. Aug. 28, 1919. Aerial machines with aerostats, aerostats; cars and cabins; frame work; planes, arrangement of; propelling; steering; floats, arrangement of.-An aircraft is constructed with a longitudinal aerostat and two elongated transverse parallel enclosing frames upon which are mounted side and upper sustaining-planes. The pro. pellers, engines, controlling planes, and two float members are aLso attached to these frames. The transverse frames A, A<1> are built up of T- section bars 1, 2, 3, 4, and struts 6. Radial members 42, which pass through the aerostat D to radial members 9, are also used. External struts 16 support the floats B. The aerostat frame is octagonal in section and formed of transverse frames connected by longitudinals, the transverse frames having an inner circular frame braced to the octagonal outer frame and suitable cross stays 21. An outer cover is used, and there is a gasbag between each pair of frames. A cabin C is placed at the bottom of the aerostat. Tandem biplanes F, with tractor and pusher propellers 39 and driving engines, are mounted on the two frames A, A<1>. In addition, pivoted controlling- planes G are placed between the wings of each biplane member. Directional control is effected by a rudder E, pivoted to the central rod 5 of the framework of the after main frame A'. Above the main frames an additional central biplane H is fitted, and planes J may be fitted to the floats.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2110919A GB154970A (en) | 1919-08-28 | 1919-08-28 | Air craft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2110919A GB154970A (en) | 1919-08-28 | 1919-08-28 | Air craft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB154970A true GB154970A (en) | 1920-11-29 |
Family
ID=10157367
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2110919A Expired GB154970A (en) | 1919-08-28 | 1919-08-28 | Air craft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB154970A (en) |
-
1919
- 1919-08-28 GB GB2110919A patent/GB154970A/en not_active Expired
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