GB262089A - Improvements in hot air airships - Google Patents
Improvements in hot air airshipsInfo
- Publication number
- GB262089A GB262089A GB2887426A GB2887426A GB262089A GB 262089 A GB262089 A GB 262089A GB 2887426 A GB2887426 A GB 2887426A GB 2887426 A GB2887426 A GB 2887426A GB 262089 A GB262089 A GB 262089A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aerostat
- cars
- envelope
- gases
- exhaust gases
- 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
- B64B1/58—Arrangements or construction of gas-bags; Filling arrangements
- B64B1/62—Controlling gas pressure, heating, cooling, or discharging gas
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Exhaust Silencers (AREA)
Abstract
262,089. Tallei, G. Nov. 16, 1926. Aerostats; propelling; cars. - The air within the envelope of a rigid airship is heated by the exhaust gases from the internal combustion engines used for propulsion. The envelope is formed of two sheet metal walls, an outer smooth wall 1, Fig. 4, and an inner corrugated wall of aluminium. The framework comprises a central longitudinal tube 8, Fig. 2, closed at the front end and to which spaced ring-shaped members 6 are connected by supporting spokes. The exhaust gases are delivered into the tube 8 in which openings may be provided to permit part of the gases to escape into the aerostat. The escape of the gases from the rear end of the tube 8 assists propulsion. Valves may be provided for maintaining a predetermined pressure within the aerostat. Aspirators may be used for actuating or retarding the flow of air or exhaust gases into and out of the envelope and for maintaining them in any desired position. Cars 5, Fig. 1, each provided with two or more propellers 18, are arranged on each side of the aerostat, communication be. tween the cars being effected through a recess 16.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2887426A GB262089A (en) | 1926-11-16 | 1926-11-16 | Improvements in hot air airships |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2887426A GB262089A (en) | 1926-11-16 | 1926-11-16 | Improvements in hot air airships |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB262089A true GB262089A (en) | 1927-08-18 |
Family
ID=10282552
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2887426A Expired GB262089A (en) | 1926-11-16 | 1926-11-16 | Improvements in hot air airships |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB262089A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2599241A (en) * | 1950-07-11 | 1952-06-03 | Walter E Farmer | Lighter than air aircraft with heating means for the gas bags thereof |
-
1926
- 1926-11-16 GB GB2887426A patent/GB262089A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2599241A (en) * | 1950-07-11 | 1952-06-03 | Walter E Farmer | Lighter than air aircraft with heating means for the gas bags thereof |
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