GB398069A - Aeroplanes with autostable arrangements of planes - Google Patents
Aeroplanes with autostable arrangements of planesInfo
- Publication number
- GB398069A GB398069A GB35352/32A GB3535232A GB398069A GB 398069 A GB398069 A GB 398069A GB 35352/32 A GB35352/32 A GB 35352/32A GB 3535232 A GB3535232 A GB 3535232A GB 398069 A GB398069 A GB 398069A
- Authority
- GB
- United Kingdom
- Prior art keywords
- planes
- fuselages
- plane
- divided
- aeroplanes
- 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
- B64C39/04—Aircraft not otherwise provided for having multiple fuselages or tail booms
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Current-Collector Devices For Electrically Propelled Vehicles (AREA)
- Automatic Cycles, And Cycles In General (AREA)
Abstract
398,069. Aeroplanes. ALBESSARD, J., 31, Rue du Laos, Paris. Dec. 13, 1932, No. 35352. [Class 4.] An aeroplane has tandem planes with the rear plane b divided and the halves arranged beyond the span of the front plane a as shown in Fig. 3 to act in the upward currents escaping without interference from the ends of the front plane, or the front plane a may be divided and the rear plane b arranged behind the gap, as shown in Fig. 4. Successive pairs of such planes may be arranged in tandem along a single fuselage or on twin fuselages provided the space between planes on the same fore-andaft line exceeds 3À5 times the chord of the preceding plane. The planes may also be at different levels. Among other arrangements described is a machine with four fuselages having a leading plane between the two inner fuselages, two planes arranged between the inner and outer fuselages and farther back, and two rearmost planes outside the outer fuselages. Another machine with four fuselages has three forward planes abreast with gaps between the inner and outer fuselages and two planes behind the gaps. Girders p connect the divided halves of the planes and fairings are pivoted around them to trail in the wind. Specifications 18109/13, 245,268, and 284,637, [all in Class 4, Aeronautics], are referred to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB35352/32A GB398069A (en) | 1932-12-13 | 1932-12-13 | Aeroplanes with autostable arrangements of planes |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB35352/32A GB398069A (en) | 1932-12-13 | 1932-12-13 | Aeroplanes with autostable arrangements of planes |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB398069A true GB398069A (en) | 1933-09-07 |
Family
ID=10376770
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB35352/32A Expired GB398069A (en) | 1932-12-13 | 1932-12-13 | Aeroplanes with autostable arrangements of planes |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB398069A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2469619A (en) * | 1943-11-17 | 1949-05-10 | Douglas K Warner | Aircraft whose lift is increased by power means |
| GB2328918A (en) * | 1997-09-04 | 1999-03-10 | British Aerospace | Selecting modules to produce aircraft variants |
-
1932
- 1932-12-13 GB GB35352/32A patent/GB398069A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2469619A (en) * | 1943-11-17 | 1949-05-10 | Douglas K Warner | Aircraft whose lift is increased by power means |
| GB2328918A (en) * | 1997-09-04 | 1999-03-10 | British Aerospace | Selecting modules to produce aircraft variants |
| US6065720A (en) * | 1997-09-04 | 2000-05-23 | British Aerospace Public Limited Company | Manufacture of aircraft |
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