GB191400867A - Improvements in connection with Aeroplanes for Stabilising and Steering them while Flying at Slow Speeds. - Google Patents
Improvements in connection with Aeroplanes for Stabilising and Steering them while Flying at Slow Speeds.Info
- Publication number
- GB191400867A GB191400867A GB191400867DA GB191400867A GB 191400867 A GB191400867 A GB 191400867A GB 191400867D A GB191400867D A GB 191400867DA GB 191400867 A GB191400867 A GB 191400867A
- Authority
- GB
- United Kingdom
- Prior art keywords
- planes
- steering
- adjusted
- rear edge
- 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
- 230000003019 stabilising effect Effects 0.000 title 1
- JHIVVAPYMSGYDF-UHFFFAOYSA-N cyclohexanone Chemical compound O=C1CCCCC1 JHIVVAPYMSGYDF-UHFFFAOYSA-N 0.000 abstract 1
- 230000000087 stabilizing effect Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/10—Drag reduction
Abstract
867. Soc. Anon. Ateliers d'Aviation L. BrÚguet. Dec. 15, 1913, [Convention date]. Steering and balancing; propelling.-In an areoplane having a single propeller of large diameter driven at a slow speed through rejucing - gear, auxiliary stabilizing surfaces or sails are arranged at or near to the front or rear edge of the main supporting-planes in the path of the current of air from the propeller, in order to increase their efficiency. In one form, the horizontal planes b<1>, Fig. 1, are arranged between the leading edges of the upper and lower planes and are adjusted about transverse pivots either together or separately. Vertical adjustable planes b<2> are arranged centrally of the machine near the forward edges of the planes. As applied to a monoplane, the adjustable planes b<1>, Fig. 6, are hinged to the rear edge of the main plane c<2>, which may itself be adjusted about the transverse axis j<1> ; in this case, the operating- cords h<1> of the planes b<1> pass over pulleys i<1> coincident with the axis j<1>.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR191400867X | 1913-12-15 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB191400867A true GB191400867A (en) | 1914-11-12 |
Family
ID=32526479
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB191400867D Expired GB191400867A (en) | 1913-12-15 | 1914-01-12 | Improvements in connection with Aeroplanes for Stabilising and Steering them while Flying at Slow Speeds. |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB191400867A (en) |
-
1914
- 1914-01-12 GB GB191400867D patent/GB191400867A/en not_active Expired
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