GB190907209A - Improvements in Flying Machines, Air Ships, and the like. - Google Patents
Improvements in Flying Machines, Air Ships, and the like.Info
- Publication number
- GB190907209A GB190907209A GB190907209DA GB190907209A GB 190907209 A GB190907209 A GB 190907209A GB 190907209D A GB190907209D A GB 190907209DA GB 190907209 A GB190907209 A GB 190907209A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wings
- ribs
- wing
- arms
- over pulleys
- 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
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
7209. BrÚguet, L. Oct. 28, 1908, [Convention date]. Balancing automatically by oppositely tilting wings connected in pairs. The lateral balance of an aerial machine is maintained by so connecting the sustaining-wings that a variation in wind pressure deflecting the wing on one side is balanced by an equal and opposite deflexion of the wing on the other side. The main ribs a of the wings may for this purpose (1) be differentially geared as shown in Fig. 1, or (2) be provided with arms f, Fig. 2, connected with a pivoted beam h; or (3) these arms may be connected to a continuous belt running over pulleys, or (4) a belt may run over pulleys mounted on the ribs a. Planes, construction of.-The fabric &c. of the wings is preferably supported by cross-ribs b, Fig. 7, mounted with limited spring-controlled movement on the rib a.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR190907209X | 1908-10-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB190907209A true GB190907209A (en) | 1909-12-02 |
Family
ID=32407122
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB190907209D Expired GB190907209A (en) | 1908-10-28 | 1909-03-25 | Improvements in Flying Machines, Air Ships, and the like. |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB190907209A (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2584667A (en) * | 1947-02-14 | 1952-02-05 | George E Bockrath | Gust alleviating control means for airplanes |
US3140844A (en) * | 1963-03-29 | 1964-07-14 | Alan H Rich | Aircraft stabilization device |
US4483498A (en) * | 1982-07-14 | 1984-11-20 | Mcdonnell Douglas Corporation | Flight control surface coupling system |
US5280863A (en) * | 1991-11-20 | 1994-01-25 | Hugh Schmittle | Lockable free wing aircraft |
US5340057A (en) * | 1991-11-20 | 1994-08-23 | Freewing Aerial Robotics Corporation | Thrust vectoring free wing aircraft |
US5395073A (en) * | 1992-03-13 | 1995-03-07 | Freewing Aerial Robotics Corporation | STOL/VTOL free wing aircraft with articulated tail boom |
US5769359A (en) * | 1993-01-22 | 1998-06-23 | Freewing Aerial Robotics Corporation | Active feedback loop to control body pitch in STOL/VTOL free wing aircraft |
US5863013A (en) * | 1991-11-20 | 1999-01-26 | Freewing Aerial Robotics Corporation | STOL/VTOL free wing aircraft with improved shock dampening and absorbing means |
USRE36487E (en) * | 1989-02-09 | 2000-01-11 | Freewing Aerial Robotics Corporation | Airplane with variable-incidence wing |
-
1909
- 1909-03-25 GB GB190907209D patent/GB190907209A/en not_active Expired
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2584667A (en) * | 1947-02-14 | 1952-02-05 | George E Bockrath | Gust alleviating control means for airplanes |
US3140844A (en) * | 1963-03-29 | 1964-07-14 | Alan H Rich | Aircraft stabilization device |
US4483498A (en) * | 1982-07-14 | 1984-11-20 | Mcdonnell Douglas Corporation | Flight control surface coupling system |
USRE36487E (en) * | 1989-02-09 | 2000-01-11 | Freewing Aerial Robotics Corporation | Airplane with variable-incidence wing |
US5280863A (en) * | 1991-11-20 | 1994-01-25 | Hugh Schmittle | Lockable free wing aircraft |
US5340057A (en) * | 1991-11-20 | 1994-08-23 | Freewing Aerial Robotics Corporation | Thrust vectoring free wing aircraft |
US5863013A (en) * | 1991-11-20 | 1999-01-26 | Freewing Aerial Robotics Corporation | STOL/VTOL free wing aircraft with improved shock dampening and absorbing means |
US5395073A (en) * | 1992-03-13 | 1995-03-07 | Freewing Aerial Robotics Corporation | STOL/VTOL free wing aircraft with articulated tail boom |
US5769359A (en) * | 1993-01-22 | 1998-06-23 | Freewing Aerial Robotics Corporation | Active feedback loop to control body pitch in STOL/VTOL free wing aircraft |
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