GB395259A - Improvements in or relating to the control of aircraft - Google Patents
Improvements in or relating to the control of aircraftInfo
- Publication number
- GB395259A GB395259A GB36771/32A GB3677132A GB395259A GB 395259 A GB395259 A GB 395259A GB 36771/32 A GB36771/32 A GB 36771/32A GB 3677132 A GB3677132 A GB 3677132A GB 395259 A GB395259 A GB 395259A
- Authority
- GB
- United Kingdom
- Prior art keywords
- lever
- spring
- bias
- control
- pivot
- 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
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tires In General (AREA)
Abstract
395,259. Controlling aircraft. AIRSPEED, Ltd. and TILTMAN, A. H., Piccadilly, York. Dec. 29, 1932, No. 36771. [Class 4.] Relates to spring bias means operat ing either on the control member or on the transmission and including means for rendering it operative to bias the control surface to either side of its neutral position. In one form, Fig. 2, a spring C is attached to a rudder bar A at one end C<1> and to one end of a lever D, pivoted to the fuselage at D<4>, at the other end C<2>. Lever D is normally maintained in a position in which the point of attachment C<2> is co-axial with the pivot axis of the rudder bar. To bring spring C into action to bias the rubber bar one way or the other lever D is displaced in the manner shown by a cable E operated by a hand-wheel E<3>. Fig. 3 shows a similar arrangement in which spring C is pivoted at C<3> to a lever D and at C<4> to a lever G connected at G<1> to a control cable. Pivot point C<3> is normally maintained co-axial with pivot H<2> of lever G but may be displaced in either direction from this position by rocking lever D.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB36771/32A GB395259A (en) | 1932-12-29 | 1932-12-29 | Improvements in or relating to the control of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB36771/32A GB395259A (en) | 1932-12-29 | 1932-12-29 | Improvements in or relating to the control of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB395259A true GB395259A (en) | 1933-07-13 |
Family
ID=10391060
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB36771/32A Expired GB395259A (en) | 1932-12-29 | 1932-12-29 | Improvements in or relating to the control of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB395259A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2009046508A2 (en) | 2007-10-09 | 2009-04-16 | EMBRAER-Empresa Brasileira de Aeronáutica S.A. | Mechanisms and methods for providing rudder control assist during symmetrical and asymmetrical thrust conditions |
-
1932
- 1932-12-29 GB GB36771/32A patent/GB395259A/en not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2009046508A2 (en) | 2007-10-09 | 2009-04-16 | EMBRAER-Empresa Brasileira de Aeronáutica S.A. | Mechanisms and methods for providing rudder control assist during symmetrical and asymmetrical thrust conditions |
| WO2009046508A3 (en) * | 2007-10-09 | 2010-02-04 | EMBRAER-Empresa Brasileira de Aeronáutica S.A. | Mechanisms and methods for providing rudder control assist during symmetrical and asymmetrical thrust conditions |
| EP2197740A2 (en) * | 2007-10-09 | 2010-06-23 | EMBRAER - Empresa Brasileira de Aeronáutica S.A. | Mechanisms and methods for providing rudder control assist during symmetrical and asymmetrical thrust conditions |
| US7984880B2 (en) * | 2007-10-09 | 2011-07-26 | Embraer-Empresa Brasileira De Aeronautica S.A. | Mechanisms and methods for providing rudder control assist during symmetrical and asymmetrical thrust conditions |
| EP2197740A4 (en) * | 2007-10-09 | 2014-11-26 | Embraer Aeronautica Sa | Mechanisms and methods for providing rudder control assist during symmetrical and asymmetrical thrust conditions |
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