GB456632A - Landing gear for aeroplanes - Google Patents
Landing gear for aeroplanesInfo
- Publication number
- GB456632A GB456632A GB8350/36A GB835036A GB456632A GB 456632 A GB456632 A GB 456632A GB 8350/36 A GB8350/36 A GB 8350/36A GB 835036 A GB835036 A GB 835036A GB 456632 A GB456632 A GB 456632A
- Authority
- GB
- United Kingdom
- Prior art keywords
- strut
- struts
- jointed
- jack
- gear
- 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
- B64C25/00—Alighting gear
- B64C25/02—Undercarriages
- B64C25/08—Undercarriages non-fixed, e.g. jettisonable
- B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
- B64C25/12—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like sideways
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tires In General (AREA)
Abstract
456,632. Aircraft alighting gear. AEROPLANES MORANE-SAULNIER SOC. ANON. DE CONSTRUCTIONS AERONAUTIQUES, 3, Rue Volta, Puteaux, Seine, France. March 20, 1936, No. 8350. Convention date, March 22, 1935. [Class 4] Aircraft landing-gear comprises three struts pivoted at fixed points to the aeroplane, the outer ends of the struts being connected together, one of the struts being jointed such that folding of the jointed strut 11 causes the landing-gear to pivot with respect to the aeroplane ; the jointed strut is controlled to fold and straighten by a fluid-actuated jack 13 entirely supported by the strut 11 and disposed at right angles to the line of the strut when in the straightened position, the three struts constituting a pyramidal structure adapted to be folded in any direction depending upon which strut is the jointed strut. The two parts of the strut 11 may be articulated on either side of the jack cylinder, or the jack may be mounted at the common point of articulation. The jack is further connected to the strut 11 by links 16 and in one form two of the struts are pivoted about a spindle 20. Specification 442,133 is referred to.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE456632X | 1935-03-22 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB456632A true GB456632A (en) | 1936-11-12 |
Family
ID=6539205
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB8350/36A Expired GB456632A (en) | 1935-03-22 | 1936-03-20 | Landing gear for aeroplanes |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB456632A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2652559A1 (en) * | 1989-09-29 | 1991-04-05 | Fontanille Guy | Retractable or withdrawable thruster using a trapezoidal device with deforming rotation generating a rectilinear movement inside a well |
| JP2012101784A (en) * | 2010-11-05 | 2012-05-31 | Goodrich Corp | Vertically retracting side articulating landing gear for aircraft |
-
1936
- 1936-03-20 GB GB8350/36A patent/GB456632A/en not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2652559A1 (en) * | 1989-09-29 | 1991-04-05 | Fontanille Guy | Retractable or withdrawable thruster using a trapezoidal device with deforming rotation generating a rectilinear movement inside a well |
| US5152240A (en) * | 1989-09-29 | 1992-10-06 | Guy Fontanille | Retractable or storable thruster using a trapezodidal deformably rotatable device producing rectilinear movement inside a well |
| JP2012101784A (en) * | 2010-11-05 | 2012-05-31 | Goodrich Corp | Vertically retracting side articulating landing gear for aircraft |
| US9205917B2 (en) | 2010-11-05 | 2015-12-08 | Goodrich Corporation | Vertically retracting side articulating landing gear for aircraft |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| SE7601399L (en) | RETRABLE, LINKED AIRPORT FROM AIRCRAFT | |
| GB456632A (en) | Landing gear for aeroplanes | |
| US2021439A (en) | Retractable landing gear | |
| GB490151A (en) | Improvements relating to folding wings for aeroplanes | |
| US2478426A (en) | Retractable undercarriage for aircraft | |
| US2589434A (en) | Retractable landing gear for aircraft | |
| US1485775A (en) | Folding chassis for aircraft | |
| GB485414A (en) | Improvements in or relating to self-folding struts for aeroplane landing chassis | |
| US2069994A (en) | Folding landing gear | |
| GB393445A (en) | Improvements in or relating to aircraft landing gear | |
| GB510164A (en) | Improvements in aircraft landing (or alighting) gear | |
| GB613051A (en) | Improvements to retractable landing gears for aircraft | |
| GB478778A (en) | Retractable landing gear of aeroplanes | |
| GB508367A (en) | Improvements relating to aeroplanes | |
| US2154984A (en) | Self-folding strut for airplane landing chassis | |
| GB458187A (en) | Improvements relating to retractable undercarriages for aircraft | |
| GB397964A (en) | Improvements in or relating to aeroplanes | |
| GB568644A (en) | Improvements in retractable aircraft undercarriages | |
| GB463807A (en) | Improvements in or relating to retractable landing gear, and and the like, for aircraft | |
| GB506528A (en) | Improvements relating to folding wing aircraft | |
| GB600477A (en) | Improvements in or relating to airplanes with pivoting wings | |
| GB438296A (en) | Improvements relating to retractable aircraft undercarriages | |
| GB420209A (en) | Improvements in and relating to aeroplanes with folding wings | |
| GB571782A (en) | Improvement in retractable landing gear for airplanes | |
| GB429867A (en) | Improvements in or relating to landing gear for aeroplanes |