GB242599A - Improvements in landing frames for aeroplanes - Google Patents
Improvements in landing frames for aeroplanesInfo
- Publication number
- GB242599A GB242599A GB21525/25A GB2152525A GB242599A GB 242599 A GB242599 A GB 242599A GB 21525/25 A GB21525/25 A GB 21525/25A GB 2152525 A GB2152525 A GB 2152525A GB 242599 A GB242599 A GB 242599A
- Authority
- GB
- United Kingdom
- Prior art keywords
- struts
- axle
- fuselage
- rotatable
- elastic
- 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
- B64C25/06—Undercarriages fixed
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/60—Oleo legs
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vehicle Body Suspensions (AREA)
- Handcart (AREA)
Abstract
242,599. Potez, H. C. A. Nov. 6, 1924, [Convention date]. No Patent granted (Sealing fee not paid). Land wheels; shock-absorbers, applications of. -A landing frame comprises an axle 30 in two parts hinged together at 19, so as to be capable of relative movement in a substantitlly vertical plane but not in a horizontal one. The hinge member 17 is secured to a V-shaped member 2 pivoted to the fuelage at 11, 12 by means of a pivot pin 16, formed on the member 2 and passing through the hinge member, the arrangement being such that the member 17 can move only in the plane of symmetry of the aeroplane. In an alternative construction, Figs. 4, 5 the pivot pin 20 is rotatable in the member 2 and the axle joint employs a single pin 23. The outer ends of the axle are connected to elastic struts 5, 6 and to struts 3, 4, which may be elastic, by means of universal joints and sleeves 13, 14 rotatable on the axle. The struts are connected to the fuselage by universal joints. The attachments of the member 2 to the fuselage may be made adjacent those of the struts 5, 6 or those of the struts 3, 4.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR242599X | 1924-11-06 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB242599A true GB242599A (en) | 1926-03-25 |
Family
ID=8883405
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB21525/25A Expired GB242599A (en) | 1924-11-06 | 1925-08-27 | Improvements in landing frames for aeroplanes |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB242599A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2691496A (en) * | 1950-05-12 | 1954-10-12 | United Aircraft Corp | Aircraft landing gear |
| FR3028837A1 (en) * | 2014-11-24 | 2016-05-27 | Beringer Aero | LANDING TRAIN COMPRISING AT LEAST TWO WHEELS FOR LIGHT AIRCRAFT |
-
1925
- 1925-08-27 GB GB21525/25A patent/GB242599A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2691496A (en) * | 1950-05-12 | 1954-10-12 | United Aircraft Corp | Aircraft landing gear |
| FR3028837A1 (en) * | 2014-11-24 | 2016-05-27 | Beringer Aero | LANDING TRAIN COMPRISING AT LEAST TWO WHEELS FOR LIGHT AIRCRAFT |
| WO2016083726A1 (en) * | 2014-11-24 | 2016-06-02 | Beringer Aero | Landing gear for a light aircraft, comprising at least two wheels |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB461587A (en) | Improvements in spring suspension means for wheeled vehicles | |
| GB242599A (en) | Improvements in landing frames for aeroplanes | |
| GB526116A (en) | Improvements relating to aircraft undercarriages with resilient wheel mountings | |
| GB393445A (en) | Improvements in or relating to aircraft landing gear | |
| US2699302A (en) | Undercarriage for airplanes | |
| GB572377A (en) | Improvements in or relating to aircraft building, assembling and repairing | |
| GB602081A (en) | Improved swivel joint | |
| GB306412A (en) | Improvements in and relating to undercarriages for aircraft | |
| GB745965A (en) | Improvements in or relating to aircraft undercarriage fairings | |
| GB376634A (en) | Elastic seaplane undercarriages | |
| GB768934A (en) | Improvements in or relating to aircraft undercarriage fairings | |
| GB781059A (en) | Improvements relating to winged aerial targets | |
| GB432868A (en) | Improvements in or relating to elastic landing gear for aeroplanes | |
| GB508158A (en) | Improvements in and relating to under-carriages for aircraft | |
| GB376616A (en) | Improvements in the construction of aeroplanes and like aircraft | |
| GB491298A (en) | Improvements in or relating to landing gear for aircraft | |
| GB165773A (en) | Improvements relating to carriages for aircraft | |
| GB344207A (en) | Improvements in and relating to eyeglasses and the like | |
| GB525013A (en) | Improvements in supporting wings for aircraft | |
| GB571024A (en) | Improvements in endless track landing elements for aircraft | |
| USD144308S (en) | Fuselage for grounded aviation trainers | |
| GB300267A (en) | Improvements in supporting structures for aeroplanes | |
| GB582527A (en) | Improvements in or relating to a truss structure particularly for aircraft | |
| GB350047A (en) | Improvements in aeroplanes | |
| GB627313A (en) | Improvements in vehicle undercarriages |