GB458187A - Improvements relating to retractable undercarriages for aircraft - Google Patents
Improvements relating to retractable undercarriages for aircraftInfo
- Publication number
- GB458187A GB458187A GB2029435A GB2029435A GB458187A GB 458187 A GB458187 A GB 458187A GB 2029435 A GB2029435 A GB 2029435A GB 2029435 A GB2029435 A GB 2029435A GB 458187 A GB458187 A GB 458187A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- wing
- articulated
- pivoted
- guided
- 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
- B64C25/14—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like fore-and-aft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
458,187. Aircraft alighting gear. DOWTY, G. H., Arle Court, Cheltenham. July 16, 1935, No. 20294. [Class 4] In a retractable aircraft undercarriage in which an articulated radius rod 6, 8 has one of its lengths 8 pivoted about an axis 9 for retracting or extending the undercarriage, the length 8 is formed with an arm 10 connected by a link 12 or its equivalent to the moving part 16 of a fixedly aligned jack, the part 16 being guided in the fixed alignment. As shown, a, landing wheel 2 is carried between cross braced shockabsorber members 1 articulated at 3 to the aircraft wing structure. The radius-rod 6, 8 is pivoted to the shock-absorber at 5 and to the wing at 9. The part 16 is guided on a fixed stem 15, of a hydraulic jack 14, the stem is mounted between swing spars 17, 18. The wing is provided with a lined cavity 4a to receive the wheel when retracted. Locking and indicating means may be provided.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2029435A GB458187A (en) | 1935-07-16 | 1935-07-16 | Improvements relating to retractable undercarriages for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2029435A GB458187A (en) | 1935-07-16 | 1935-07-16 | Improvements relating to retractable undercarriages for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB458187A true GB458187A (en) | 1936-12-15 |
Family
ID=10143586
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2029435A Expired GB458187A (en) | 1935-07-16 | 1935-07-16 | Improvements relating to retractable undercarriages for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB458187A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2422577A (en) * | 1942-07-15 | 1947-06-17 | Martin James | Retractable undercarriage for aircraft |
US3111292A (en) * | 1962-08-06 | 1963-11-19 | Joseph C Martin | Retractable aircraft undercarriage |
US3121547A (en) * | 1962-02-21 | 1964-02-18 | Emanuel F Paxhia | Landing gear |
FR2983170A1 (en) * | 2011-11-30 | 2013-05-31 | Airbus Operations Sas | FRONT AIRCRAFT FUSELAGE STRUCTURE COMPRISING A LANDING TRAIN |
-
1935
- 1935-07-16 GB GB2029435A patent/GB458187A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2422577A (en) * | 1942-07-15 | 1947-06-17 | Martin James | Retractable undercarriage for aircraft |
US3121547A (en) * | 1962-02-21 | 1964-02-18 | Emanuel F Paxhia | Landing gear |
US3111292A (en) * | 1962-08-06 | 1963-11-19 | Joseph C Martin | Retractable aircraft undercarriage |
FR2983170A1 (en) * | 2011-11-30 | 2013-05-31 | Airbus Operations Sas | FRONT AIRCRAFT FUSELAGE STRUCTURE COMPRISING A LANDING TRAIN |
CN103129733A (en) * | 2011-11-30 | 2013-06-05 | 空中客车营运有限公司 | Front structure of an aircraft fuselage comprising landing gear |
US8840063B2 (en) | 2011-11-30 | 2014-09-23 | Airbus Operations Sas | Front structure of an aircraft fuselage comprising landing gear |
CN103129733B (en) * | 2011-11-30 | 2015-11-04 | 空中客车营运有限公司 | Comprise the aircraft fuselage front structure of alighting gear and comprise the aircraft of this structure |
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