GB1199618A - Improvements in or relating to Large-capacity Aircraft and more particularly to their Main Landing-Gear - Google Patents
Improvements in or relating to Large-capacity Aircraft and more particularly to their Main Landing-GearInfo
- Publication number
- GB1199618A GB1199618A GB5283367A GB5283367A GB1199618A GB 1199618 A GB1199618 A GB 1199618A GB 5283367 A GB5283367 A GB 5283367A GB 5283367 A GB5283367 A GB 5283367A GB 1199618 A GB1199618 A GB 1199618A
- Authority
- GB
- United Kingdom
- Prior art keywords
- retract
- wheels
- units
- cavities
- aircraft
- 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
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/34—Alighting gear characterised by elements which contact the ground or similar surface wheeled type, e.g. multi-wheeled bogies
-
- 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
- B64C25/18—Operating mechanisms
- B64C25/22—Operating mechanisms fluid
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Body Structure For Vehicles (AREA)
- Vehicle Body Suspensions (AREA)
- Vehicle Cleaning, Maintenance, Repair, Refitting, And Outriggers (AREA)
Abstract
1,199,618. Aircraft undercarriages. SUD-AVIATION SOC. NATIONALE DE CONSTRUCTIONS AERONATIQUES. 21 Nov., 1967 [8 Dec., 1966], No. 52833/67. Heading B7G. A low-wing aircraft has a retractable steerable forward undercarriage and a main landing gear comprising three units substantially side by side each comprising an independent mechanism carrying a shock-absorber 31, 46 and groundengaging elements (e.g. wheels 4a and 4c) so arranged that each unit has a similar load/ deflection relationship, the main undercarriage being retractable so that when retracted the ground-engaging elements are housed within the fuselage. When lowered the wheels 4a may be slightly behind or in front of the wheels 4c. In an illustrated embodiment the lateral units, carrying wheels 4c, retract sideways inboard, and the central units retract forwards. The lateral units retract pivoting at 40 when hydraulic jacks 51 and 54 extend and retract, respectively (Fig. 10). The central units retract when hydraulic jacks 34 and 39 retract (Fig. 11). The cavities 6, 13 into which the wheels 4a and 4c retract are below the pressurized floor of the aircraft fuselage 1. The cavities 6, 13 are separated by fore-aft beams 14 which carry closure flaps at their lower ends. The support mechanism for the lateral units retracts into cavities in the wings 2, the apertures for these cavities being closed partially by flaps carried by the mechanism and partially by flaps pivoted to the wing outboard of the pivot 40.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR86627A FR1513398A (en) | 1966-12-08 | 1966-12-08 | Improvements made to large tonnage aircraft and in particular to their main landing gear |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1199618A true GB1199618A (en) | 1970-07-22 |
Family
ID=8622148
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5283367A Expired GB1199618A (en) | 1966-12-08 | 1967-11-21 | Improvements in or relating to Large-capacity Aircraft and more particularly to their Main Landing-Gear |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE1531458A1 (en) |
FR (1) | FR1513398A (en) |
GB (1) | GB1199618A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113844643A (en) * | 2021-11-04 | 2021-12-28 | 中国商用飞机有限责任公司 | Front wheel turning load shedding mechanism |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2185537B1 (en) * | 1972-05-26 | 1974-09-27 | Messier Hispano Sa | |
FR2443369A1 (en) * | 1978-12-07 | 1980-07-04 | Messier Hispano Sa | Retractable wheel assembly for vehicle - includes pivoted leg with three stays and is ram operated |
US4917334A (en) * | 1988-09-30 | 1990-04-17 | The Boeing Company | Multiwheeled trailing type landing gear assembly |
-
1966
- 1966-12-08 FR FR86627A patent/FR1513398A/en not_active Expired
-
1967
- 1967-11-21 GB GB5283367A patent/GB1199618A/en not_active Expired
- 1967-11-22 DE DE19671531458 patent/DE1531458A1/en not_active Withdrawn
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113844643A (en) * | 2021-11-04 | 2021-12-28 | 中国商用飞机有限责任公司 | Front wheel turning load shedding mechanism |
Also Published As
Publication number | Publication date |
---|---|
DE1531458A1 (en) | 1970-02-26 |
FR1513398A (en) | 1968-02-16 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |