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Machine translation
1. (WO2013124636) LANDING GEAR
Latest bibliographic data on file with the International Bureau   

Pub. No.:    WO/2013/124636    International Application No.:    PCT/GB2013/050391
Publication Date: 29.08.2013 International Filing Date: 19.02.2013
Chapter 2 Demand Filed:    17.06.2013    
IPC:
B64C 25/20 (2006.01), B64C 25/26 (2006.01), B64C 25/62 (2006.01)
Applicants: MESSIER-DOWTY LIMITED [GB/GB]; Cheltenham Road Gloucester Gloucestershire GL2 9QH (GB)
Inventors: SCHMIDT, Kyle; (GB)
Agent: LATHAM, Stuart; Withers & Rogers LLP 4 More London Riverside London SE1 2AU (GB)
Priority Data:
1203248.8 24.02.2012 GB
Title (EN) LANDING GEAR
(FR) TRAIN D'ATTERRISSAGE
Abstract: front page image
(EN)A landing gear (10) for an aircraft having a main fitting (12) arranged to be coupled to the aircraft and arranged to move between a stowed condition and a deployed condition and a trailing arm (14) movably coupled to the main fitting (12). A torsion spring (24) is coupled to the trailing arm (14) such that the movement of the trailing arm (14) causes torsion loading of the torsion spring (24). A stay assembly (24,26) is provided which comprises the torsion spring (24), the stay assembly (24,26) having a first condition in which it is arranged to react axial loading thereof so as to maintain the main fitting (12) in the deployed condition and a second condition in which it is arranged to permit the main fitting (12) to move between the stowed condition and the deployed condition.
(FR)L'invention concerne un train (10) d'atterrissage pour avion comprenant un organe principal (12) agencé en vue d'être couplé à l'avion et de se déplacer entre un état escamoté et un état déployé et un bras tiré (14) couplé de façon mobile à l'organe principal (12). Un ressort (24) de torsion est couplé au bras tiré (14) de telle façon que le mouvement du bras tiré (14) provoque un chargement en torsion du ressort (24) de torsion. Un ensemble contrefiche (24, 26) est incorporé, qui comporte le ressort (24) de torsion, l'ensemble contrefiche (24, 26) possédant un premier état dans lequel il est agencé en vue de réagir à son chargement axial de façon à maintenir l'organe principal (12) dans l'état déployé et un deuxième état dans lequel il est agencé en vue de permettre à l'organe principal (12) de se déplacer entre l'état escamoté et l'état déployé.
Designated States: AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, BN, BR, BW, BY, BZ, CA, CH, CL, CN, CO, CR, CU, CZ, DE, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IS, JP, KE, KG, KM, KN, KP, KR, KZ, LA, LC, LK, LR, LS, LT, LU, LY, MA, MD, ME, MG, MK, MN, MW, MX, MY, MZ, NA, NG, NI, NO, NZ, OM, PA, PE, PG, PH, PL, PT, QA, RO, RS, RU, RW, SC, SD, SE, SG, SK, SL, SM, ST, SV, SY, TH, TJ, TM, TN, TR, TT, TZ, UA, UG, US, UZ, VC, VN, ZA, ZM, ZW.
African Regional Intellectual Property Organization (BW, GH, GM, KE, LR, LS, MW, MZ, NA, RW, SD, SL, SZ, TZ, UG, ZM, ZW)
Eurasian Patent Organization (AM, AZ, BY, KG, KZ, RU, TJ, TM)
European Patent Office (AL, AT, BE, BG, CH, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HR, HU, IE, IS, IT, LT, LU, LV, MC, MK, MT, NL, NO, PL, PT, RO, RS, SE, SI, SK, SM, TR)
African Intellectual Property Organization (BF, BJ, CF, CG, CI, CM, GA, GN, GQ, GW, ML, MR, NE, SN, TD, TG).
Publication Language: English (EN)
Filing Language: English (EN)