CA2511067C - Train d'atterrissage avec amortisseur de vibrations - Google Patents
Train d'atterrissage avec amortisseur de vibrations Download PDFInfo
- Publication number
- CA2511067C CA2511067C CA2511067A CA2511067A CA2511067C CA 2511067 C CA2511067 C CA 2511067C CA 2511067 A CA2511067 A CA 2511067A CA 2511067 A CA2511067 A CA 2511067A CA 2511067 C CA2511067 C CA 2511067C
- Authority
- CA
- Canada
- Prior art keywords
- landing gear
- housing
- fluid
- damping element
- vibration damper
- 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.)
- Active
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
- F16F9/10—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium using liquid only; using a fluid of which the nature is immaterial
- F16F9/14—Devices with one or more members, e.g. pistons, vanes, moving to and fro in chambers and using throttling effect
- F16F9/16—Devices with one or more members, e.g. pistons, vanes, moving to and fro in chambers and using throttling effect involving only straight-line movement of the effective parts
- F16F9/18—Devices with one or more members, e.g. pistons, vanes, moving to and fro in chambers and using throttling effect involving only straight-line movement of the effective parts with a closed cylinder and a piston separating two or more working spaces therein
-
- 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
- B64C25/50—Steerable undercarriages; Shimmy-damping
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F9/00—Springs, vibration-dampers, shock-absorbers, or similarly-constructed movement-dampers using a fluid or the equivalent as damping medium
- F16F9/32—Details
- F16F9/3207—Constructional features
- F16F9/3214—Constructional features of pistons
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Vibration Prevention Devices (AREA)
- Fluid-Damping Devices (AREA)
- Steering-Linkage Mechanisms And Four-Wheel Steering (AREA)
Abstract
La présente invention porte sur un train d'atterrissage doté d'un logement de train d'atterrissage et d'une tige de connexion ayant un premier et un deuxième levier de commande, le premier levier de commande étant directement ou indirectement relié au logement de train d'atterrissage et le deuxième levier de commande directement ou indirectement relié à la tige de connexion et un amortisseur de vibrations qui a un logement et un élément d'amortissement, l'élément d'amortissement étant déplaçable dans la zone remplie de liquide, préférablement une zone remplie d'huile de l'amortisseur de vibrations, de sorte que le mouvement de l'élément d'amortissement est amorti par le fluide, et le premier ou le deuxième levier de commande étant indirectement ou directement connecté au logement et l'autre levier de commande relié directement ou indirectement à l'élément d'amortissement, et un réservoir de fluide, préférablement un réservoir d'huile, qui est connecté avec la zone remplie de fluide, le réservoir de fluide étant intégré dans le logement de l'amortisseur de vibrations.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102004031992.8 | 2004-06-30 | ||
DE102004031992A DE102004031992B4 (de) | 2004-06-30 | 2004-06-30 | Flugzeugfahrwerk mit Schwingungsdämpfer |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2511067A1 CA2511067A1 (fr) | 2005-12-30 |
CA2511067C true CA2511067C (fr) | 2014-01-28 |
Family
ID=35508072
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA2511067A Active CA2511067C (fr) | 2004-06-30 | 2005-06-29 | Train d'atterrissage avec amortisseur de vibrations |
Country Status (3)
Country | Link |
---|---|
BR (1) | BRPI0502563B1 (fr) |
CA (1) | CA2511067C (fr) |
DE (1) | DE102004031992B4 (fr) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105584628B (zh) * | 2015-10-27 | 2021-03-30 | 成都飞机工业(集团)有限责任公司 | 一种护板起落架联动收放装置 |
CN105711858B (zh) * | 2016-03-22 | 2023-02-28 | 成都凯天电子股份有限公司 | 蓄压变频率装置 |
FR3056553B1 (fr) * | 2016-09-29 | 2018-10-12 | Safran Landing Systems | Atterrisseur d'aeronef equipe d'un dispositif d'attenuation de shimmy |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2651385A (en) * | 1950-04-18 | 1953-09-08 | United Aircraft Prod | Shimmy dampener |
US3499621A (en) * | 1967-09-06 | 1970-03-10 | Mc Donnell Douglas Corp | Torque linkage damper |
US5224668A (en) * | 1991-12-09 | 1993-07-06 | Mcdonnell Douglas Corporation | Torque linkage damper |
-
2004
- 2004-06-30 DE DE102004031992A patent/DE102004031992B4/de not_active Expired - Lifetime
-
2005
- 2005-06-29 CA CA2511067A patent/CA2511067C/fr active Active
- 2005-06-29 BR BRPI0502563-0A patent/BRPI0502563B1/pt active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
CA2511067A1 (fr) | 2005-12-30 |
BRPI0502563B1 (pt) | 2023-01-24 |
BRPI0502563A (pt) | 2006-02-07 |
DE102004031992B4 (de) | 2011-01-05 |
DE102004031992A1 (de) | 2006-01-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request |