WO1997025548B1 - Dispositif retenu de freinage pour avion - Google Patents
Dispositif retenu de freinage pour avionInfo
- Publication number
- WO1997025548B1 WO1997025548B1 PCT/US1997/000889 US9700889W WO9725548B1 WO 1997025548 B1 WO1997025548 B1 WO 1997025548B1 US 9700889 W US9700889 W US 9700889W WO 9725548 B1 WO9725548 B1 WO 9725548B1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- torque tube
- wheel
- foot
- axle
- annular
- Prior art date
Links
- 230000000452 restraining Effects 0.000 claims 8
- 239000012212 insulator Substances 0.000 claims 6
- 230000002093 peripheral Effects 0.000 claims 2
- 210000001847 Jaw Anatomy 0.000 claims 1
- 230000004323 axial length Effects 0.000 claims 1
- 230000003247 decreasing Effects 0.000 claims 1
- 230000001419 dependent Effects 0.000 claims 1
- 230000002401 inhibitory effect Effects 0.000 claims 1
- 238000009434 installation Methods 0.000 claims 1
- 230000000670 limiting Effects 0.000 claims 1
- 230000000712 assembly Effects 0.000 abstract 1
Abstract
Le mouvement axial et de rotation du pied du tube tournant (49) d'un ensemble à frein à disques (10) d'un avion est retenu de sorte que la vibration haute fréquence à intervalles courts apparaissant jusqu'à maintenant lors de l'actionnement des freins, soit sensiblement amortie ou éliminée. On supprime ainsi les dommages dus aux vibrations subis par les composants de freins et de train d'atterrissage comprenant des ensembles de freinage utilisés jusqu'à maintenant.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/585,791 | 1996-01-12 | ||
US08/585,791 US5862890A (en) | 1996-01-16 | 1996-01-16 | Restrained aircraft brake apparatus |
Publications (3)
Publication Number | Publication Date |
---|---|
WO1997025548A2 WO1997025548A2 (fr) | 1997-07-17 |
WO1997025548A3 WO1997025548A3 (fr) | 1997-10-16 |
WO1997025548B1 true WO1997025548B1 (fr) | 1997-10-16 |
Family
ID=24342979
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US1997/000889 WO1997025548A2 (fr) | 1996-01-12 | 1997-01-09 | Dispositif retenu de freinage pour avion |
Country Status (2)
Country | Link |
---|---|
US (2) | US5862890A (fr) |
WO (1) | WO1997025548A2 (fr) |
Families Citing this family (39)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5862890A (en) * | 1996-01-16 | 1999-01-26 | Mcdonnell Douglas Corporation | Restrained aircraft brake apparatus |
FR2755094B1 (fr) * | 1996-10-31 | 1998-11-27 | Messier Bugatti | Agencement de disques de frein en carbone pour unite de freinage d'aeronef, et procede d'assemblage de disques selon un tel agencement |
GB2342415B (en) * | 1998-10-02 | 2000-10-04 | Dunlop Ltd | Torque transmission device |
GB2331135B (en) * | 1998-10-02 | 1999-10-13 | Dunlop Ltd | Torque transmission device |
FR2786239B1 (fr) * | 1998-11-25 | 2001-02-16 | Messier Bugatti | Dispositif de friction a disques a commande pneumatique pour transmission |
US6581730B1 (en) * | 1999-09-13 | 2003-06-24 | Goodrich Corporation | Aircraft landing gear with integrated brake actuation system |
US6349800B1 (en) * | 2000-02-07 | 2002-02-26 | Shimano Inc. | Bicycle disc brake assembly |
US6302244B1 (en) * | 2000-04-07 | 2001-10-16 | The Boeing Company | Brake squeal attenuator apparatus and method |
US6530859B2 (en) | 2001-08-10 | 2003-03-11 | Caterpillar Inc | Drive assembly with mounting for rotating axle |
US20030150674A1 (en) * | 2002-02-13 | 2003-08-14 | White Hydraulics, Inc. | Disk spring hydraulic clutch/brake |
FR2842496B1 (fr) | 2002-07-19 | 2005-02-11 | Messier Bugatti | Systeme de freinage pour roues d'aeronef |
FR2859259B1 (fr) | 2003-08-28 | 2006-02-03 | Messier Bugatti | Ensemble de freinage d'aeronef |
FR2862280B1 (fr) * | 2003-11-14 | 2006-03-03 | Messier Bugatti | Atterrisseur, frein pour roue d'aeronef, ensemble de roue freinee d'aeronef, et procede de maintenance d'un tel atterrisseur |
JP4606867B2 (ja) * | 2004-12-22 | 2011-01-05 | 株式会社荏原製作所 | シース型計測器及び軸受、並びに回転機械 |
US7331430B2 (en) * | 2006-01-05 | 2008-02-19 | Delphi Technologies, Inc. | Multi-disc brake with fixed center brake pad assembly |
US8087824B2 (en) * | 2007-07-26 | 2012-01-03 | Honeywell International Inc. | Aircraft brake assembly having a temperature probe and method of mounting a temperature probe in a brake assembly |
DE102007040156B4 (de) * | 2007-08-24 | 2013-08-29 | Shimano Inc. | Hinterer Fahrradumwerfer |
US8319384B2 (en) * | 2010-12-15 | 2012-11-27 | Honeywell International Inc. | Electromechanical brake actuator motor brake |
FR3015951B1 (fr) * | 2013-12-31 | 2017-10-06 | Messier Bugatti Dowty | Jante de roue d'aeronef a talon amovible. |
US10300740B2 (en) * | 2014-07-30 | 2019-05-28 | Honeywell International Inc. | Wheel hub bearing bore |
US9670975B1 (en) * | 2015-12-21 | 2017-06-06 | Goodrich Corporation | Torque tube damping devices and assemblies |
FR3048955B1 (fr) * | 2016-03-21 | 2020-02-07 | Safran Landing Systems | Atterrisseur d'aeronef |
FR3056671B1 (fr) * | 2016-09-26 | 2018-10-12 | Safran Landing Systems | Procede pour equiper un tube fin d'une butee d'extremite reglable par vissage |
US10180167B2 (en) | 2016-10-20 | 2019-01-15 | Bendix Spicer Foundation Brake Llc | Brake assembly apparatus for a vehicle braking system |
US9989112B1 (en) | 2017-02-24 | 2018-06-05 | Akebono Brake Industry Co., Ltd | Caliper housing having a mass damper |
US10228030B2 (en) * | 2017-05-15 | 2019-03-12 | Goodrich Corporation | Multi-disk brake assembly with travel limit pin |
US10473171B2 (en) | 2017-05-15 | 2019-11-12 | Goodrich Corporation | Extended torque tube |
US10598209B2 (en) * | 2017-09-08 | 2020-03-24 | Goodrich Corporation | Aircraft brake torque load reaction through landing gear bogie structure |
US10145429B1 (en) * | 2017-09-08 | 2018-12-04 | Goodrich Corporation | Aircraft brake torque and clamp force reaction through landing gear structure |
US10309468B2 (en) * | 2017-10-20 | 2019-06-04 | Goodrich Corporation | Torque plate barrel having blended barrel support pedestal |
US10408290B2 (en) * | 2018-02-08 | 2019-09-10 | Goodrich Corporation | Insulated torque plate foot assembly |
FR3083579B1 (fr) * | 2018-07-06 | 2020-11-27 | Safran Landing Systems | Bague de centrage anti-vibration pour pied de tube de torsion d'un frein d'aeronef et frein equipe d'une telle bague |
EP3597496B1 (fr) | 2018-07-16 | 2020-09-02 | Safran Landing Systems UK Limited | Ensemble de train d'atterrissage d'aeronef |
FR3085453B1 (fr) * | 2018-08-29 | 2020-11-20 | Safran Landing Systems | Disque arriere d’une pile de disques en carbone de frein d’aeronef equipe de plots, et frein faisant application |
US11644071B2 (en) | 2019-07-08 | 2023-05-09 | Honeywell International Inc. | Rotor drive key assembly |
CN110203380B (zh) * | 2019-07-08 | 2024-02-23 | 西安航空制动科技有限公司 | 一种用于飞机刹车装置的整体式隔热屏 |
US11274715B2 (en) | 2019-07-16 | 2022-03-15 | Goodrich Corporation | Heat shield retainer and methods |
US11231081B2 (en) | 2019-10-09 | 2022-01-25 | Goodrich Corporation | Heat shield grommet |
US11834155B2 (en) * | 2021-03-23 | 2023-12-05 | Goodrich Corporation | Landing gear wheel retention device |
Family Cites Families (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2875855A (en) * | 1953-09-28 | 1959-03-03 | Bendix Aviat Corp | Wheel and brake assembly for aircraft landing gear |
US3351157A (en) * | 1965-12-23 | 1967-11-07 | Claveau Emile | Brake systems for motor vehicles |
US3357519A (en) * | 1966-03-21 | 1967-12-12 | Bendix Corp | Aircraft brake damper mechanism |
US3368653A (en) * | 1966-05-26 | 1968-02-13 | Bendix Corp | Aircraft brake damper mechanism |
US3845919A (en) * | 1974-01-07 | 1974-11-05 | Boeing Co | Landing gear truck pitch damping |
DE2840346C2 (de) * | 1978-09-15 | 1980-09-18 | Siemens Ag, 1000 Berlin Und 8000 Muenchen | Aus Schaltern, Kondensatoren und Verstärkern bestehendes Filter für elektrische Schwingungen |
US4290505A (en) * | 1979-10-29 | 1981-09-22 | Mcdonnell Douglas Corp. | Pin centered brake |
US4383594A (en) * | 1981-06-08 | 1983-05-17 | Goodyear Aerospace Corporation | Configuration for a disk brake torque tube assembly having replaceable keys and backplate |
DE3211366C2 (de) * | 1982-03-27 | 1985-05-30 | Zahnradfabrik Friedrichshafen Ag, 7990 Friedrichshafen | Federspeicherbremse mit druckmittelbetätigbarer Lüfteinrichtung |
US4805744A (en) * | 1982-09-24 | 1989-02-21 | Pringle William L | Brake actuator assembly and method |
FR2548303B1 (fr) * | 1983-06-30 | 1985-10-25 | Dba | Perfectionnements apportes aux freins multidisques |
US4944370A (en) * | 1989-03-27 | 1990-07-31 | Allied-Signal Inc. | Drum drive for use with multiple disc brakes |
US5035305A (en) * | 1989-10-02 | 1991-07-30 | Caterpillar Inc. | Cushioned brake assembly |
US5255761A (en) * | 1989-12-21 | 1993-10-26 | The B. F. Goodrich Company | Aircraft brake |
US5205832A (en) * | 1990-04-06 | 1993-04-27 | Tuman David H | Endo-tracheal tube support device |
US5062503A (en) * | 1990-09-19 | 1991-11-05 | Allied-Signal Inc. | Ablative brake bushing for axle thermal protection |
US5205382A (en) * | 1990-10-09 | 1993-04-27 | The B. F. Goodrich Company | Aircraft brake |
US5107968A (en) * | 1991-02-12 | 1992-04-28 | The B. F. Goodrich Company | Heatshield for aircraft brake |
US5143184A (en) * | 1991-02-14 | 1992-09-01 | Allied-Signal Inc. | Carbon composite brake disc with positive vibration damping |
US5323881A (en) * | 1992-04-17 | 1994-06-28 | Aircraft Braking Systems Corporation | Configuration for a disk brake torque tube |
US5402865A (en) * | 1993-07-01 | 1995-04-04 | Alliedsignal Inc. | Aircraft brake assembly retention mechanism |
US5437352A (en) * | 1993-07-01 | 1995-08-01 | Alliedsignal Inc. | Aircraft brake torque transfer assembly |
GB9322877D0 (en) * | 1993-11-05 | 1993-12-22 | Dunlop Ltd | Multi-disc brake |
US5485898A (en) * | 1994-06-22 | 1996-01-23 | Alliedsignal Inc. | Spacer member for aircraft brakes |
US5494138A (en) * | 1994-10-14 | 1996-02-27 | Alliedsignal, Inc. | Aircraft brake torque transfer assembly |
US5579873A (en) * | 1995-01-25 | 1996-12-03 | New York Air Brake Corporation | Brake actuator vibration isolation system |
US5862890A (en) * | 1996-01-16 | 1999-01-26 | Mcdonnell Douglas Corporation | Restrained aircraft brake apparatus |
-
1996
- 1996-01-16 US US08/585,791 patent/US5862890A/en not_active Expired - Lifetime
-
1997
- 1997-01-09 WO PCT/US1997/000889 patent/WO1997025548A2/fr active Application Filing
- 1997-07-08 US US08/889,245 patent/US6003641A/en not_active Expired - Lifetime
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