GB1303663A - - Google Patents
Info
- Publication number
- GB1303663A GB1303663A GB463470A GB463470A GB1303663A GB 1303663 A GB1303663 A GB 1303663A GB 463470 A GB463470 A GB 463470A GB 463470 A GB463470 A GB 463470A GB 1303663 A GB1303663 A GB 1303663A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fluid
- undercarriage
- jack
- distributer
- door
- 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
- B64C25/18—Operating mechanisms
- B64C25/22—Operating mechanisms fluid
-
- 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
- B64C25/16—Fairings movable in conjunction with undercarriage elements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B11/00—Servomotor systems without provision for follow-up action; Circuits therefor
- F15B11/16—Servomotor systems without provision for follow-up action; Circuits therefor with two or more servomotors
- F15B11/20—Servomotor systems without provision for follow-up action; Circuits therefor with two or more servomotors controlling several interacting or sequentially-operating members
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/8593—Systems
- Y10T137/86493—Multi-way valve unit
- Y10T137/86574—Supply and exhaust
- Y10T137/8667—Reciprocating valve
- Y10T137/86694—Piston valve
- Y10T137/8671—With annular passage [e.g., spool]
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- General Engineering & Computer Science (AREA)
- Closing And Opening Devices For Wings, And Checks For Wings (AREA)
- Power-Operated Mechanisms For Wings (AREA)
- Loading And Unloading Of Fuel Tanks Or Ships (AREA)
Abstract
1303663 Retractable undercarriage for aircraft MESSIER 30 Jan 1970 [31 Jan 1969] 4634/70 Heading B7G An undercarriage leg 1 is extendible and retractable under the control of a fluid-operated jack 2 and is braced in the lowered position (Fig. 1) by a strut comprising arms 3 and 4. The arm 4 is pivoted at 41 and carries a plate 5 having a cam slot 51 which controls, via arms 6 and 7, the position of slide 73 of fluid distributer 12 also interconnected via arms 7 and 9 with catch 8 which engages member 24 to lock the undercarriage when retracted. Door 16 of the undercarriage bay is opened and closed by fluid-operated jack 23, being locked when closed by the engagement of catch 17 and roller 19, and movement of the door controls, by means of arm 15 and cam slot 141 of plate 14 the position of slide 131 of fluid distributer 13 (see Fig. 7). When the undercarriage is locked down fluid is being fed under pressure to line X to enter distributer 12 (which is in the position shown in Fig. 4) at 122 and to be passed via cavity 1226 of the distributer to cavity 232 of jack 23 to maintain the door 11 closed; line Y is connected to a fluid reservoir. In this position of the door distributer 13 causes both sides of the jack 2 to be connected to vent line 138, Fig. 7, so that the undercarriage is not actuated. In order to raise the undercarriage line X is connected to the reservoir and pressure fluid is instead fed to line Y, to pass via cavity 1227 of distributer 12 to jack 20 to release the catch 17 and to cavity 233 of the jack 23 to open the door. As soon as it has opened beyond a certain angle, a new position of distributer 13 (Fig. 8, not shown) allows fluid to pass via channels 134 and 136 to the jack 2 so as to raise the undercarriage. This causes slide 73 to assume a first new position (Fig. 5, not shown), wherein the fluid is still fed to jack 23 so as to open the door, but at reduced pressure, via narrow channel 1218 and non- return valve 1219, and then a second new position (Fig. 6, not shown), wherein the fluid is fed from cavity 1226 to cavity 232 of the jack 23 so as to close the door. The pressure fluid also causes jack 24 to close the catch 8 as the undercarriage is raised, while spring 18 closes the catch 17. In order to lower the undercarriage the connection of lines X and Y is again reversed; catches 8 and 17 are disengaged by jacks 11 and 20, respectively, and the above-described sequence is reversed.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR6902189A FR2036686B1 (en) | 1969-01-31 | 1969-01-31 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1303663A true GB1303663A (en) | 1973-01-17 |
Family
ID=9028483
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB463470A Expired GB1303663A (en) | 1969-01-31 | 1970-01-30 |
Country Status (4)
Country | Link |
---|---|
US (1) | US3652039A (en) |
DE (1) | DE2004097C3 (en) |
FR (1) | FR2036686B1 (en) |
GB (1) | GB1303663A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114215804A (en) * | 2022-02-22 | 2022-03-22 | 中国空气动力研究与发展中心高速空气动力研究所 | Electro-hydraulic servo system for driving curved knife supporting mechanism |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2061559B2 (en) * | 1969-06-27 | 1974-06-14 | Messier Hispano Sa | |
FR2529859A1 (en) * | 1982-07-12 | 1984-01-13 | Messier Hispano Sa | Integrated block for control of the landing gear for an aircraft. |
US4573649A (en) * | 1983-08-01 | 1986-03-04 | The Boeing Company | Integrated alternate gear extension and ground-crew door opening/closing system for an aircraft |
GB9802458D0 (en) | 1998-02-06 | 1998-04-01 | Normalair Garrett Ltd | Uplock assembly |
US6027070A (en) * | 1998-02-17 | 2000-02-22 | Triumph Controls, Inc. | Aircraft landing gear manual release assembly |
US6854689B1 (en) * | 2004-02-09 | 2005-02-15 | The Boeing Company | Methods and systems for operating aircraft landing gears |
DE102007032779B4 (en) * | 2007-07-13 | 2020-06-18 | Liebherr-Aerospace Lindenberg Gmbh | Locking system and method for operating a locking system |
EP2352670B1 (en) * | 2008-12-05 | 2017-03-29 | Safran Landing Systems Canada Inc. | Landing gear bay door with roller slot mechanism |
US8231078B2 (en) | 2008-12-05 | 2012-07-31 | Messier-Dowty Inc | Double hook door mechanism |
FR2980461B1 (en) * | 2011-09-26 | 2013-10-04 | Messier Bugatti Dowty | DEVICE FOR MANEUVERING THE GROUND OF A TRAPPER OF AN AIRCRAFT ENGINEER. |
EP2796673B1 (en) * | 2013-04-22 | 2018-03-07 | Hilite Germany GmbH | Central valve for a pivotable motor adjuster |
DE202015003619U1 (en) * | 2015-05-19 | 2016-08-22 | Liebherr-Aerospace Lindenberg Gmbh | Locking device of an aircraft landing gear |
US10259568B2 (en) | 2016-12-14 | 2019-04-16 | Goodrich Corporation | Non-jamming shrink latch assembly for retractable aircraft landing gear |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR965855A (en) * | 1950-09-23 | |||
FR891651A (en) * | 1943-03-03 | 1944-03-15 | Messerschmitt Boelkow Blohm | Hydraulic device for actuating landing gear or the like retractable inside the airplane as well as the flaps closing the passage openings |
US2552843A (en) * | 1948-08-23 | 1951-05-15 | Northrop Aircraft Inc | Sequence control for landing gears |
US2701695A (en) * | 1949-08-18 | 1955-02-08 | Mcdonnell Aircraft Corp | Hydraulic interlock for retractable landing gear and closure operators for the chambers therefor |
US3107886A (en) * | 1961-11-09 | 1963-10-22 | Kaman Aircraft Corp | Hydraulic system for aircraft landing gear and hydraulic actuator therefor |
US3263574A (en) * | 1964-06-15 | 1966-08-02 | Hydraulic Unit Specialities Co | Speed and directional control valve for double acting lift cylinder |
-
1969
- 1969-01-31 FR FR6902189A patent/FR2036686B1/fr not_active Expired
-
1970
- 1970-01-30 US US3652039D patent/US3652039A/en not_active Expired - Lifetime
- 1970-01-30 GB GB463470A patent/GB1303663A/en not_active Expired
- 1970-01-30 DE DE2004097A patent/DE2004097C3/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN114215804A (en) * | 2022-02-22 | 2022-03-22 | 中国空气动力研究与发展中心高速空气动力研究所 | Electro-hydraulic servo system for driving curved knife supporting mechanism |
Also Published As
Publication number | Publication date |
---|---|
US3652039A (en) | 1972-03-28 |
FR2036686B1 (en) | 1974-02-22 |
DE2004097B2 (en) | 1979-01-11 |
FR2036686A1 (en) | 1970-12-31 |
DE2004097A1 (en) | 1970-08-27 |
DE2004097C3 (en) | 1979-09-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PCNP | Patent ceased through non-payment of renewal fee |