GB565213A - Improvements in or relating to hydraulic jacking systems for aircraft landing gears and the like - Google Patents
Improvements in or relating to hydraulic jacking systems for aircraft landing gears and the likeInfo
- Publication number
- GB565213A GB565213A GB1572742A GB1572742A GB565213A GB 565213 A GB565213 A GB 565213A GB 1572742 A GB1572742 A GB 1572742A GB 1572742 A GB1572742 A GB 1572742A GB 565213 A GB565213 A GB 565213A
- Authority
- GB
- United Kingdom
- Prior art keywords
- piston
- cylinder
- relating
- fluid
- aircraft landing
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Actuator (AREA)
Abstract
565,213. Hydraulic jacks for aircraft. ARMANDIAS, L. S., and ASSOCIATED MESSIER INVESTMENTS, Ltd. Nov. 6,1942, No. 15727. [Class 69 (ii)] [Also in Groups XXX and XXXIII] A jack for operating undercarriages, bomb doors &c. on aircraft comprises a double-acting cylinder 38 and a piston 40 with a hollow rod in slidable telescopic communication with an accumulator chamber 53 in the cylinder, the piston being movable in one direction by supply of fluid from a pump 58 through valve devices against the accumulator pressure, and in the opposite direction either by supply of fluid or by the accumulator pressure. In another form of apparatus, the hollow piston rod extends on both sides of the piston and is open at its inner end and thus in communication with an accumulator chamber formed in the cylinder end by a partition through which the hollow rod extension slides. Piston locking means as described in Specifications 527,225 and 551,673 may be provided. Specification 485,617 also is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1572742A GB565213A (en) | 1942-11-06 | 1942-11-06 | Improvements in or relating to hydraulic jacking systems for aircraft landing gears and the like |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1572742A GB565213A (en) | 1942-11-06 | 1942-11-06 | Improvements in or relating to hydraulic jacking systems for aircraft landing gears and the like |
Publications (1)
Publication Number | Publication Date |
---|---|
GB565213A true GB565213A (en) | 1944-11-01 |
Family
ID=10064410
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1572742A Expired GB565213A (en) | 1942-11-06 | 1942-11-06 | Improvements in or relating to hydraulic jacking systems for aircraft landing gears and the like |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB565213A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2935277A (en) * | 1954-12-27 | 1960-05-03 | Siam | Bracing-strut for aircraft |
GB2000227B (en) * | 1977-06-10 | 1982-02-24 | Jungheinrich Kg | Hydraulic lifting device |
GB2192029A (en) * | 1986-04-28 | 1987-12-31 | Bt Ind Ab | A hydraulic lifting arrangement |
US5184465A (en) * | 1990-09-28 | 1993-02-09 | The Boeing Company | Landing gear drag strut actuator having self-contained pressure charge for emergency use |
-
1942
- 1942-11-06 GB GB1572742A patent/GB565213A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2935277A (en) * | 1954-12-27 | 1960-05-03 | Siam | Bracing-strut for aircraft |
GB2000227B (en) * | 1977-06-10 | 1982-02-24 | Jungheinrich Kg | Hydraulic lifting device |
GB2192029A (en) * | 1986-04-28 | 1987-12-31 | Bt Ind Ab | A hydraulic lifting arrangement |
GB2192029B (en) * | 1986-04-28 | 1990-05-23 | Bt Ind Ab | A hydraulic lifting arrangement |
US5184465A (en) * | 1990-09-28 | 1993-02-09 | The Boeing Company | Landing gear drag strut actuator having self-contained pressure charge for emergency use |
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