GB652406A - Improvements in and relating to the means for driving auxiliary parts or apparatus on board aircraft - Google Patents
Improvements in and relating to the means for driving auxiliary parts or apparatus on board aircraftInfo
- Publication number
- GB652406A GB652406A GB2644/50A GB264450A GB652406A GB 652406 A GB652406 A GB 652406A GB 2644/50 A GB2644/50 A GB 2644/50A GB 264450 A GB264450 A GB 264450A GB 652406 A GB652406 A GB 652406A
- Authority
- GB
- United Kingdom
- Prior art keywords
- box
- auxiliary
- power
- relating
- gear
- 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
-
- 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
- F16H—GEARING
- F16H57/00—General details of gearing
- F16H57/02—Gearboxes; Mounting gearing therein
- F16H57/033—Series gearboxes, e.g. gearboxes based on the same design being available in different sizes or gearboxes using a combination of several standardised units
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Details Of Gearings (AREA)
- Gear Transmission (AREA)
Abstract
652,406. Auxiliary power systems. AIREQUIPEMENT. May 18, 1945, No. 2644/50. Convention date, Sept. 7, 1942. Divided out of 652,351. [Class 4] A drive for auxiliaries on aircraft comprises a main gear-box provided with at least one auxiliary gear-box detachably mounted thereon and incorporating a number of power take-off points. As shown, a main gear-box 41 has a main driving shaft 2e and power take-offs 40f, 56a, 56b, and in addition an auxiliary gear-box 61 with four take-off points 62, 63, 64, 65. The ends of the power shafts or pinions are supported in bearings in the sides of the gearboxes and are splined internally for engagement with the auxiliary transmission shafts. The power take-offs may incorporate universal joints as described in Specification 652,407,
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR652406X | 1942-09-07 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB652406A true GB652406A (en) | 1951-04-25 |
Family
ID=9005206
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2644/50A Expired GB652406A (en) | 1942-09-07 | 1945-05-18 | Improvements in and relating to the means for driving auxiliary parts or apparatus on board aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB652406A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ITMO20110262A1 (en) * | 2011-10-18 | 2013-04-19 | Rossi S P A | GEAR REDUCER. |
-
1945
- 1945-05-18 GB GB2644/50A patent/GB652406A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ITMO20110262A1 (en) * | 2011-10-18 | 2013-04-19 | Rossi S P A | GEAR REDUCER. |
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