GB514634A - Improvements in and relating to the mounting on an aircraft of accessory apparatus to be driven from the or a propelling engine - Google Patents
Improvements in and relating to the mounting on an aircraft of accessory apparatus to be driven from the or a propelling engineInfo
- Publication number
- GB514634A GB514634A GB14026/38A GB1402638A GB514634A GB 514634 A GB514634 A GB 514634A GB 14026/38 A GB14026/38 A GB 14026/38A GB 1402638 A GB1402638 A GB 1402638A GB 514634 A GB514634 A GB 514634A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shaft
- box
- drives
- gear
- driven
- 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
- 230000008878 coupling Effects 0.000 abstract 1
- 238000010168 coupling process Methods 0.000 abstract 1
- 238000005859 coupling reaction Methods 0.000 abstract 1
- 239000012530 fluid Substances 0.000 abstract 1
- 239000000314 lubricant Substances 0.000 abstract 1
- 238000005461 lubrication Methods 0.000 abstract 1
- 230000004048 modification Effects 0.000 abstract 1
- 238000012986 modification Methods 0.000 abstract 1
- 230000010355 oscillation Effects 0.000 abstract 1
- 230000001681 protective effect Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/04—Aircraft characterised by the type or position of power plants of piston type
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Auxiliary Drives, Propulsion Controls, And Safety Devices (AREA)
Abstract
514,634. Power driven accessories. AIREQUIPEMENT. May 11. 1938, No. 14026.. Convention date, May 18, 1937. [Class 4] The mounting of all or, part of the accessory apparatus not directly necessary for the operation of the aero engine is effected on the outside . of a multi-drive gear-box fixed on. the aeroplane structure independently of the engine from which the gear-box is driven through a cardan joint allowing oscillations of the engine relative to the gear-box.' In one form, an electric 'generator 1, a high-pressure aircompresser 2, a medium-pressure air-compresser symmetrically placed with compresser2, a vacuum pump 4, also serving as a low-pressure compressor and side by side with it a hydraulic pump supplying fluid for operation of the undercarriage jacks, . are mounted on a box 6 mounted on the aircraft structure. The aeroengine drives a shaft 27, Fig. 4, which through bevel-gears 26, 29 drives a shaft 28 connected to a shaft 12 drives by a ball joint 31 and splines 32 permitting movement about the joint. The shaft 12 through splines permitting angular and axial movement and a friction coupling forming a torque-limiting device 19, Fig. 3, a shaft 15 which drives the accessories. The generator is driven through bevel gears 18, 18a, and a torquelimiting device 34 adjusted so that it only transmits the maximum torque for normally driving the generator. The shaft 15 drives two gear-wheel pumps 36 one of., which lubricates the gear-box and accessories requiring lubrication and the other pumps lubricant from the box to a reservoir. The shaft 12 is resilient.. In a modification, the shaft 12 is splined for freedom of axial movement to a ball-joint 39, Fig. 6, from which the drive is transmitted through splines 40 to the torque limiting device . A protective casing 42 is provided.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR514634X | 1937-05-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB514634A true GB514634A (en) | 1939-11-14 |
Family
ID=8914273
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB14026/38A Expired GB514634A (en) | 1937-05-18 | 1938-05-11 | Improvements in and relating to the mounting on an aircraft of accessory apparatus to be driven from the or a propelling engine |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB514634A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2432359A (en) * | 1947-12-09 | Internal-combustion turbine power | ||
CN110254730A (en) * | 2019-07-05 | 2019-09-20 | 重庆隆鑫通航发动机制造有限公司 | A kind of generator mounting device and a kind of aviation aircraft |
-
1938
- 1938-05-11 GB GB14026/38A patent/GB514634A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2432359A (en) * | 1947-12-09 | Internal-combustion turbine power | ||
CN110254730A (en) * | 2019-07-05 | 2019-09-20 | 重庆隆鑫通航发动机制造有限公司 | A kind of generator mounting device and a kind of aviation aircraft |
CN110254730B (en) * | 2019-07-05 | 2023-01-31 | 重庆隆鑫通航发动机制造有限公司 | Generator installation device and aviation aircraft |
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