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 engine

Info

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
Application number
GB14026/38A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
AIR EQUIPMENT
Air Equipement SA
Original Assignee
AIR EQUIPMENT
Air Equipement SA
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by AIR EQUIPMENT, Air Equipement SA filed Critical AIR EQUIPMENT
Publication of GB514634A publication Critical patent/GB514634A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/04Aircraft 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.
GB14026/38A 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 Expired GB514634A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (3)

* Cited by examiner, † Cited by third party
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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