GB104708A - Improvements in Flying Machines. - Google Patents

Improvements in Flying Machines.

Info

Publication number
GB104708A
GB104708A GB3607/16A GB360716A GB104708A GB 104708 A GB104708 A GB 104708A GB 3607/16 A GB3607/16 A GB 3607/16A GB 360716 A GB360716 A GB 360716A GB 104708 A GB104708 A GB 104708A
Authority
GB
United Kingdom
Prior art keywords
propeller
shaft
wheel
sleeve
vertical
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
GB3607/16A
Inventor
James Jesse Jackson
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB3607/16A priority Critical patent/GB104708A/en
Publication of GB104708A publication Critical patent/GB104708A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/08Helicopters with two or more rotors
    • B64C27/10Helicopters with two or more rotors arranged coaxially

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Catching Or Destruction (AREA)
  • Toys (AREA)

Abstract

104,708. Jackson, J. J. March 10, 1916. Aerial machines without aerostats; cars; propelling; planes, arrangement of. - A flying- machine comprises a body sustained by oppositely revolving propellers of adjustable pitch which can also act as a plane for supporting the machine during a gliding flight controlled by an elevator; a tractor and a steering-propeller, both of adjustable pitch, being also provided. The car is oval in plan and has a rear extension 31, and the floor 2 has a central opening 4 to allow a clear path for the down-draught of the supporting-propellers. A motor 7 drives through a clutch 21 a forward tractor 9, and a motor 8 drives through gearing 17e and a clutch 17d a propeller 12 mounted on a transverse shaft, the blades of the propeller 12 normally lying in the plane of a vertical surface 3C having a hole 29 to accommodate the propeller. The motor 8 also drives through a one-way clutch 53 a bevel-wheel 51 gearing with wheels 49, 50 mounted respectively on a vertical shaft 36 and a concentric sleeve 37 carrying the propellers 10, 11. Steering and balancing; planes, construction of. -Each propeller 10, 11 consists of inner and outer rings connected together by radial members and connected to a similar pair of rings by vertical posts. A single annular, flexible surface is supported on the radial members by links 63 and arms 62, Fig. 11, by movement of which the surface may be adjusted to form a helix or a flat annular plane. Cords 64, 65 connect the various arms 62 to two sleeves 66, 40 slidably mounted on the shaft 36 and sleeve 37 respectively. The sleeve 40 is engaged by an arm 42 adapted to be raised and lowered by a screwed shaft 46 provided with a hand-wheel 48. The sleeve 66, Fig. 7, is connected by a rod 68, accommodated in a groove in the shaft 36, to a sleeve 38 engaged by an arm 41 adapted to be raised and lowered by a screwed shaft 45 provided with a hand-wheel 47. Fig. 18 shows a modification in which the surface is connected by links 63<1> to holes 62a in levers 62<1>, the connexions being made at different distances from the fulcrum to correspond with the requited displacement of that part of the flexible surface. A surface divided into three sections may be used instead of a single surface. The tractor 9 comprises two blades 14, 15 mounted within a ring 13 on radial spindles having cranks 20, Fig. 4, connected by links 19 to a rod 18 within the propeller shaft 17. The rear end of the rod 18 has a projection passing through a slot in the shaft 17 and engaging a groove in a sleeve 27, Fig. 1, connected by rods 26 to a hand-wheel 25 which engages a screwed part of the propeller-shaft bearing. The blades of the steering-propeller 12 are adjusted by a similar rod 18, Fig. 6, having a swivelled connexion with a rack-bar 18a, which is engaged by a pinion 18b on a shaft 18c provided with a hand-wheel 18d, Fig. 1. An elevator 32, occupying a vertical position when the flight is vertical, is operated by cords 33 to control horizontal flight. Parachutes.-When the pitch of the flexible surfaces is zero, they may act as parachutes, and mechanism is provided to ensure their adjustment to that position should the motor stop. The screwed shaft 45 has a one-way clutch connexion to a sprocket-wheel 72 geared by a chain 71 to a sprocket-wheel on the propeller shaft 36, so that as the propeller reverses under the action of the air when the machine falls, the shaft 45 is rotated and adjusts the pitch of the propeller 10. A similar connexion effects the adjustment of the propeller 11.
GB3607/16A 1916-03-10 1916-03-10 Improvements in Flying Machines. Expired GB104708A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3607/16A GB104708A (en) 1916-03-10 1916-03-10 Improvements in Flying Machines.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3607/16A GB104708A (en) 1916-03-10 1916-03-10 Improvements in Flying Machines.

Publications (1)

Publication Number Publication Date
GB104708A true GB104708A (en) 1917-03-12

Family

ID=32244433

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3607/16A Expired GB104708A (en) 1916-03-10 1916-03-10 Improvements in Flying Machines.

Country Status (1)

Country Link
GB (1) GB104708A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112478125A (en) * 2020-12-11 2021-03-12 西安电子科技大学 Flight array system with autonomous flight capability

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112478125A (en) * 2020-12-11 2021-03-12 西安电子科技大学 Flight array system with autonomous flight capability

Similar Documents

Publication Publication Date Title
US2478847A (en) Convertible helicopter-airplane
US2318259A (en) Direct-lift aircraft
US2487020A (en) Helicopter
US1783458A (en) Vertical-lift airplane
US2996269A (en) Helicopter with counter-rotating propeller
US3103327A (en) Helicopter control system
US2818123A (en) Rotary wing aircraft
US1994488A (en) Direct lift aircraft
US1960141A (en) Helicopter
US2284902A (en) Airplane
GB104708A (en) Improvements in Flying Machines.
US1023233A (en) Flying-machine.
US2381417A (en) Helicopter
US1788218A (en) Helicopter
US2375592A (en) Helicopter
US1915855A (en) Airship
US1398750A (en) Aeroplane
US1688186A (en) Air vehicle
US1849766A (en) Airplane
US1721450A (en) Heavier-than-air flying machine
US2518008A (en) Convertible aircraft
US1923973A (en) Aircraft
US1040136A (en) Gyroplane.
US1754910A (en) Aeroplane
US2440003A (en) Helicopter and airplane sustained aircraft