GB273745A - Improvements in retarding devices with movable planes, serving as a parachute and facilitating the landing of aeroplanes - Google Patents

Improvements in retarding devices with movable planes, serving as a parachute and facilitating the landing of aeroplanes

Info

Publication number
GB273745A
GB273745A GB17544/27A GB1754427A GB273745A GB 273745 A GB273745 A GB 273745A GB 17544/27 A GB17544/27 A GB 17544/27A GB 1754427 A GB1754427 A GB 1754427A GB 273745 A GB273745 A GB 273745A
Authority
GB
United Kingdom
Prior art keywords
planes
spider
spring
pivoted
releases
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
GB17544/27A
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
Publication of GB273745A publication Critical patent/GB273745A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/02Gyroplanes
    • B64C27/021Rotor or rotor head construction
    • B64C27/026Devices for converting a fixed wing into an autorotation rotor and viceversa

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Hinge Accessories (AREA)

Abstract

273,745. Ehmig, V., and Hofmann, F. July 1, 1926, [Convention date]. Helicopters; stopping way. - An aeroplane has a series of planes normally housed in a recess in one of the m a i n planes but adapted to be released to form a rotary retarding surface above the machine. In the case of a biplane additional surfaces are housed in the lower plane and hinge upwards into the air stream when released. Fig. 3 shows the machine after planes 7, 8 have been withdrawn from a recess 5 in the upper plane of a biplane to form a rotary retarding device, and after planes 9 have been permitted to rise against stops on the plane bracing. A streamlined central tube 3, Fig. 7, is secured to a frame 14 pivoted to the aircraft at 15 and having a pin 16 at its forward end normally locked at the lower end of a slot 17 on the aircraft frame by a hook 51. Two pairs of planes 7, 8 have central ribs pivoted respectively to two rings 12, 13 rotating about ball bearings provided on the central column. A spider 20 capable of sliding within the column has parts extending through slots 21 and carries ball races for the two rings 23, 26 carrying links 25, 27 which are pivoted to the central ribs of the planes 7, 8. Half-way slots are formed in the planes as shown in Fig. 10 to permit the passage of the links 25, 27. The spider has two projections 32 normally engaged by pivoted hooks 33, but when a cam 36 is moved by the pilot, the lower ends of the hooks are drawn together by a spring 45 to release the projections 32, and the spider 20 is raised by a spring 19 to raise the planes 7, 8. Simultaneously a spring 28 swings the pairs of planes into a position at right-angles to one another. Another cam 43 releases the hook 51 to enable the frame 14 to swing upwards until the pin 16 engages pawls 60 at the top of the slot 17 and simultaneously another hook 52 releases a spring-influenced lever 54 to turn a shaft 56 which releases the planes 9. Portions of the planes as shown at 8b, Fig. 10, may be given an inclination by varying the length of struts 61 to cause the planes 7, 8 to rotate. A screw 63 enables the spider 20 to be forced into its normal position again.
GB17544/27A 1926-07-01 1927-07-01 Improvements in retarding devices with movable planes, serving as a parachute and facilitating the landing of aeroplanes Expired GB273745A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR273745X 1926-07-01

Publications (1)

Publication Number Publication Date
GB273745A true GB273745A (en) 1928-06-21

Family

ID=8886157

Family Applications (1)

Application Number Title Priority Date Filing Date
GB17544/27A Expired GB273745A (en) 1926-07-01 1927-07-01 Improvements in retarding devices with movable planes, serving as a parachute and facilitating the landing of aeroplanes

Country Status (1)

Country Link
GB (1) GB273745A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103523199A (en) * 2013-09-29 2014-01-22 郭献民 Novel tubular-structure electric unmanned helicopter

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103523199A (en) * 2013-09-29 2014-01-22 郭献民 Novel tubular-structure electric unmanned helicopter

Similar Documents

Publication Publication Date Title
GB606022A (en) Improvements in safety or retaining devices for seats on aircraft and other vehicles
US2481502A (en) Mechanism for projecting and retracting aircraft lift rotors
GB273745A (en) Improvements in retarding devices with movable planes, serving as a parachute and facilitating the landing of aeroplanes
US2163893A (en) Autogiro rotor hub
US2052086A (en) Flying machine
US2178014A (en) Helicopter
US2681775A (en) Convertible airplane having autorotatable sustaining elements
US1464339A (en) Safety appliance for aeroplanes
US2010511A (en) Bomb sway brace
US1792014A (en) Aeroplane
US2545736A (en) Rotating wing parachute
US1765818A (en) Airplane-landing speed-retarding device
US2494367A (en) Retractable step
US2500512A (en) Wing lift modification means
US2187295A (en) Airplane
US1842637A (en) Aeroplane construction
US1719048A (en) Flying machine
US1339828A (en) Safety device or appliance for use with aeroplanes, airships, and other aircraft
US2479655A (en) Separable airplane for safe flying
US1731491A (en) Parachute for flying machines
US1889038A (en) Safety parachute for aeroplanes
US1713450A (en) Aeroplane construction
US2239670A (en) Rotating parachute
US1928560A (en) Safety device for heavier-than-air machines
US1861977A (en) Aeroplane