GB499932A - Improvements in or relating to screw propellers, particularly for aircraft - Google Patents

Improvements in or relating to screw propellers, particularly for aircraft

Info

Publication number
GB499932A
GB499932A GB1318338A GB1318338A GB499932A GB 499932 A GB499932 A GB 499932A GB 1318338 A GB1318338 A GB 1318338A GB 1318338 A GB1318338 A GB 1318338A GB 499932 A GB499932 A GB 499932A
Authority
GB
United Kingdom
Prior art keywords
sleeve
slot
blade
key
socket
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
GB1318338A
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.)
Argus Motoren GmbH
Original Assignee
Argus Motoren GmbH
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 Argus Motoren GmbH filed Critical Argus Motoren GmbH
Priority to GB1318338A priority Critical patent/GB499932A/en
Publication of GB499932A publication Critical patent/GB499932A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/02Hub construction
    • B64C11/04Blade mountings

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Friction Gearing (AREA)

Abstract

499,932. Airscrews. REISSNER, H., and ARGUS MOTOREN GES. May 3, 1938, No. 13183. [Class 114] A variable-pitch propeller in which the blades are mounted to turn freely about the longitudinal axis at right-angles to the propeller shaft, and also about a pivot disposed on a transverse axis with respect to the propeller shaft, such disposal and the distance of axis from the propeller shaft are so chosen that the blade under the combined action of the engine torque engine thrust and centrifugal force is automatically adjusted to the desired pitch. A boss 1 carries a number of adjustable sockets 2 in which is mounted a sleeve 5 turnable in relation to the socket upon the ball race 4. This sleeve 5 carries a transverse pin 7 upon which is mounted a second socket 9 to which the root 8 of the blade is attached. Adjustment of the pin within the sleeve 5 is effected by the screwed carrier 6. In an alternative the blade root 9 is provided with a sleeve carrying a number of sphericalshaped discs 13 adapted to coact with corresponding shaped discs 11, 12 carried by the sleeve 2 that is screwed in a socket in the hub. A lower spherical member 16 is provided with a transverse slot and engages a key 17 on the lower spherical surface 14. In a modification the spherical surface is reversed and the root of the blade 23 has a spherical bearing surface 21 upon a spherical surface 20 on the sleeve carrier 2. For the purpose of providing a vertical transverse axis, a pin 24 is continued inwardly and provided with a curved key engaging a slot 17 in a sleeve 16. The key may be held in place by a spring 27 so that it can be raised clear of the slot when it is desired to rotate the sleeve 16 and readjust the position of the slot. Alternative to setting the groove to fixed positions, it is possible to arrange for a relative movement during rotation as by the use of the centrifugal weight 38, the stem of which moves the key member 17, but moves it along a slightly helical path 36 whereby new settings are effective. These settings may only become effective at particular speed ranges of the plant as by providing either a very stiff spring 39 or a weak one in which case the centrifugal weight remains inoperative above or below a certain range of speeds. Alternatively, instead of an automatic centrifugal control, the control may be effected by using a piston 41 similarly coupled to the surface 17, the piston itself being moved by liquid lead thereto through a pipe 43 under the control of the pilot.
GB1318338A 1938-05-03 1938-05-03 Improvements in or relating to screw propellers, particularly for aircraft Expired GB499932A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1318338A GB499932A (en) 1938-05-03 1938-05-03 Improvements in or relating to screw propellers, particularly for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1318338A GB499932A (en) 1938-05-03 1938-05-03 Improvements in or relating to screw propellers, particularly for aircraft

Publications (1)

Publication Number Publication Date
GB499932A true GB499932A (en) 1939-01-31

Family

ID=10018346

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1318338A Expired GB499932A (en) 1938-05-03 1938-05-03 Improvements in or relating to screw propellers, particularly for aircraft

Country Status (1)

Country Link
GB (1) GB499932A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2416516A (en) * 1939-08-26 1947-02-25 Everel Propeller Corp Variable pitch propeller
US8801383B2 (en) 2011-06-29 2014-08-12 Hamilton Sundstrand Corporation Ball bearing retention for propeller blade and method of assembly
CN112520015A (en) * 2020-11-25 2021-03-19 常州市长昊机械有限公司 Convertible aviation folding blade
CN112607003A (en) * 2020-11-25 2021-04-06 常州市长昊机械有限公司 Easily accomodate formula aviation blade
CN112937837A (en) * 2021-02-05 2021-06-11 安徽羲禾航空科技有限公司 Variable pitch propeller

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2416516A (en) * 1939-08-26 1947-02-25 Everel Propeller Corp Variable pitch propeller
US8801383B2 (en) 2011-06-29 2014-08-12 Hamilton Sundstrand Corporation Ball bearing retention for propeller blade and method of assembly
CN112520015A (en) * 2020-11-25 2021-03-19 常州市长昊机械有限公司 Convertible aviation folding blade
CN112607003A (en) * 2020-11-25 2021-04-06 常州市长昊机械有限公司 Easily accomodate formula aviation blade
CN112520015B (en) * 2020-11-25 2023-06-20 常州市长昊机械有限公司 Convertible aviation folding blade
CN112607003B (en) * 2020-11-25 2023-06-20 常州市长昊机械有限公司 Easily accomodate formula aviation blade
CN112937837A (en) * 2021-02-05 2021-06-11 安徽羲禾航空科技有限公司 Variable pitch propeller
CN112937837B (en) * 2021-02-05 2024-01-05 安徽羲禾航空科技有限公司 Pitch-variable propeller

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