GB145180A - Improvements in and relating to airscrews - Google Patents

Improvements in and relating to airscrews

Info

Publication number
GB145180A
GB145180A GB856419A GB856419A GB145180A GB 145180 A GB145180 A GB 145180A GB 856419 A GB856419 A GB 856419A GB 856419 A GB856419 A GB 856419A GB 145180 A GB145180 A GB 145180A
Authority
GB
United Kingdom
Prior art keywords
ring
pin
slot
hub
roots
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
GB856419A
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 GB856419A priority Critical patent/GB145180A/en
Publication of GB145180A publication Critical patent/GB145180A/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
    • B64C11/06Blade mountings for variable-pitch blades
    • B64C11/065Blade mountings for variable-pitch blades variable only when stationary

Abstract

145,180. Ireland, A. J. T. April 4. 1919. Screw propellers.-In screw propellers with cylindrical or cored roots adjustably engaging sockets in the boss, a multiple-part collar and uninterrupted ring are used to encircle the portions of the blade root. The blades are formed from two metal sheets welded together, and to the flanges 8 are secured the metal roots which are in two pieces and have half-cylindrical extensicns 11 with flanges 12, 13, Figs. 1, 2. The blades are kept in the bosses 14 of the propeller hub by two half-rings 15 which are encircled by the ring 16, a flange 18 holding the coned portion of the pieces 15 up against a corresponding bevel on the hub. At the inner end, a plain ring 20 is provided. For adjusting the pitch, the cap 21 carried by a pin 24 mounted in a curved slot has a projection 22 adapted to engage a slot 23 in the blade root. For ready adjustment, the pin 21 is engaged by a right-angled lug on a ring, the ring having a second pin which passes through a slot in the front face of the propeller hub. For securing the second pin, the washer of the securing-nut and the face of the hub are serrated. In a modification, the ring has teeth which engage pinions on the first pins. Further, the pins may be fixed at right-angles to the blade roots and project through the blade bosses and engage a radial slot in a disk on the propeller shaft. When wooden blades are employed, the root is coned and surrounded by a three part sleeve upon which the internally coned two part collar seats itself. Specification 132,070 is referred to.
GB856419A 1919-04-04 1919-04-04 Improvements in and relating to airscrews Expired GB145180A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB856419A GB145180A (en) 1919-04-04 1919-04-04 Improvements in and relating to airscrews

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB856419A GB145180A (en) 1919-04-04 1919-04-04 Improvements in and relating to airscrews

Publications (1)

Publication Number Publication Date
GB145180A true GB145180A (en) 1920-07-02

Family

ID=9854892

Family Applications (1)

Application Number Title Priority Date Filing Date
GB856419A Expired GB145180A (en) 1919-04-04 1919-04-04 Improvements in and relating to airscrews

Country Status (1)

Country Link
GB (1) GB145180A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112607003A (en) * 2020-11-25 2021-04-06 常州市长昊机械有限公司 Easily accomodate formula aviation blade
CN114348240A (en) * 2020-10-14 2022-04-15 保时捷股份公司 Ducted propeller of aircraft and aircraft

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114348240A (en) * 2020-10-14 2022-04-15 保时捷股份公司 Ducted propeller of aircraft and aircraft
CN114348240B (en) * 2020-10-14 2023-10-31 保时捷股份公司 Ducted propeller of aircraft and aircraft
CN112607003A (en) * 2020-11-25 2021-04-06 常州市长昊机械有限公司 Easily accomodate formula aviation 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

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