GB544425A - Improvements in or relating to spinners or nosings for the hubs of airscrews - Google Patents
Improvements in or relating to spinners or nosings for the hubs of airscrewsInfo
- Publication number
- GB544425A GB544425A GB1723340A GB1723340A GB544425A GB 544425 A GB544425 A GB 544425A GB 1723340 A GB1723340 A GB 1723340A GB 1723340 A GB1723340 A GB 1723340A GB 544425 A GB544425 A GB 544425A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pins
- hub
- airscrews
- spinner
- sockets
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/02—Hub construction
- B64C11/14—Spinners
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Moulds For Moulding Plastics Or The Like (AREA)
- Tires In General (AREA)
Abstract
544,425. Airscrews. CONSTANT SPEED AIRSCREWS, Ltd., and MARSHALL, F. G. Dec. 4, 1940, No. 1733. [Class 114] Spinners or nose-caps are secured to the hubs of airscrews by adopting existing features on the hub, such as bolts for connecting two halves of the hub together or the screw studs that secure the spinner support to a hub flange, to form one set of elements of a series of readily separable connections of the pin and hole or socket type. In the construction shown in Figs. 1 and 5 the bolts c connecting the hub halves a, b are extended axially to form pins d adapted to coact with sockets e which are mounted on the front spinner support f, preferably through the intermediary of rubber mountings y. The heads n of the pins d are provided with grooves m which, after the pins have been passed through the enlarged parts of bayonetlike slots o, in a locking-ring k and the locking-ring has been circumferentially displaced, are simultaneously engaged and locked in the narrower parts of the slots o, the necessary displacement of the locking-ring being effected by means of a pivoted lever p. In a modification, Fig. 4, the pins d<SP>1</SP> provided with the grooves m are formed as integral portions of screw studs i which serve to attach the front spinner support f to a flange h on the hub. In either construction, where the mounting of a spinner is concerned, co-operating pins and sockets may be arranged as required on a back hub-plate w and on an annular flange x secured to the spinner, either the pins or the sockets being supported in rubber mountings. Specifications 451,553, 485,903, 514,119 [Group XXV], 537,451 and 542,051, [Group XXV], are referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1723340A GB544425A (en) | 1940-12-04 | 1940-12-04 | Improvements in or relating to spinners or nosings for the hubs of airscrews |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1723340A GB544425A (en) | 1940-12-04 | 1940-12-04 | Improvements in or relating to spinners or nosings for the hubs of airscrews |
Publications (1)
Publication Number | Publication Date |
---|---|
GB544425A true GB544425A (en) | 1942-04-13 |
Family
ID=10091575
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1723340A Expired GB544425A (en) | 1940-12-04 | 1940-12-04 | Improvements in or relating to spinners or nosings for the hubs of airscrews |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB544425A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2504559A (en) * | 1943-08-19 | 1950-04-18 | Gen Motors Corp | Dual rotation propeller |
US8529204B2 (en) | 2008-02-26 | 2013-09-10 | Rolls-Royce Plc | Gas turbine engine having a nose cone assembly rigidly attached in an axial direction but flexible in a radial direction |
CN106828881A (en) * | 2016-12-13 | 2017-06-13 | 惠阳航空螺旋桨有限责任公司 | A kind of connector of propeller hub and radome fairing |
-
1940
- 1940-12-04 GB GB1723340A patent/GB544425A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2504559A (en) * | 1943-08-19 | 1950-04-18 | Gen Motors Corp | Dual rotation propeller |
US8529204B2 (en) | 2008-02-26 | 2013-09-10 | Rolls-Royce Plc | Gas turbine engine having a nose cone assembly rigidly attached in an axial direction but flexible in a radial direction |
CN106828881A (en) * | 2016-12-13 | 2017-06-13 | 惠阳航空螺旋桨有限责任公司 | A kind of connector of propeller hub and radome fairing |
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