GB566427A - Improvements in propeller hub fairings - Google Patents
Improvements in propeller hub fairingsInfo
- Publication number
- GB566427A GB566427A GB1181843A GB1181843A GB566427A GB 566427 A GB566427 A GB 566427A GB 1181843 A GB1181843 A GB 1181843A GB 1181843 A GB1181843 A GB 1181843A GB 566427 A GB566427 A GB 566427A
- Authority
- GB
- United Kingdom
- Prior art keywords
- plates
- spinner
- hub
- blade
- secured
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
566,427. Airscrew &c. spinners. DE HAVILLAND AIRCRAFT CO., Ltd., GOURLAY, G. K. L., and GAMBLE, F. W. July 20, 1943, No. 11818. [Class 114] [Also in Group XXVI] A spinner 10 is secured to the hub 12 of an airscrew, marine propeller, or fan, by means of transversely extending sector-shaped plates 28, 30 located in the spaces between the blade shanks 32 and secured at their inner and outer edges to the hub and spinner respectively. In the form shown, each blade shank 32 is sur. rounded by a frame 16 which is internally circular and externally rectangular, these frames being held firmly in position by means of plate connecting links 24. The sectorshaped plates 28, 30 are externally flanged at 29, 31 so as to be riveted or otherwise permanently secured to the spinner 10, their radial margins are riveted to flanged plates 34 and their inner edges are connected by plates 35, so as to form box-like structures between the blade-shanks 32. Interengaging dowels and sockets, and externally accessible locking devices, for detachably securing the whole spinner assembly to the hub, are illustrated and described in detail in the Specification. The sector-shaped plates 28, 30 may be formed with lightening holes 71. In the case of new propellers, the frames 16 may be replaced by flanges or the like provided initially on the limb.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1181843A GB566427A (en) | 1943-07-20 | 1943-07-20 | Improvements in propeller hub fairings |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1181843A GB566427A (en) | 1943-07-20 | 1943-07-20 | Improvements in propeller hub fairings |
Publications (1)
Publication Number | Publication Date |
---|---|
GB566427A true GB566427A (en) | 1944-12-29 |
Family
ID=9993244
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1181843A Expired GB566427A (en) | 1943-07-20 | 1943-07-20 | Improvements in propeller hub fairings |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB566427A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2780297A (en) * | 1954-03-11 | 1957-02-05 | Gen Motors Corp | Spinner construction |
US3712757A (en) * | 1969-10-28 | 1973-01-23 | Secr Defence | Bladed rotors for fluid flow machines |
US10589842B2 (en) * | 2017-05-25 | 2020-03-17 | Textron Innovations Inc. | Spinners for use on tiltrotor aircraft |
-
1943
- 1943-07-20 GB GB1181843A patent/GB566427A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2780297A (en) * | 1954-03-11 | 1957-02-05 | Gen Motors Corp | Spinner construction |
US3712757A (en) * | 1969-10-28 | 1973-01-23 | Secr Defence | Bladed rotors for fluid flow machines |
US10589842B2 (en) * | 2017-05-25 | 2020-03-17 | Textron Innovations Inc. | Spinners for use on tiltrotor aircraft |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB582152A (en) | Improvements in or relating to turbine apparatus | |
ES174918A1 (en) | IMPROVEMENTS MADE IN THE ALA PROFILES, ESPECIALLY IN THE ROTOR BLADES FOR HELICOPTERS | |
GB566427A (en) | Improvements in propeller hub fairings | |
CH257958A (en) | Device for adjusting the blades of a propeller. | |
GB619694A (en) | Improvements in or relating to rotor blades | |
GB489420A (en) | Improvements in or relating to rotary wing aircraft | |
GB586443A (en) | Improvements in or relating to rotor blades for rotary wing aircraft | |
USD138091S (en) | Rodewald airplane | |
USD144986S (en) | Prewitt helicopter | |
CH250260A (en) | Device for adjusting the blades of a propeller. | |
GB572052A (en) | Improvements in or relating to spinners for the hubs of airscrews | |
GB591499A (en) | Improvements in or relating to airfoils | |
GB569009A (en) | Improvements in and relating to the shape of bodies, fuselages, hulls and the like for air, land and sea | |
FR980312A (en) | Twin-blade propellers and rotary airfoils with split effect | |
GB545736A (en) | Improvements in airscrew spinners | |
GB372422A (en) | Improvements in flying machines | |
USD123161S (en) | Flying boat hull | |
GB551556A (en) | Improvements in or relating to metal airscrews | |
GB504493A (en) | Aeroplane | |
BURNELL | Review of the present state of knowledge concerning aerodynamics of ducted propellers | |
SCHMIDT et al. | Effect of the number of blades on the weight of an axial turbine rotor | |
GB614621A (en) | Improvements in and relating to rotative aerofoils with propulsive ducts | |
FEDORCHENKO et al. | Summation of errors in the manufacture and assembly of aircraft parts, using the limit values of the instantaneous-distribution parameters | |
BERMAN | A new approach to the solution of rotor blade dynamic problems(Matrix solution of simultaneous linear differential equations describing dynamics of two degree-of-freedom helicopter rotor blades) | |
GB495176A (en) | Improvements in rotating-wing aircraft with side-by-side rotors |