GB372134A - Improvements in propelling means for aircraft - Google Patents
Improvements in propelling means for aircraftInfo
- Publication number
- GB372134A GB372134A GB1770731A GB1770731A GB372134A GB 372134 A GB372134 A GB 372134A GB 1770731 A GB1770731 A GB 1770731A GB 1770731 A GB1770731 A GB 1770731A GB 372134 A GB372134 A GB 372134A
- Authority
- GB
- United Kingdom
- Prior art keywords
- class
- grooves
- aircraft
- blades
- propeller
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Catching Or Destruction (AREA)
- Sampling And Sample Adjustment (AREA)
- Toys (AREA)
Abstract
372,134. Propellers. KNOTT, R. H. JARRETT-, 37, Dalmeny Road, Tufnell Park, London. June 18, 1931, No. 17707. Addition to 332,089, [Class 114, Ships &c., Propelling &c.]. [Class 114.] To increase the effect of the propeller grooves 7 formed on the exterior of the conical boss 4 f om the base of which the blades 3 radiate, interior threads, grooves or conduits 11 of any suitable shape are provided in the interior of the boss, the streams of air entering at 10 being directed at the rear on to any suitable part of the propeller blades.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1770731A GB372134A (en) | 1931-06-18 | 1931-06-18 | Improvements in propelling means for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1770731A GB372134A (en) | 1931-06-18 | 1931-06-18 | Improvements in propelling means for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB372134A true GB372134A (en) | 1932-05-05 |
Family
ID=10099787
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1770731A Expired GB372134A (en) | 1931-06-18 | 1931-06-18 | Improvements in propelling means for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB372134A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3228475A (en) * | 1961-11-30 | 1966-01-11 | Worthmann Wilhelm | Windmill |
GB2369161A (en) * | 2000-11-20 | 2002-05-22 | Ajoy Kumar Kundu | Spinner for a propeller |
US20100021310A1 (en) * | 2008-07-28 | 2010-01-28 | Rolls-Royce Deutschland Ltd & Co Kg | Method for improving the flow conditions on the propeller or fan of an aircraft engine and accordingly designed hub cone |
US20110020109A1 (en) * | 2009-07-23 | 2011-01-27 | Jose Angel Acosta | Peripheral Tunnels Propeller |
EP2298643A3 (en) * | 2009-09-16 | 2013-04-24 | EADS Deutschland GmbH | Drive rotor with air duct |
EP3090949A1 (en) * | 2015-04-16 | 2016-11-09 | Hamilton Sundstrand Corporation | Power augmentation for an air cycle machine of an environmental control system |
-
1931
- 1931-06-18 GB GB1770731A patent/GB372134A/en not_active Expired
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3228475A (en) * | 1961-11-30 | 1966-01-11 | Worthmann Wilhelm | Windmill |
GB2369161A (en) * | 2000-11-20 | 2002-05-22 | Ajoy Kumar Kundu | Spinner for a propeller |
GB2369161B (en) * | 2000-11-20 | 2004-11-10 | Ajoy Kumar Kundu | Spinner for a propeller |
EP2151378A3 (en) * | 2008-07-28 | 2013-05-01 | Rolls-Royce Deutschland Ltd & Co KG | Method for improving the flow conditions of a propeller or fan of an airplane engine and nose cone constructed according to the method |
DE102008035160A1 (en) * | 2008-07-28 | 2010-02-04 | Rolls-Royce Deutschland Ltd & Co Kg | Method for improving the flow conditions on the propeller or fan of an aircraft engine and then trained hub cone |
EP2151378A2 (en) * | 2008-07-28 | 2010-02-10 | Rolls-Royce Deutschland Ltd & Co KG | Method for improving the flow conditions of a propeller or fan of an airplane engine and nose cone constructed according to the method |
US8221080B2 (en) | 2008-07-28 | 2012-07-17 | Rolls-Royce Deutschland Ltd & Co Kg | Method for improving the flow conditions on the propeller or fan of an aircraft engine and accordingly designed hub cone |
US20100021310A1 (en) * | 2008-07-28 | 2010-01-28 | Rolls-Royce Deutschland Ltd & Co Kg | Method for improving the flow conditions on the propeller or fan of an aircraft engine and accordingly designed hub cone |
US20110020109A1 (en) * | 2009-07-23 | 2011-01-27 | Jose Angel Acosta | Peripheral Tunnels Propeller |
US9157324B2 (en) * | 2009-07-23 | 2015-10-13 | Jose Angel Acosta | Peripheral tunnels propeller |
EP2298643A3 (en) * | 2009-09-16 | 2013-04-24 | EADS Deutschland GmbH | Drive rotor with air duct |
DE102009041667B4 (en) * | 2009-09-16 | 2016-02-18 | Airbus Defence and Space GmbH | Drive rotor with air duct |
EP3090949A1 (en) * | 2015-04-16 | 2016-11-09 | Hamilton Sundstrand Corporation | Power augmentation for an air cycle machine of an environmental control system |
US9856026B2 (en) | 2015-04-16 | 2018-01-02 | Hamilton Sundstrand Corporation | Power augmentation for an air cycle machine of an environmental control system |
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