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A device for indicating the Mach number of a supersonic aircraft comprising an element carried by the craft and exposed to the free supersonic air stream, said element creating a shock wave during supersonic flight, the angle of the wave varying with These details and drawings of patents granted in the United States are taken, by permission of the changes in the Mach number of flight, means sensing Department of Commerce, from the 'Official Gazette of the United States Patent Office'. Printed copies the variations in the angle of said wave, and an in- of the full specifications can be obtained, price 10 cents each, from the Commissioner of Patents, dicating device responsive to said means for in- dicating the Mach number of flight. Washington, D.C., U.S.A. They are usually available for inspection at the British Patent Office, Southampton Buildings, Chancery Lane, London, W.C.2. to Lockheed Aircraft Corporation, Burbank, Calif. 2,510,698. Radio Aerial, Particularly for Aircraft Original application July 2, 1942. Serial No. 449,431. and Other Vehicles. William Arthur Johnson, Farn- borough, England, assignor to Minister of Supply in Divided and this application November 8, 1946, Serial His Majesty's Government of the United Kingdom of No. 708,484. 6 Claims. (Cl. 244-42.) Great Britain and Northern Ireland, London, Eng- land. Application July 28, 1947, Serial No. 764.098. In Great Britain January 28, 1946. Section 1, Public Law 690, August 8, 1946. Patent expires January 28, 1966. 1 Claim. l 250—33.) 2,512,902. Aircraft Altitude Control. Francis Henry S. Rossire, Leonia, N.J., assignor to Bendix Aviation Corporation, Teterboro, N.J., a corporation of Dela- 2,511,858. Method of Making Propeller Blades. ware. Application January 28, 1948. 2,510,735. Turbine Element. Walter Kenneth Glen T. Lampton, West Hartford, Conn., assignor to An altitude controller for operating the elevator Bodger, Glastonbury, Conn., assignor to United United Aircraft Corporation, East Hartford. Conn., a surface of an aircraft to automatically maintain craft Aircraft Corporation, East Hartford, Conn., a corporation of Delaware. Application April 23, 1943. flight at a predetermined altitude level comprising a corporation of Delaware. Application April 10, 1946. Serial No. 484,254. 14 Claims. (Cl. 29—156.8.) displaceable signal generator which when actuated Serial No. 661,168. 1 Claim. Cl. 253—77.) develops a signal for operating said elevator, a dis- placeable member responsive to changes in static pressure when the craft departs from said predeter- mined altitude level for actuating said generator, means for drivably connecting said generator with said pressure responsive member. 2,511,862. Propeller. Erie Martin, West Hartford, Conn., assignor to United Aircraft Corporation, East Hartford, Conn., a corporation of Delaware. Applica- 2,510,969. Foldablc and Retractable Endless Track tion April 23, 1943. Serial No. 484,229. 8 Claims. Type Landing Gears. Alfred A. Gassner, New York, (Cl. 170—159.) 2,513,325. Combustion Apparatus. Richard L. N. Y., assignor to Fairchild Engine and Aeroplane Hundstad, Pittsburgh, Pa., assignor to Wcstinghousc Corporation, New York, N.Y., a corporation of Electric Corporation, East Pittsburgh, Pa., a corpora- Maryland. Application February 23, 1949. Serial No. tion of Pennsylvania. Application August 29, 1946. 77,754. 15 Claims. (Cl. 244—102.) In combustion apparatus, wall structure defining a combustion chamber and an overlapping air space, said wall structure including an annular wall separat- ing said chamber from said air space, said annular wall having a plurality of elongated openings therein for admission of air to said chamber, flanges extend- 2,512,453. Aerofoil Construction. Herbert M. ing inwardly from the sides of said openings, and Woodhams and Sidney W. D. Lockwood, Coventry, baffles extending laterally of said openings between England, assignors to Sir W. G. Armstrong Whit- said flanges and supported by the latter. worth Aircraft Limited, Coventry, Warwickshire, England. Application July 19,1947. Serial No. 762,104. In Great Britain August 1, 1946. '2 Claims. (Cl. 244—124.) It has been suggested to us that the drawing alone gives insufficient indication of the contents of a specifica- tion and, starting with No. 2,512,790, we are therefore 2,511,502. Tailless Aeroplane. Michael E. Glu- reverting to our former practice of including an extract h-IT , Bridgeport, Conn., assignor to United Aircraft from the official abstract in each case. Corporation, East Hartford, Conn., a corporation of Delaware. Application June 5,1946. Serial No. 674,491 2,512,790. Control and Indicator for Supersonic 10 Claims. (Cl. 244—13.) Vehicles. Frank A. Cleveland, II, Pasadena, Calif., 2,514,408. Gas Turbine Apparatus. George M. assignor to Lockheed Aircraft Corporation, Burbank, Mierley, Havertown, Pa., assignor to Westinghouse Calif. Application January 9, 1948. Electric Corporation, East Pittsburgh, Pa„ a cor- poration of Pennsylvania. Application April 19, 1948. Aircraft propulsion apparatus comprising a casing structure, a rotor mounted in said casing structure, a plurality of radially extending propeller blades having base portions, a plurality of tension members inter- posed between the base portions of said blades, each of said tension members being substantially tangen- tially aligned with relation to said rotor, means connecting said rotor and each tension member inter- mediate the ends thereof, and means for securing the base portion of each blade between the abutting ends of the adjacent tension members, including a plurality of co-operating tongues formed on each of said ends, and a plurality of radial slots formed in said base portion of each corresponding blade for 2,511,504. Aeroplane Wing and Slotted Flap. receiving said tongues in interleaved relation. Willis M. Hawkins, North Hollywood, Calif., assignor 28 4 Aircraft Engineering
Aircraft Engineering and Aerospace Technology – Emerald Publishing
Published: Sep 1, 1950
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