Vistara Soars Toward Expansion New Flight-Planning Technology Enhances Safety, Cuts Costs
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Annual Report 2004 - 2005 to Be Innovative, World Class, Contemporary and Build India's Most Desirable Brands
TITAN INDUSTRIES 21 Annual Report 2004 - 2005 To be Innovative, World class, Contemporary and build India's most desirable brands X To be the most desirable jewellery brand for Indian women TITAN INDUSTRIES Twenty-first annual report 2004-2005 Board of Directors Rameshram Mishra (Chairman) Bhaskar Bhat (Managing Director) Ishaat Hussain N N Tata Farrokh Kavarana T K Balaji A C Mukherji C G Krishnadas Nair Rama Bijapurkar (upto 25 May 2005) Md. Nasimuddin (upto 4 Jan 2005) Pradeep Yadav (upto 8 June 2005) S Susai Company Secretary Usha lyengar Auditors A F Ferguson & Co. (Chartered Accountants) Bankers Canara Bank Contents Bank of Baroda Notice 2 Hongkong Bank Standard Chartered Bank Directors' Report 9 Oriental Bank of Commerce Management Discussion & Analysis 17 Union Bank of India Corporate Governance Report 25 Registered Office Auditors' Report 36 3, SIPCOT Industrial Complex Balance Sheet 40 Hosur635 126 Profit & Loss Account 41 Share Department Cash Flow Statement 42 Tata Share Registry Limited Schedules & Notes to Accounts 49 Unit:Titan Industries Limited Army & Navy Building Interest in Subsidiaries 63 148, Mahatma Gandhi Road Consolidated Accounts 65 Mumbai 400 001 Financial Statistics 91 Titan Industries is a TATA Enterprise in association with the Tamil Nadu Industrial Development Corporation TITAN INDUSTRIES Twenty-first annual report 2004-2005 Titan Industries Limited Notice The Twenty-first Annual General Meeting of Titan Industries Limited will be held at the Registered Office of the Company, at 3 SIPCOT Industrial Complex, Hosur 635 126, on Wednesday, 31 st August 2005 at 3.30 p.m. to transact the following business: 1) To receive and adopt the Directors' Report and Audited Profit and Loss Account for the year ended 31st March 2005 and the Balance Sheet as at that date together with the report of the Auditors thereon. -
Sr. No. Name of the Person Relationship
Tata Chemicals Limited List of Related party under SEBI (Listing Obligations and Disclosure Requirements) Regulations, 2015 / The Companies Act, 2013 as on 31st March, 2017 (as per IND AS 24) Listing Regulations / The Companies Act, 2013 reference Sr. Name of the Person Relationship Nature [Section 2(76) of No. CA, 2013 + Regulation 2 (zb) of LR] Directors, Key Managerial Personnel & Related Parties 1 Mr. Nasser Munjee Director (Independent, Non - Executive) 2 Mrs. Subur Ahmad Munjee Director's Relative 3 Smt. Niamat Mukhtar Munjee Director's Relative 4 Master Akbar Azaan Munjee Director's Relative 5 Smt. Sorayyah Kanji Director's Relative 6 Aarusha Homes Pvt. Ltd A private company in which a director is a member or director 7 Aga Khan Rural Support Programme, India (AKRSP,I) A private company in which a director is a member or director 8 Indian Institute of Human Settlements (Pvt Ltd) (Section 8) A private company in which a director is a member or director 9 Dr. Y.S.P. Thorat Director (Independent, Non - Executive) 10 Smt Usha Thorat Director's Relative 11 Smt Abha Thorat-Shah Director's Relative 12 Smt Aditi Thorat-Mortimer Director's Relative 13 Shri Darshak Shah Director's Relative 14 Shri Owen Mortimer Director's Relative 15 Ambit Holdings Pvt. Ltd (Merged with Ambit Private Limited) A private company in which a director is a member or director 16 Sahayog Micro Management (Pvt Ltd) (Section 8) A private company in which a director is a member or director 17 Syngenta Foundation India (Private Company) (Section 8) A private company in which a director is a member or director 18 Financial Benchmarks India Private Limited A private company in which a relative is a member or director 19 Sahayog Clean Milk Pvt. -
Swift E-Bulletin Edition 22/20-21 Week – December 14Th to December 18Th
Swift e-Bulletin Edition 22/20-21 Week – December 14th to December 18th Quote for the week: "Things work out best for those who make the best of how things work out." - John Wooden Introduction We welcome you to our weekly newsletter! The ‘Swift e-Bulletin’ - weekly newsletter, covers all regulatory updates and critical judgements passed during the week. We hope that you liked our previous editions and found it to be of great value in its content. We want this newsletter to be valuable for you so, please share your feedback and suggestions to help us improve. In the wake of COVID-19, we all are witnessing many relaxations, exemptions and amendments to the various legislations by regulatory authorities to ease out the operations during this time of crisis. Further, various regulatory authorities have been proactive in bringing significant regulatory changes in recent challenging times. This week’s newsletter covers various Circulars/notifications issued by certain regulatory authorities such as, the Ministry of Corporate Affairs (“MCA”), the Securities and Exchange Board of India (“SEBI”) and the Reserve Bank of India (“RBI”), and critical judgements and orders passed by the National Company Law Tribunal (“NCLT”), SEBI, Supreme Court and High Court. We have prepared a comprehensive summary for quick reference of the aforesaid updates and Judgements / orders issued during the week of December 14, 2020 to December 18, 2020. Thank you, Swift Team 1 Table of Contents REGULATORY UPDATES ........................................................................................................ 3 MCA UPDATES ....................................................................................................................... 3 1. MCA amends the Companies (Compromises, Arrangements and Amalgamations) Rules, 2016 vide Gazette Notification dated December 17, 2020 ............................ -
United States Patent (19) 11) Patent Number: 4,691,879 Greene 45) Date of Patent: Sep
United States Patent (19) 11) Patent Number: 4,691,879 Greene 45) Date of Patent: Sep. 8, 1987 54 JET AIRPLANE gravity. Full control of the airplane is possible under 76 Inventor: Vibert F. Greene, 19400 Sorenson high maneuverability conditions, extremely high accel Ave., Cupertino, Calif. 95014 erations and at large angles of attack. The delta nose wing creates swirling vortices that contribute substan 21 Appl. No.: 875,024 tially to the lift of the nose section. The winglet, an 22). Filed: Jun. 16, 1986 extension of the delta nose wing, allows the turbulent wake from the leading edge of the delta nose wing to 51 Int. Cl." .............................................. B64C39/08 flow over its upper surface to create additional lift while 52 U.S.C. .................................... 244/45 R; 24.4/13; the midspan wing causes the turbulent flow over its 244/45 A; 244/15 upper surface to form a turbulent wake at its leading 58 Field of Search .................. 244/45 R, 45 A, 4 R, edge. The V-tail delta wing with a V-shaped underside 244/15, 13 and blunt leading edge gives additional lift and control (56) References Cited to the airplane. A flow regulator helps to direct and U.S. PATENT DOCUMENTS control the flow field to the underside of the delta nose D. 138,538 8/1944 Clerc .................................. D12/331 wing and nose strake. There are eight pairs of control D. 155,569 10/1949 Bailey ............ ... D12/331 surfaces including an upper body stabilizer system for 3,447,76 6/1969 Whitener et al. ..................... 244/5 the control and stability of the airplane. -
Water-Tunnel and Analytical Investigation of the Effect of Strake
https://ntrs.nasa.gov/search.jsp?R=19800019803 2020-03-21T17:02:56+00:00Z NASA TP " 1676 NASA Technical Paper 1676 ,.,I c. 1 Water-Tunneland Analytical Investigation of the Effect of Strake Design Variables on Strake VortexBreakdown. Characteristics Neal T. Frink and John E. Lamar AUGUST 1980 TECH LIBRARY KAFB, NM NASA Technical Paper 1676 Water-Tunnel andAnalytical Investigation of the Effect of Strake Design Variables on Strake VortexBreakdown Characteristics Neal T. Frink andJohn E. Lamar Lavzgley Research Cetzter Haznptorz, Virgivzia National Aeronautics and Space Administration Scientific and Technical Information Branch 1980 SUMMARY A systematic water tunnel study was made to determine the vortex breakdown characteristics of43 strakes, more than half of which were generated from a new analytical strake design method. The strakes were mountedon a l/2-scale model of a Langley Research Center general research fighter fuselage mode1 with a 44O leading-edge-sweep trapezoidal wing. This study develops, in conjunction with a common wing-body, a parametric set of strake data for use in establishing and verifying a new strake design procedure. To develop this parametric data base, several series of isolated strakes were designedon the basis of a simplified approach which relates pre- scribed suction and pressure distributions in a simplified flow field to plan- form shapes. The resulting planform shapes provided examples of the effects of the pri- mary design parameters of size, span, and slenderness on the vortex breakdown characteristics. These effects are analyzed in relation to the respective strake leading-edge suction distributions. Included are examples of the effects of detailed strake planform shaping for strakes with the same general size and slenderness. -
Global Equity Fund Description Plan 3S DCP & JRA MICROSOFT CORP
Global Equity Fund June 30, 2020 Note: Numbers may not always add up due to rounding. % Invested For Each Plan Description Plan 3s DCP & JRA MICROSOFT CORP 2.5289% 2.5289% APPLE INC 2.4756% 2.4756% AMAZON COM INC 1.9411% 1.9411% FACEBOOK CLASS A INC 0.9048% 0.9048% ALPHABET INC CLASS A 0.7033% 0.7033% ALPHABET INC CLASS C 0.6978% 0.6978% ALIBABA GROUP HOLDING ADR REPRESEN 0.6724% 0.6724% JOHNSON & JOHNSON 0.6151% 0.6151% TENCENT HOLDINGS LTD 0.6124% 0.6124% BERKSHIRE HATHAWAY INC CLASS B 0.5765% 0.5765% NESTLE SA 0.5428% 0.5428% VISA INC CLASS A 0.5408% 0.5408% PROCTER & GAMBLE 0.4838% 0.4838% JPMORGAN CHASE & CO 0.4730% 0.4730% UNITEDHEALTH GROUP INC 0.4619% 0.4619% ISHARES RUSSELL 3000 ETF 0.4525% 0.4525% HOME DEPOT INC 0.4463% 0.4463% TAIWAN SEMICONDUCTOR MANUFACTURING 0.4337% 0.4337% MASTERCARD INC CLASS A 0.4325% 0.4325% INTEL CORPORATION CORP 0.4207% 0.4207% SHORT-TERM INVESTMENT FUND 0.4158% 0.4158% ROCHE HOLDING PAR AG 0.4017% 0.4017% VERIZON COMMUNICATIONS INC 0.3792% 0.3792% NVIDIA CORP 0.3721% 0.3721% AT&T INC 0.3583% 0.3583% SAMSUNG ELECTRONICS LTD 0.3483% 0.3483% ADOBE INC 0.3473% 0.3473% PAYPAL HOLDINGS INC 0.3395% 0.3395% WALT DISNEY 0.3342% 0.3342% CISCO SYSTEMS INC 0.3283% 0.3283% MERCK & CO INC 0.3242% 0.3242% NETFLIX INC 0.3213% 0.3213% EXXON MOBIL CORP 0.3138% 0.3138% NOVARTIS AG 0.3084% 0.3084% BANK OF AMERICA CORP 0.3046% 0.3046% PEPSICO INC 0.3036% 0.3036% PFIZER INC 0.3020% 0.3020% COMCAST CORP CLASS A 0.2929% 0.2929% COCA-COLA 0.2872% 0.2872% ABBVIE INC 0.2870% 0.2870% CHEVRON CORP 0.2767% 0.2767% WALMART INC 0.2767% -
4 INVENTOR 16%/6/S G
May 21, 1968 F. G., NEUBECK 3,384,326 AERODYNAMIC STRAKE Filed Aug. 24, 1965 - E - - 4 INVENTOR 16%/6/s G. MazMayaea ... it is ATTORNEYsa 3,384,326 United States Patent Office Patented May 21, 1968 1. 2 bination of parts involved in the embodiment of the inven 3,384,326 tion as will appear from the following description and AERODYNAMC STRAKE accompanying drawings, wherein: Francis G. Neubeck, Eglin Air Force Base, Fla. FIG. 1 is a front elevation of the airplane showing the (94.67 Somerset Lane, Cypress, Calif. 90630) 5 angular relationship of the strakes in relation to the ver Filed Aug. 24, 1965, Ser. No. 482,304 tical axis of the airplane; 1 Claim. (CI. 244-13) FIG. 2 is a side elevation of the airplane showing the longitudinal position of a strake; FIG. 3 is an enlarged view of the rear portion of FIG. ABSTRACT OF THE DISCLOSURE 2, and showing with greater clarity the relationship be An elongated aerodynamic strake for use on an air 0 tween the aerodynamic strake and well-known airplane plane, and being in the form of a pentahedral prominence elements; and in plan and joined to and extending from each lower FIG. 4 is an enlarged plan view of the strake only. quarter aft section of the fuselage between the trailing The aerodynamic strake 10, constituting this invention, edge of the wing and the leading edge of the horizontal 5 is joined to the exterior of the fuselage skin on airplane stabilizer to be in the upwash area for improving overall 12, as shown on FIG. -
Aerodynamic Design of the Strake for the Rocket Plane in Tailless Configuration
AERODYNAMIC DESIGN OF THE STRAKE FOR THE ROCKET PLANE IN TAILLESS CONFIGURATION. M. Figat, A. Kwiek, K. Seneńko Warsaw University of Technology Keywords: Optimization, gradient method, strake, CFD Abstract of the MAS. Moreover, the Rocket Plane is able The paper presents results of the to fly at high angles of attack. It is assumed that, aerodynamic design of the Rocket Plane in a it should be equipped with a strake. tailless configuration. It is part of a Modular Airplane System - MAS. The system is devoted to the space tourism and the Rocket Plane is the main component of the system. The main goal of the research was improving aerodynamic characteristic of the Rocket Plane. The paper presents the proposal of modification of the initial Rocket Plane geometry which is being results from the optimization process. The final geometry of the Rocket Plane is resulting of a number of optimization. 1 Introduction Fig. 1 Concept of the MAS Space tourism is a very promising and fast developing branch of an aerospace technology The mission profile of the MAS is [1]. Especially the idea of suborbital tourist presented in Fig. 2. The mission profile of the flights is a very promising concept. The main MAS consists of the following five main advantage of this type of flights is a lower price phases: [1] compare to a tourist visit on the International Take-off Space Station. During a suborbital flight the Objects separation boundary between the Earth’s atmosphere and outer space is crossed, zero gravity condition Climbing and ballistic flight appears due to parabolic trajectory. -
Effect of Wing Planform and Canard Location and Geometry on the of a Close-Coupled Canard Wing
AND NASA TECHNICAL NOTE NASA TN D-7910 o-J WING PLANFORM N75-23514 -- (NASA-TN-D-7910)- EFFECT OF AND CANARD LOCATION AND GEOMETRY ON THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A CLOSE-COUPLED CANARD WING MODEL AT Unclas 1/02 23802 SUBSONIC SPEEDS (NASA) 86 pHC $.7,5 EFFECT OF WING PLANFORM AND CANARD LOCATION AND GEOMETRY ON THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A CLOSE-COUPLED CANARD WING MO[ AT SUBSONIC SPEEDS Blair B. Gloss C; .LT Langley Research Center 0T, Hampton, Va. 23665 16 .191 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION * WASHINGTON,-D. * JUNE 1975 1. Report No. 2. Government Accession No. 3. Recipient's Catalog No. NASA TN D-7910 4. Title and Subtitle 5. Report Date EFFECT OF WING PLANFORM AND CANARD LOCATION June 1975 AND GEOMETRY ON THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A CLOSE-COUPLED CANARD WING MODEL AT SUBSONIC SPEEDS 7. Author(s) 8. Performing Organization Report No. L-9987 Blair B. Gloss 10. Work Unit No. 9. Performing Organization Name and Address 505-11-21-02 NASA Langley Research Center 11. Contract or Grant No. Hampton, Va. 23665 13. Type of Report and Period Covered 12. Sponsoring Agency Name and Address Technical Note National Aeronautics and Space Administration 14. Sponsoring Agency Code Washington, D.C. 20546 15. Supplementary Notes 16. Abstract A generalized wind-tunnel model with canard and wing planforms typical of highly maneu- verable aircraft was tested in the Langley 7- by 10-foot high-speed tunnel at a Mach number of 0.30 to determine the effect of canard location, canard size, wing sweep, and canard strake on canard-wing interference to high angles of attack. -
Tata Technology Annual Report 2021
ABOUT TATA TECHNOLOGIES Tata Technologies is a global engineering and product development digital services company focused on fulfilling its mission of helping the 7900+ world drive, fly, build and farm by enabling manufacturing clients Employees across the automotive, industrial machinery and aerospace verticals realize better products and drive efficiencies in their businesses, leading to the development of products which are better for the end customer, environment and society at large. 3 Active Regions Europe, There are two components to the company’s value proposition; the and North America first one being outsourced product engineering services for our clients helping them conceptualize, design and develop better products, and NGiNEERiN the second one is helping them identify and deploy technologies and 4 Key Industries solutions that are used to manufacture, service and realize better FOR THE NEW REALITY products. These offerings are delivered through two lines of business: a) Engineering, Research and Development (ER&D) services, and b) Automotive Aerospace Industrial Industrials Digital Enterprise Solutions which includes offerings in Connected Machinery Enterprise IT (CEIT) and Product Lifecycle Management (PLM) services and products. 17 Global Delivery Centers USA (Headcount: 371) – Troy, Detroit We are committed to ‘Engineering a better world’ through Europe (Headcount: 1247) - Warwick (UK), collaborative innovation and adoption of sustainable technologies and Gothenburg (Sweden), Brasov, Craiova & Iasi processes. Tata Technologies has over 7900+ employees serving (Romania) clients across three continents through our uniquely balanced India (Headcount: 7469) - New Delhi, Blue Ridge & on-shore/offshore global delivery model that enables us to provide Hinjawadi - Pune, Bengaluru, Thane aligned on-shore customer proximity required to support the iterative China (Headcount: 126) - Shanghai (China) nature of product development services together with the capacity SEA (Headcount: 59) - Osaka (Japan), Bangkok and cost-effectiveness of offshore locations. -
Tata Global Beverages Limited
.,.. TATA July 17, 2018 The Secretary BSE Ltd. The Secretary National Stock Exchange Corporate Relationship Calcutta Stock of India Ltd. Dept. 1st Floor, New Exchange Asscn. Ltd. Exchange Plaza.5th floor Plot Trading Wing Rotunda 7 Lyons Range No. C/1, G Block Sandra Kurla Building, PJ Towers Kolkata 700 001 Complex Sandra (E) Dalal Street Scrip Code- Mumbai 400 051 Mumbai 400 001 10000027 (Demat) Scrip Code - TATAGLOBAL Scrip Code- 500800 27 (Physical) Dear Sirs, Sub: Annual Report 2017-18 Pursuant to Regulation 34 of SEBI (Listing Obligations and Disclosure Requirements), 2015, we are attaching a copy of Annual Report for the Financial Year 2017-18. We request you to kindly take the above on record . Thanking You, Encl.: as above TATA GLOBAL BEVERAGES LIMITED Kirloskar Business Park Block-( 3rd & 4th Floor Hebbal Bengaluru-560 024 Tel 91-80·67171200 Fax 91-80 6717 1201 Registered Office 1 Bishop lefroy Road Kolkata 700 020 Corporate Identity Number (CIN) - L1 5491 W81962PLC03142S E-mail id - [email protected] Website addren - www.tataglobalbeverages.com Annual Report 2017-18 TATA TEA 1868, A SPECIALLY CURATED RANGE OF TEAS, TO CELEBRATE 150 YEARS OF TATA GROUP, DEBUTED AT WORLD ECONOMIC FORUM 2018, DAVOS MILESTONE MOMENTS TETLEY CELEBRATES 180 YEARS TATA STARBUCKS OPENS 100TH STORE IN INDIA HIMALAYAN SPARKLING ELEVATES THE FINE-DINE EXPERIENCE JAAGO RE 2.0 SUBMITS 1.8 MILLION PETITIONS TO HRD MINISTER ON WOMEN’S SAFETY AND SPORTS CULTURE Corporate Information BOARD OF DIRECTORS Committee for Special Projects N. Chandrasekaran (w.e.f. July 3, 2017) (Chairman) V. Leeladhar (Chairman) Mallika Srinivasan (Mrs.) Ranjana Kumar (Mrs.) V. -
Chapter-I Introduction
CHAPTER-I INTRODUCTION 1 INTRODUCTION Tata Group Type Private Industry Conglomerate Founded 1868 Founder(s) Jamsetji Tata Bombay,house Headquarters Mumbai, India Area served Worldwide RatanTata Key people (Chairman) Steel Automobiles Telecommunications Products Software Hotels Consumer goods 2 Revenue 319,534 crore (US$69.34 billion) Profit 8,240 crore (US$1.79 billion) Total assets US$ 52.8 billion (2009-10) Employees 396,517 (2009-10) TataSteel TataSteelEurope TataMotors TataConsultancyServices TataTechnologies TataTea Subsidiaries TitanIndustries TataPower TataCommunications TataTeleservices TataAutoCompSystemsLimited Taj Hotels Website Tata.com Tata Group Companies CMC · Tata BP Solar · Tata Coffee · Tata Chemicals · Tata Consultancy Services · Tata Elxsi · Tata Interactive Systems · Tata Motors · Tata Steel · Tata Power · Tata India-basedTea · Tata Communications · Tata Technologies Limited · Tata Teleservices · Titan Industries · Tata Voltas · The Indian Hotels Company · Trent (Westside) · Cromā 3 Brunner Mond · Jaguar Land Rover (Jaguar Cars · Land Other Rover) · Tata Daewoo Commercial Vehicle · Tata Steel Europe · Tetley · VSNL International Canada Ginger · Good Earth Teas · Tanishq · Taj Hotels · I-shakti · Tata Salt · Brands Tata Sky · Tata Indicom · Tata DoCoMo · Titan · Westside · Voltas · Virgin Mobile India Notable Jamsetji Tata · Ratanji Dadabhoy · Dorabji Tata · Nowroji People Saklatwala · J. R. D. Tata · Ratan Tata · Pallonji Mistry Bombay House is the head office of Tata Group The Tata Group is an Indian multinational conglomerate company headquartered in the Bombay House in Mumbai, India. In terms of market capitalization and revenues, Tata Group is the largest private corporate group in India. It has interests in chemicals, steel, automobiles, information technology, communication, power, beverages, and hospitality. The Tata Group has operations in more than 80 countries across six continents and its companies export products and services to 80 nations.