Section 2: Air Brakes
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Palm Beach International Airport (PBI)
Agenda Item:~ PALM BEACH COUNTY BOARD OF COUNTY COMMISSIONERS AGENDA ITEM SUMMARY -===================================================================== Meeting Date: January 12, 2021 [ ] Consent [ X] Regular [ ] Ordinance [ ] Public Hearing Submitted By: Department of Airports ---------------------------------------------------------------------- I. EXECUTIVE BRIEF Motion and Title: Staff recommends motion to approve: a Contract for Air Service Development Consulting Services (Contract) with Ailevon Pacific Aviation Consulting LLC (Ailevon), a Florida limited liability company, commencing on February 1, 2021, and expiring on January 31, 2024, with one 24-month option to renew for an amount not to exceed $200,000 per contract year for a total not to exceed amount of $600,000 for the initial term. Summary: This Contract provides for professional and technical consulting services on an as-needed basis in support of the air service development program for the Palm Beach International Airport (PBI). Ailevon's principal place of business is Atlanta, GA. Air service development consulting services may include, but are not limited to, air service strategy and planning, airline route study and forecasting, competitive service analysis, business case development for new/expanded air service, development of incentive programs, catchment area demographic and leakage studies and analysis of air traffic demand and airfare data. The Contract provides for a not to exceed amount of $200,000 per contract year with an initial three-year term and an option to renew for an additional 24 months at the County's sole option. Due to lack of availability of qualified Small/Minority/Women Owned Business Enterprises providing the services required by this Contract, the Office of Equal Business Opportunity issued a waiver of Affirmative Procurement Initiatives on July 30, 2020. -
Hoffmann Aircraft
HOFFMANN AIRCRAFT HOFFMANN AIRCRAFT CORP P.0: Box No. 100 A-1214 Vienna Austria Phone (0 22 2/39 88 18 or 39 89 05 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS H36 DIMONA This Service and Maintenance Manual is for U.S. registered gliders. (Type Certificate Data Sheet No.: ………………….EU) Reg. No.:……………………… Ser. No.. ……………………………. Owner: …………………………………………………………………. ………………………………………………………………….. ………………………………………………………………….. Published 15 Nov 1985 Approval of translation has been done by best knowledge and judgment. In any case the original text in German language is authoritative. —1— Hoffmann General H 36 DIMONA 1. GENERAL: Table of contents Page 1. General ------------------------------------ 1 2. List of Revisions --------------------------- 2 3. System Description -------------------------- 3 4. Maintenance and Inspections --------- 23 5. Rigging ------------------------------------ 35 6. Weight and Balance --------------------------- 39 7 . Servicing ------------------------------------ 42 8. Repair ------------------------------------ 45 9. Table of consumables ------------------ 57 10. Airworthiness Limitations ------------------ 60 -2- Hoffmann Revisions H 36 Dimona 2. REVISIONS: 2. Revisions . Revision No Affected Pages Source Date Signature -3- Hoffmann Systems H 36 Dimona Description 3. SYSTEMS DESCRIPTION: Table of Contents Paragraph page 3.1 FLIGHT CONTROLS ------------------ 4 3.2 AIRBRAKES & WHEEL-BRAKES --- 5 3.3 TRIM UNIT ------------------------------- 5 3.4 FUEL SYSTEM ---------------------- 10 3.5 POWER PLANT ---------------------- -
Top 40 Singles Top 40 Albums
12 May 2008 CHART #1616 Top 40 Singles Top 40 Albums Forever Don't Hold Back Unbreakable: 2008 NZ Tour Edition 50th Anniversary 1 Chris Brown 21 The Potbelleez 1 Westlife 21 Gray Bartlett Last week 5 / 3 weeks SBME Last week 22 / 12 weeks MOS/Universal Last week 10 / 22 weeks Platinum x1 / SBME Last week 17 / 3 weeks EMI Take A Bow Stop And Stare Rockferry Past, Present, Future 2 Rihanna 22 OneRepublic 2 Duffy 22 Tiki Taane Last week 4 / 2 weeks Universal Last week 18 / 17 weeks Universal Last week 3 / 5 weeks Gold x1 / Universal Last week 22 / 25 weeks Gold x1 / DirtyDub/Rhythm/DRM... Love In This Club Tattoo Flight Of The Conchords Rejoice 3 Usher feat. Young Jeezy 23 Jordin Sparks 3 Flight Of The Conchords 23 Katherine Jenkins Last week 1 / 10 weeks Gold x1 / SBME Last week 36 / 2 weeks SBME Last week 1 / 3 weeks Gold x1 / SubPop/Rhythmethod Last week 32 / 3 weeks Universal No Air Sorry Believe Legend: The Very Best Of 4 Jordin Sparks feat. Chris Brown 24 Buckcherry 4 Geoff Sewell 24 Willie Nelson Last week 2 / 10 weeks Platinum x1 / SBME Last week 26 / 6 weeks Universal Last week 2 / 4 weeks Gold x1 / SewellMusic/Ode Last week 18 / 6 weeks Gold x1 / SBME Lollipop What Is It? Back To Black: Deluxe Edition E=MC2 5 Lil Wayne 25 Baby Bash feat. Sean Kingston 5 Amy Winehouse 25 Mariah Carey Last week 6 / 3 weeks Universal Last week 33 / 6 weeks SBME Last week 6 / 49 weeks Platinum x2 / Universal Last week 20 / 3 weeks Universal 4 Minutes Party People The Swing Sessions Watershed 6 Madonna feat. -
Air Automated Manifest System
AIR AUTOMATED MANIFEST SYSTEM FREQUENTLY ASKED QUESTIONS 1. Systems to be Used 2 2. Required and Voluntary Participation 2 3. When Air AMS Filing Required 4 4. Participant Procedures 4 5. Bond Requirements 5 6. Air AMS Documentation 6 7. Compliance Dates 7 8. Enforced Compliance Procedures – Phase 1 7 9. Enforced Compliance Procedures – Phase 2 9 10. Delivery Authorization 9 11. Split Shipments 10 12. Cargo that Fails to Arrive in the United States 11 13. Consolidated Shipments 11 14. Order of Receipt of Master and House Air Waybill 12 15. Simple and Master Air Waybill Format 12 16. House Air Waybill Format 13 17. In-bond Authorization 13 18. Permits to Transfer (Local Transfer) 15 19. Incomplete House Air Waybills 16 20. Manifest Holds 17 21. Foreign Cargo Remaining On Board (FROB) 17 22. Flights Without Cargo 18 23. Air AMS Problem Resolution 18 24. Scheduled Air AMS Downtime 19 25. Presentation of Documents 20 26. Manifest Discrepancy Reporting 20 27. Freight Report Inbound and Freight Report Change 20 28. Carrier Nomination/Agent Field 21 29. Emergency/Forced Landings 21 30. Location of Data Input 22 31. Duplicate Air Waybills 22 32. Quantity to Be Reported 22 33. Freight Status Information Messages 24 34. Carrier Codes 24 35. Company Material/Postal Mail/Letters and Documents 25 36. Code-Share Flights 25 37. Shipper/Consignee Information 27 38. Express Consignment Operations 29 1 Updated 07/25/2005 Updated Questions # 36 U.S. Customs and Border Protection (CBP) has received numerous questions concerning the regulations promulgated pursuant to the Trade Act of 2002. -
Braking Systems in Railway Vehicles
International Journal of Engineering Research & Technology (IJERT) ISSN: 2278-0181 Vol. 4 Issue01,January-2015 Braking Systems in Railway Vehicles Rakesh Chandmal Sharma1 , Manish Dhingra2, Rajeev Kumar Pathak3 1Department of Mechanical Engineering, M. M. University, Mullana (Ambala) INDIA, 2Department of Mechanical Engineering, T. M. University, Moradabad INDIA 3Department of Mechanical Engg, Rakshpal Bahahur College of Engg. and Tech., Bareilly INDIA Abstract— Brake is an essential feature in order to retard and Researchers in the past have investigated different stop the railway vehicle within minimum possible time. This aspects of braking of railway vehicle. Bureika & Mikaliunas paper presents a discussion about the different braking [1] provided the calculations for Vehicle Braking Force systems used in railway vehicles. This paper also considers Fitted with UIC Air Brake for Passenger Trains, Wagon electrodynamic and electromagnetic braking of trains, which is Braking Force Fitted with a UIC Air Brake for Freight of particular importance in high-speed trains. The calculation Trains Wagon, Braking Distance. Liudvinavicius & Lingaitis for stopping distance for railway vehicle is provided in this [2] studied different features and related mathematics of study. electrodynamic braking in high‐speed trains. Vernersson [3] developed a dimensional finite element model of block and Keywords— Air brake; Straight air brake system; Automatic air brake system; Braking distance; Brake cylinder; Brake pipe; Vacuum brake; wheel, which was coupled through a contact interface for the Brake delay time purpose of control of heat generation and also the heat partitioning at block-wheel surface through thermal contact I. INTRODUCTION resistances. Influence of temperature in wheels and brake The brakes are used on the coaches of railway trains to block at rail tread braking was analyzed under brake rig enable deceleration, control acceleration (downhill) or to conditions in the later part of study by Vernersson [4]. -
Design and Analysis of the Eddy Current Brake with the Winding Change
ISSN (Print) 1226-1750 ISSN (Online) 2233-6656 Journal of Magnetics 22(1), 23-28 (2017) https://doi.org/10.4283/JMAG.2017.22.1.023 Design and Analysis of the Eddy Current Brake with the Winding Change Sooyoung Cho1, Huai-Cong Liu1, Ju Lee1, Chang-Moo Lee2, Sung-Chul Go3, Sang-Hwan Ham4, Jong-Hyuk Woo1, and Hyung-Woo Lee5* 1Department of Electrical Engineering, Hanyang University, Seoul, 04763, Republic of Korea 2Korea Railroad Research Institute, Uiwang 16105, Republic of Korea 3Samsung Electronics Company, Ltd., Suwon, Gyeongi-do, 16677, Republic of Korea 4School of Electrical Engineering, Kyungil University, Gyeongsan, 38428, Republic of Korea 5Department of Railway Vehicle System Engineering, Korea National University of Transportation, Uiwang, 16106, Republic of Korea (Received 24 January 2017, Received in final form 16 February 2017, Accepted 21 February 2017) This paper is a study of the eddy current brake designed to replace the air brake of railway application. The eddy current brake has the advantage of being able to take a high current density compared to the other application because this brake is used for applying brakes to the rolling stock for a shorter amount of time. Also, this braking system has the merit of being able to take a high current density at low speed rather than at high speed, because the heat generated by the low speed operation is less than that of the high speed operation. This paper also presents a method of improving the output torque of the eddy current brake at low speed operation through a change of the winding as well as the basic design. -
NATIONAL ADTSSORY COMMITTEE No. 475 for AERONAUTICS +“” T= EFI'ect 03' SPLIT TIUILING-EDGE ??ING FLAPS on TEE AERODYNAMI
,.{ .. ”..-. .,-‘-} .. * _-d.& . ---- —.. -- +“” NATIONAL ADTSSORY COMMITTEE FOR AERONAUTICS No. 475 . -r..—. —— . ..> ..- >+ 1“ ... .“ T= EFI’ECT 03’ SPLIT TIUILING-EDGE ??ING FLAPS ON TEE AERODYNAMIC CHAIUIOTERISTICS OF A PARASOL MONOPLANE By Rudolf l?. Wallace .- Langley Memorial Aeronautical Laboratory “ -. t J..-,-- -. -w “-”Washington Novonber 1933 -. ..:”- . > 1 -.. L s I?.4TIOITALADVISORY COMMITTEE I’ORAERONAUTICS ——- -- . TECHNICAL NOTE NO. 475 --* —— . THE EFFECT OF SPLIT TRAILING-I!!DGE WING FLAPS ON — THE AERODYNAMIC CHARACTERISTICS OF A PARASOL MONOPLANE By Rudolf N. Wallace SUMMARY This paper presents the results of tests conducted in a the N.A.C,A, full-scale wind tunnel on a Fairchild F-22 —; airplane equipped with a special wing having split trailing- —* edge flaps. The flaps extendefl over the outer 90 pertien~----- of the wing span, and were of the fixed-b-inge” “type having a “-...2 --- width equal to 20 percent of the wing chord. The results show that with a flap setting of 590 the maximum lift of the wing was increased 42 percent, .a-gdthat the range of available gliding angies the flaps increased .— -- --4 froin 2.7° to 7.Oo. De-flection of” the split fkps did not increase the stalling angle or seriously affect the longi- tudinal baiance of the airplane. With flaps d-own”the land- .. ing speed of the airplane is decreased, but the talc-ulated clim-~ and level-flight performance is inferior to that with the normal wing. Calculations indicate that tke- ~~e:of”~ distance required to clear an obstacle 100 feet high–ig not affected ky flap settings from @to 20° hut is greatly in- creased by larger flap angles. -
AP3456 the Central Flying School (CFS) Manual of Flying: Volume 4 Aircraft Systems
AP3456 – 4-1- Hydraulic Systems CHAPTER 1 - HYDRAULIC SYSTEMS Introduction 1. Hydraulic power has unique characteristics which influence its selection to power aircraft systems instead of electrics and pneumatics, the other available secondary power systems. The advantages of hydraulic power are that: a. It is capable of transmitting very high forces. b. It has rapid and precise response to input signals. c. It has good power to weight ratio. d. It is simple and reliable. e. It is not affected by electro-magnetic interference. Although it is less versatile than present generation electric/electronic systems, hydraulic power is the normal secondary power source used in aircraft for operation of those aircraft systems which require large power inputs and precise and rapid movement. These include flying controls, flaps, retractable undercarriages and wheel brakes. Principles 2. Basic Power Transmission. A simple practical application of hydraulic power is shown in Fig 1 which depicts a closed system typical of that used to operate light aircraft wheel brakes. When the force on the master cylinder piston is increased slightly by light operation of the brake pedals, the slave piston will extend until the brake shoe contacts the brake drum. This restriction will prevent further movement of the slave and the master cylinder. However, any increase in force on the master cylinder will increase pressure in the fluid, and it will therefore increase the braking force acting on the shoes. When braking is complete, removal of the load from the master cylinder will reduce hydraulic pressure, and the brake shoe will retract under spring tension. -
Flight Manual, Sect
P I L A T U S A I R C R A F T LTD. S T A N S (Switzerland) A P P R O V E D F L I G H T M A N U A L and O P E R A T I N G M A N U A L for S A I L P L A N E MODEL PILATUS B4-PC11 Registration Serial No. *** Document No. 23-11-00-01473 June 1972 This sailplane must be operated in compliance with the present manual. This manual must be kept in the sailplane at all times. PILPTUS AIRCRAFT LTD. Flight Manual, Sect. 1-5 Techn. Publications. Page. 1. to 24 approved: Doc. No.01473 F l i g h t M a n u a l Index Sailplane Model B4-PC11 June 1972 INDEX PART 1 — FLIGHT MANUAL 1 Description Page 1.1 Distinctive Features 1 1.2 Certification Basis 1 1.3 Type Certificate 1 1.4 Technical Data 1 – 3 2 Limitations 2.1 Air Speeds (CAS) 4 2.2 Flight Load Factors 4 2.3 Operating Limits 4 2.4 Weights and C.G. Limits 5 2.5 Placards 5 – 7 2.6 Flight Instrument Markings 7 3 Controls and Procedures 3.1 Description of Controls 8 – 9 3.2 Procedures 9 – 14 4 Weight and Balance Information 4.1 Empty Weight and C.G. Location 15 – 16 4.2 State of Empty Weight and Load 16 – 17 4.3 Loading Instruction 18 – 19 4.4 Equipment 19 – 21 5 Control Surface Deflections and Adjustments 5.1 Elevator Control 22 5.2 Aileron Control 22 5.3 Rudder Control 23 5.4 Air Brake 23 5.5 Landing Gear Retracting Mechanism 24 Annex Aerobatic Figures 24A / 24B Page ii Doc. -
Nat'l Highway Traffic Safety Admin., DOT § 570.57
Nat’l Highway Traffic Safety Admin., DOT § 570.57 [(A ¥ B) / A] × 100 (c) Vacuum brake system integrity. (1) The vacuum brake system shall dem- The engine must be operating when onstrate integrity by meeting the fol- power-assisted brakes are checked. lowing requirements: (d) Brake hoses, master cylinder, tubes (i) The vacuum brake system shall and tube assemblies. Hydraulic brake provide vacuum reserve to permit one hoses shall not be mounted so as to service brake application with a brake contact the vehicle body or chassis. pedal force of 50 pounds after the en- Hoses shall not be cracked, chafed, or gine is turned off without actuating flattened. Brake tubes shall not be flat- the low vacuum indicator. tened or restricted. Brake hoses and tubes shall be attached or supported to (ii) Trailer vacuum brakes shall oper- prevent damage by vibration or abra- ate in conjunction with the truck or sion. Master cylinder shall not show truck tractor brake pedal. signs of leakage. Hose or tube protec- (2) Inspection procedure. (i) Check the tive rings or devices shall not be con- trailer vacuum system by coupling sidered part of the hose or tubing. trailer(s) to truck or truck tractor and (1) Inspection procedure. Examine vis- opening trailer shutoff valves. Start ually brake master cylinder, hoses and the engine and after allowing approxi- tubes, including front brake hoses, mately 1 minute to build up the vacu- through all wheel positions from full um, apply and release the brake pedal. left turn to full right turn for condi- In the case of trailer brakes equipped tions indicated. -
From the Outside, You Can't See Any Difference Between a Run-Flat Tire
FEATURE Few 10 Tech Drive wer blowouts Run-Flats Offer Convenience and Peace of Mind. If you had X-ray vision, you could see that the sidewall on a 3 Series run-flat is different from that of a conventional tire. Few things are more frightening to a driver than a blowout because several bad things start happening all at once. A trained, experienced driver may be able to bring his or her vehicle to a safe stop after a blowout. However, many drivers just hang on and hope for the best, or, worse, slam on the brakes. Even for an experienced driver, a blowout while driving on a highway with other vehicles nearby is scary. “Run-flat” tires, which still support the car and provide control even when air pressure is lost, greatly reduce the danger of a blowout. Although run-flats have been available for many years, interest in these tires has surged recently. BMW has offered run-flat tires as standard or optional equipment on selected models since the late 1990s. Equipped with run-flats, a BMW can be driven some distance even though the tire has no air in it. However, the maximum recommended speed for a run-flat without air is 50 mph. So, your customer can drive to your shop for tire replace - ment, just not at high speed. In addition to their other benefits, run-flats eliminate the hassle and potential risk of pulling onto the shoulder of a busy highway to replace a flat tire. These tires even offer a convenience benefit, freeing up trunk space because a spare tire and jack are not necessary with run-flats. -
Answer Document for Practice Test 1
11_559400 ch05.qxd 6/30/04 1:59 PM Page 113 - Answer Document for Practice Test 1 English Language Arts 1 A B C D 6 F G H J 11 A B C D 16 F G H J 21 A B C D 26 F G H J 2 F G H J 7 A B C D 12 F G H J 17 A B C D 22 F G H J 27 A B C D 3 A B C D 8 F G H J 13 A B C D 18 F G H J 23 A B C D 28 F G H J 4 F G H J 9 A B C D 14 F G H J 19 A B C D 24 F G H J 5 A B C D 10 F G H J 15 A B C D 20 F G H J 25 A B C D 29 30 31 - CUT HERE - 36 F G H J 41 A B C D 46 F G H J 51 A B C D 32 F G H J 37 A B C D 42 F G H J 47 A B C D 33 A B C D 38 F G H J 43 A B C D 48 F G H J 34 F G H J 39 A B C D 44 F G H J 49 A B C D 35 A B C D 40 F G H J 45 A B C D 50 F G H J 1 Use a lined 8 ⁄2 × 11 sheet of paper to write your essay.