V22 机械配件、构件 标准查询与下载

DIN EN 4198:2007 航空航天系列.耐腐蚀钢带自润滑衬垫和螺纹柄的可调自动对心滑动轴承的杆端.尺寸和载荷

This standard specifies the characteristics of adjustable rod-ends consisting of: - a self-aligning ball bearing with self-lubricating liner,EN 2501, - a rod-end with threaded shank consisting of: - a circumferential groove to identity location, - an opational longitudinal groove for locking purposes. These rod-ends are intended for use with flying control rods or rods for aerospace structures.They shall be used within the temperature range from:-55°C to 163°C.

Aerospace series - Rod-ends, adjustable self-aligning plain bearing with self-lubricating liner and threaded shank in corrosion resisting steel - Dimensions and loads; German and English version EN 4198:2006

DIN EN 4041:2007 航空航天系列.机架滚动轴承.带扩展内圈和法兰直排轴套的防腐蚀钢中刚性单列滚珠轴承.尺寸和负荷

This standard specifies the characteristics of rigid single row ball bearings in corrosion resisting steel with an extended inner ring and a solid or lightweight flanged alignment bush,designed to withstand only slow rotations and slight oscillations under load. They are intended for used in airframe fixed and moving elements and in flight control linkages. The bearings defined in this standard shall be used in the temperature range from -54°C to 150°C. However,as they are lubricated with the following greases(see EN 3727): - ester type very hihgh pressure grease(code letter A),operating range from -73°C to 121°C or, - synthetic hydrocarbons type very high pressure grease general purpose(code letter B) operating range from -54°C to 177°C. Their field of application when lubricated with code letter A grease is limited to 121°C.

Aerospace series - Bearings, airframe rolling - Rigid single row ball bearings in corrosion resisting steel, with extended inner ring and flanged alignment bush - Dimensions and loads; German and English version EN 4041:2006

DIN EN 4036:2007 航空航天系列.减小内部径向间隙的耐腐蚀钢中可调自动对心双列滚球轴承和螺纹柄的杆端.尺寸和载荷

This standard specifies the characteristics of adjustable rod ends with self-aligning double row ball bearing with reduced internal radial clearance and threaded shank in corrosion resisting steel,designed to withstand only slow rotations and oscillations under load. They consist of: - a rod end comprising: - circumferential groove to identify location; - either seals or shields; - an optional longitudinal groove for locking purpose; - an inner ring with balls. These rod ends are intended for use with flight control rods or rods for aerospace structures. They are intended to be used in the temperature range:-54°C to 150°C. However,being lubricated with the following greases: - very high pressure grease,ester type(code A),operational rages -73°C to 121°C or - very high pressure grease,synthetic hydrocarbons,general purpose(code B),operational range -54°C to 177°C(see EN 2067), their field of application when lubricated with code A grease is limited to 121°C.

Aerospace series - Rod ends, adjustable with self-aligning double row ball bearing and threaded shank in corrosion resisting steel, reduced internal radial clearance - Dimensions and loads; German and English version EN 4036:2006

DLA A-A-59701 B-2007 静电放电机械腕绳子捆扎 常规

This commercial item description (CID) covers the general requirements for electrical discharging wrist straps.

WRIST STRAP, ELECTROSTATIC DISCHARGE, GENERAL REQUIREMENTS FOR

DIN EN 3727:2007 航空航天系列.有法兰定位盖的飞机机架用滚动轴承.技术规范

Aerospace series - Bearings, airframe rolling rigid with flanged alignment housing - Technical specification; German and English version EN 3727:2006

DLA A-A-50201 A VALID NOTICE 2-2007 带盒笔和铅笔支点弹簧绘图圆规

A-A-50201A, dated 25 September 2001, has been reviewed and determined to be valid for use in acquisition.

COMPASS, DRAFTING, PIVOT, DROP SPRING BOW, PEN& PENCIL, WITH CASE

SAE AIR5937-2007 电力制动器信息

This SAE Aerospace Information Report (AIR) describes the design, operation, and attributes of electrical braking systems for both military and commercial aircraft. At this time, the document focuses only on brakes utilizing electromechanical actuators (EMAs), as that is the present state of the art. As such, the discussions herein assume that EMAs can simply replace the hydraulic actuation portion of typical brake system leaving things such as the wheel and heat sink unchanged. Furthermore, the document provides detail information from the perspective of brake system design and operation. The document also addresses failure modes, certification issues, and past development efforts. Details on the design and control of electric motors, gear train design, ball or roller screw selection are available in the reference documents and elsewhere, but are outside the scope of this document. Other all-electric technologies such as piezoelectric actuation or more exotic methods of applying drag to a rotating wheel may be included at a later time. Important: Electric braking systems for aircraft are at the early stages of production implementation. There are also a variety of control schemes that may be used to provide acceptable EMA performance. As a result, many of the details involved in the design of electric brake systems are proprietary or competition sensitive to the brake system OEMs. This AIR attempts to provide a basic technical overview of electric brakes without compromising any particular manufacturers intellectual property concerns.

Information on Electric Brakes

DIN EN 4424:2007 航空和航天.有约束力的单叉螺纹柄:1.5旋进深度×钛合金螺纹直径的可调叉形杆端.尺寸和负载

This standard specifies the characteristics of rod-ends for flight control rods. - a single fork; - a threaded shank comprising; - a circumferential groove to identify engagement; - an optional longitudinal groove locking purpuse. These rod-ends are intended for use with control rods or rods for aircraft structures.

Aerospace series - Rod-ends, adjustable, single fork and threaded shank with engagement: 1,5 × thread diameter in titanium alloys - Dimensions and loads; German and English version EN 4424:2006

DIN EN 4425:2007 航空航天系列.飞行操纵杆用耐腐蚀钢有耳垫圈

This standard specifies the characteristics of tab washers for flight control rods. These tab washers are intended to immobilise the rod end in relation to the rod body, whilst allowing a positional adjustment.#,,#

Aerospace series - Washers, tab in corrosion resisting steel for flight control rods - Dimensions; German and English version EN 4425:2006

DIN EN 2328:2007 航空航天系列.飞机控制杆用镀镉耐腐蚀钢径向锯齿托盘垫圈.尺寸

The standard specifies the characteristics of tab washers for flight control rods. These tab washers are intended to immobilise the rod end in relation to the rod body, whilst allowing a positional adjustment of 1/2 a turn.#,,#

Aerospace series - Washers, tab in corrosion resisting steel, cadmium plated, for flight control rods - Dimensions; German and English version EN 2328:2006

DIN EN 2337:2007 航空航天系列.球形滑动轴承.技术规范

Aerospace series - Spherical plain bearings - Technical specification; German and English version EN 2337:2006

ASTM E2582-07 航空航天用合成板条和检修片红外闪热成像法的标准实施规程

FT is typically used to identify flaws that occur in the manufacture of composite structures, or to track flaw development during service. Flaws detected with FT include delamination, disbonds, voids, inclusions, foreign object debris, porosity or the presence of water that is in contact with the back surface. With dedicated signal processing and the use of representative test samples, characterization of flaw depth and size, or measurement of component thickness and thermal diffusivity may be performed. Since FT is based on the diffusion of thermal energy from the inspection surface of the specimen to the opposing surface (or the depth plane of interest), the practice requires that data acquisition allows sufficient time for this process to occur, and that at the completion of the acquisition process, the radiated surface temperature signal collected by the IR camera is strong enough to be distinguished from spurious IR contributions from background sources or system noise. This method is based on accurate detection of changes in the emitted IR energy emanating from the inspection surface during the cooling process. As the emissivity of the inspection surface deviates from ideal blackbody behavior (emissivity = 1), the signal detected by the IR camera may include components that are reflected from the inspection surface. Most composite materials can be examined without special surface preparation. However, it may be necessary to coat low-emissivity, optically translucent inspection surfaces with an optically opaque, high-emissivity water-washable paint. This practice applies to the detection of flaws with aspect ratio greater than one. This practice is based on the thermal response of a specimen to a light pulse that is uniformly distributed over the plane of the inspection surface. To ensure that 1- dimensional heat flow from the surface into the sample is the primary cooling mechanism during the data acquisition period, the height and width dimensions of the heated area should be significantly greater than the thickness of the specimen, or the depth plane of interest. This practice applies to flat panels, or to curved panels where the local surface normal is less than 30 degrees from the IR camera optical axis1.1 This practice describes a procedure for detecting subsurface flaws in composite panels and repair patches using Flash Thermography (FT), in which an infrared (IR) camera is used to detect anomalous cooling behavior of a sample surface after it has been heated with a spatially uniform light pulse from a flash lamp array.1.2 This practice describes established FT test methods that are currently used by industry, and have demonstrated utility in quality assurance of composite structures during post-manufacturing and in-service examinations.1.3 This practice has utility for testing of polymer composite panels and repair patches containing, but not limited to, bismaleimide, epoxy, phenolic, poly(amide imide), polybenzimidazole, polyester (thermosetting and thermoplastic), poly(ether ether ketone), poly(ether imide), polyimide (thermosetting and thermoplastic), poly(phenylene sulfide), or polysulfone matrices; and alumina, aramid, boron, carbon, glass, quartz, or silicon carbide fibers. Typical as-fabricated geometries include uniaxial, cross ply and angle ply laminates; as well as honeycomb core sandwich core materials.1.4 This practice has utility for testing of ceramic matrix composite panels containing, but not limited to, silicon carbide, silicon nitride and carbon matrix and fibers.1.5 This practice applies to polymer or ceramic matrix composite structures with inspection surfaces that are sufficiently optically opaque to absorb incident light, and that have sufficient emissivity to allow monitoring of the surface temperature with an IR camera. Excessively thick ......

Standard Practice for Infrared Flash Thermography of Composite Panels and Repair Patches Used in Aerospace Applications

AGMA 07FTM09-2007 Ikona离合器及差动齿轮

This paper describes two devices, a clutch and a differential, which are based on the Ikona CVT. This CVT is essentially an internal gear pair, in which the pinion is mounted on an eccentric that can drive or be driven by an electric motor/generator, thus providing a variable ratio. Since this arrangement allows for “branching” of energy flow(s), it can be classified as summation-type CVT. The range of ratios depends on the input speed. For example, with an input speed of 600 -2000 rpm, the ratio can be anything from infinite to about 1:2. When the CVT is used as a clutch, it would replace the friction-plate clutch in vehicles with standard transmissions, and the fluid torque converter in automatic transmissions. In these existing devices, energy is wasted during modulation from standstill, and at every gear change, while the engine speed is altered to match the speed of the gearbox input shaft. In the case of the fluid torque converter, energy is also lost during acceleration, due to the inefficiency of the device whenever the engine speed differs from the speed of the converter output shaft. The new clutch will be referred to as the electric torque converter. Any excess energy is converted into electrical energy, and either stored in the battery, or reintroduced into the system through the motor/generator. With very efficient energy recovery, modulation of the clutch can be very smooth which is particularly advantageous when the vehicle starts from rest on uphill slopes. Since no friction element is involved, and only a fraction of torque is being manipulated, the modulation can be repeatable regardless of conditions. Finally, in a hybrid-vehicle arrangement, the clutch can be used to maintain the engine at its optimum speed (within limits), regardless of the road speed and the gearbox ratio. Similar principals apply to the Ikona differential. Unlike today’s limited slip differentials, the Ikona differential allows full torque to be transmitted through one drive wheel, even though the other drive wheel may have completely lost traction. Unlike traditional differentials that allowwheels to rotate at different speeds, the Ikona differential forces the wheels to do so. Accordingly when the vehicle is changing direction, the differential can be used to control the speed of each drive wheel, thus providing active torque steering.

The Ikona Clutch and Differential

AGMA 07FTM18-2007 锥齿轮模型

The paper presents a method for developing an accurate generic bevel gear model including both the face milling and face hobbing processes. Starting with gear blank geometry, gear and pinion basic generator machine settings are calculated. The contact pattern and rolling quality are specified and held to the second order in terms of pattern length, contact bias and motion error. Based on the setup, a grid of tooth points are found including the tooth flank, fillet and, if it exists, the undercut area. It is proposed as themodel for the next generation of bevel gear strength calculations in that the procedure produces true bevel gear geometry, uses blank design parameters as input and is vendor independent except for cutter diameter.

Bevel Gear Model

ASTM E2580-07 航空航天用平板复合材料和夹层芯材的超声波测试用标准实施规程

This practice is intended primarily for the testing of flat panel composites and sandwich core panels to an acceptance criteria most typically specified in a purchase order or other contractual document. Basis of Application8212;There are areas in this practice that require agreement between the cognizant engineering organization and the supplier, or specific direction from the cognizant engineering organization.1.1 This practice establishes two procedures for ultrasonic testing (UT) of flat panel composites and flat sandwich core panels (parallel surfaces). Typical as-fabricated lay-ups include uniaxial, cross ply and angle ply laminates; as well as honeycomb sandwich core materials. These procedures can be used throughout the life cycle of the materials; product and process design optimization, on line process control, after manufacture inspection, and in service inspection. Contact methods such as angle-beam techniques using shear waves, or surface-beam techniques using Lamb waves, are not discussed.1.2 Ultrasonic testing is a common sub surface method for detection of laminar oriented discontinuities. Two techniques can be considered based on panel surface accessibility; pulse echo for one sided and through transmission (bubblers/squirters) for two sided. As used in this practice, both require the use of a pulsed straight-beam ultrasonic longitudinal wave followed by observing indications of either the reflected (pulse-echo) or received (through transmission) wave. The general types of anomalies detected by both techniques include foreign materials, delamination, disbond/un-bond, fiber de-bonding, inclusions, porosity, and voids.1.3 This practice provides two ultrasonic test procedures. Each has its own merits and requirements for inspection and shall be selected as agreed upon in a contractual document.1.3.1 Test Procedure A, Pulse Echo (non-contacting and contacting) is at a minimum a single transducer transmitting and receiving a longitudinal wave in the range of 0.5 to 20 MHz (see Fig. 1). This procedure requires access to only one side of the specimen. This procedure can be conducted by automated or manual means. Automated and manual test results may be imaged or recorded.1.3.2 Test Procedure B, Through Transmission is a combination of two transducers. One transmits a longitudinal wave and the other receives the longitudinal wave in the range of 0.5 MHz to 20 MHz (see Fig. 2). This procedure requires access to both sides of the specimen. This procedure is automated and the examination results are recorded.1.4 This practice does not specify accept-reject criteria.This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use.

Standard Practice for Ultrasonic Testing of Flat Panel Composites and Sandwich Core Materials Used in Aerospace Applications

SAE AS85560/1A-2007 +250°F自润滑普通管套纤维增强塑料轴承

(R) BEARING, FIBER REINFORCED PLASTIC, SLEEVE, PLAIN, SELF LUBRICATING, +250 °F;TABLE 1 - DIMENSIONS;TABLE 2 - LENGTH CODES;

(R) BEARING, FIBER REINFORCED PLASTIC, SLEEVE, PLAIN, SELF LUBRICATING, +250 °F

SAE AS5368B-2007 适配器组件.3000 psi球形扩口管端锁定的端口连接环

(R) ADAPTER ASSEMBLY - PORT CONNECTION RING LOCKED TO FLARED TUBE END, 3000 PSIFIGURE 1 - ADAPTER ASSEMBLYTABLE 1A - DIMENSIONSTABLE 1B - DIMENSIONS AND WEIGHTS

(R) ADAPTER ASSEMBLY - PORT CONNECTION RING LOCKED TO FLARED TUBE END, 3000 PSI

SAE AS21432A-2007 英寸系列减少摩擦的VII型整体柱头螺栓滚道式滚针滚柱轴承

(R) BEARING, ROLLER, NEEDLE, TRACK ROLLER, INTEGRAL STUD, TYPE VII, ANTIFRICTION, INCHTABLE 1 - TOLERANCE VALUETABLE 2 IS ABOUT SIZE ETC..

(R) BEARING, ROLLER, NEEDLE, TRACK ROLLER, INTEGRAL STUD, TYPE VII, ANTIFRICTION, INCH

SAE AS21447A-2007 英寸系列减少摩擦的VII型整体柱头螺栓滚道式冠状辐射式外径滚针滚柱轴承

(R) BEARING, ROLLER, NEEDLE, TRACK ROLLER, CROWN RADIUSED O.D. INTEGRAL STUD, TYPE VII ANTIFRICTION, INCHTABLE 1 - TOLERANCE VALUES

(R) BEARING, ROLLER, NEEDLE, TRACK ROLLER, CROWN RADIUSED O.D. INTEGRAL STUD, TYPE VII ANTIFRICTION, INCH

BS EN 2335:2005 航空航天系列.无装配槽的耐腐蚀钢制普通球面轴承.尺寸和载荷

This standard specifies the characteristics of spherical plain bearings in corrosion resisting steel, without assembly slot, with or without swaging groove, with or without lubrication holes and grooves, intended for use in fixed or moving parts of aircraft structure and control mechanisms. They may be used in the temperature range from – 54 °C to 150 °C. However, as they are lubricated with the following greases (see EN 2337):  ester type very high pressure grease (code letter A), operating range from – 73 °C to 121 °C or,  synthetic hydrocarbon type very high pressure grease general purpose (code letter B), operating range from – 54 °C to 177 °C. Their field of application when lubricated with grease code letter A is limited to 121 °C.

Aerospace series — Bearings, spherical plain in corrosion resisting steel without assembly slot — Dimensions and loads