ICS GUIDE TO HELICOPTER-SHIP OPERATION 4TH EDITION

ICS GUIDE TO HELICOPTER-SHIP OPERATION 4TH EDITION
ICS GUIDE TO HELICOPTER-SHIP OPERATION 4TH EDITION

4 GENERAL SHIP REQUIREMENTS

4.1 SHIP OPERATING AREAS

Note: When "D" is used in the following text, it represents the extent of the available

operating area on or above the deck of the ship. Only helicopters whose maximum overall

length with rotors turning is D or less (see Appendix A) may be used for operations to the

ship in question.

4.1.1 Types of Operating Area

Ship operating areas fall into two distinct types:

a. Landing Area: defined as an operating area suitable for landing helicopters. The landing area may consist of a purpose built structure located above the ship's deck (referred to as a "purpose built landing area") or a non purpose built area located on the ship's deck (referred to as a "non

purpose built landing area"). The landing area may be located on or over the bow or stern of the ship, have an over-side or ship's side location, or occupy an area amidships - usually on or near to the ship's centreline. The landing area may also be used for winching operations provided that the

winching criteria described in paragraph 4.1.3 below can be satisfied. However, where a landing

area with adequate size and obstacle clearance for the helicopter in question is provided, landing

is always the preferred option.

b. Winching Area: defined as an operating area which may only be used for winching operations.

The guidance in Sections 4.1 and 4.2 will assist ship operators when deciding upon the most

suitable location for a landing or winching area on their ship. The optimum position for a landing

or winching area will normally be determined by the availability of a suitable space on the ship.

However, where there is more than one area identified and capable of accommodating the type of

helicopter(s) expected to be used, the ship's master, in consultation with the helicopter operator, should assess the merits of each location, taking particular account of the size and position of

obstacles and expected aerodynamic and ship motion effects (see Section 4.2).

4.1.2 Location and Size of Operating Area - Landing

4.1.2.1 Landing Area at the Ship's Side

A non purpose built landing area located on a ship's side should consist of a "clear zone" and a

"manoeuvring zone" as shown in Figure 4.1.

The clear zone should be capable of containing a circle with a minimum diameter of 1 x D. No

objects should be located within the clear zone except aids whose presence is essential for the safe operation of the helicopter, and then only up to a maximum height of 2.5 cm. Such objects should

only be present if they do not represent a hazard to helicopters. Where there are immoveable fixed objects located in the clear zone such as a "Butterworth lid", these should be marked

conspicuously and annotated on the ship's operating area diagram (a document that provides

visual references to the helicopter pilot and supplements other information provided by the ship prior to commencing operations - see Appendix F).

In addition, a "manoeuvring zone" should be established, where possible, on the main deck of the

ship. The manoeuvring zone, intended to provide the helicopter with an additional degree of

protection to account for rotor overhang beyond the clear zone, should extend beyond the clear zone by a minimum of 0.25 D, at any point. The manoeuvring zone may only contain obstacles whose

presence is essential for the safe operation of the helicopter, up to a maximum height of 25 cm.

In order to improve operational safety, where the operating area is coincident with the ship's side,

the clear zone should extend to a distance of 1.5 D at the ship's side while the manoeuvring zone

should extend to a distance of 2 D measured at the ship's side. Within this manoeuvring zone, the only obstacles present should be those essential for the safe operation of the helicopter, with a maximum height of 25 cm (where there are immoveable fixed objects such as tank cleaning lines

they should be marked conspicuously and annotated on the ship's operating area diagram). Any railing located on the ship's side should be removed or collapsed along the entire length of the

manoeuvring zone at the ship's side (i.e. over a distance of at least 2 D). The general arrangements and markings for a non purpose built landing area on a ship's side are shown in Figure 4.1, while

the markings themselves are described more fully in Section 4.3.2.

4.1.2.2 Amidships Centreline Landing Area (Purpose Built and Non Purpose Built)

For some vessels, where it is not possible to accommodate the ship's side arrangement, it may only be possible to provide a landing area located in an amidships position, usually on or near to the

centreline of the ship. Where this is the case, the landing area should consist of a clear zone

capable of containing a circle with a minimum diameter of 1 x D. No objects should be located

within the clear zone except aids essential for the safe operation of the helicopter, and then only

up to a maximum height of 2.5 cm. Such objects should only be present if they do not represent a

hazard to the helicopter (where, for a non purpose built landing area, there are immoveable fixed

objects located in the clear zone such as a "Butterworth lid", these should be marked

conspicuously and annotated on the ship's operating area diagram). Forward and aft on the

centreline of the landing area should be two symmetrically located 150 degree limited obstacle sectors with apexes on the circumference of the D reference circle (shown as Reference Points on Figure 4.2). Within the area bounded by these two sectors, containing the airspace used by

helicopters during the final stages of approach and/or departure and overshoot, and around the

perimeter of the landing area D, there should be no obstructions above the level of the landing

area except obstacles whose presence is essential for the safe operation of the helicopter, and then only up to a maximum height of 25 cm. To provide protection forward and aft from obstructions

adjacent to the landing area, an obstacle protection surface should extend both fore and aft of the landing area to a distance of 1 x D on a 1:5 gradient. The general arrangement and markings for

an amidships centreline landing area are shown below in Figures 4.2 and 4.3 respectively. The markings are described more fully in Section 4.3.3.

Note: Where the requirements for the limited obstacle sector and obstacle free sector

cannot be fully met - i.e. the 1:5 gradient is infringed or the "funnel of approach" is

compromised due to the presence of obstacles greater than 25 cm above the level of the

landing area, any infringements should be conspicuously marked and annotated on the

ship's operating area diagram and assessed by the helicopter operator. The helicopter

operator may need to impose appropriate restrictions and/or limitations to ensure that

flight safety is not compromised. Where the nature of the infringement is significant, the

use of the landing area may be severely limited or prohibited altogether and winching

may be the only possibility (see Section 4.1.3).

4.1.3 Location and Size of Operating Area – Winching

Where it is impractical to provide a landing area for helicopters as described in Section 4.1.2 above, it may be possible to provide an operating area capable of supporting winching operations only. A winching area should consist of a clear zone and a manoeuvring zone. The clear zone should be at least 5 metres in diameter and should have a surface capable of accommodating personnel and/or stores during winching operations. In addition, the clear zone should be obstruction free. The

manoeuvring zone, divided into an inner and outer portion, should extend beyond the clear zone,

with a minimum overall diameter of 2 D. A portion of the manoeuvring zone may be located

beyond the ship's side. Within the inner portion of the manoeuvring zone, extending to an overall

diameter of 1.5 D, obstructions may be permitted up to an overall height above the level of the clear zone of 3 metres. Within the outer portion of the manoeuvring zone, obstructions may be

permitted up to an overall height above the level of the clear zone of 6 metres. All obstructions

should be clearly marked (see paragraph 4.5 (i)). The general arrangement for a winching area is shown in Figure 4.4, and further advice on positioning a winching area is provided in Section 4.4.1. The markings for a winching area are described in Section 4.4.3.

4.1.4 Poop Deck Platforms

Poop decks are generally subject to adverse aerodynamic effects and are susceptible to a greater influence from wave motions. A poop deck arrangement is therefore not recommended unless all

other options have been exhausted.

Where a poop deck arrangement is specified, potential problems may be eased by adopting good

design practices (see Sections 4.2.2 and 4.2.3). It may also help to manoeuvre the ship for helicopter operations so that the wind is within 35 degrees of the beam, preferably on the port side.

4.1.5 Structural Considerations

(Purpose Built and Non Purpose Built Landing Areas)

Where a purpose built structure is provided, the structural features of a purpose built landing area should take full account of the relevant applicable codes, whether from the ICAO Heliport Manual

or IMO, ISO or CAP 437 requirements.

In the case of a non purpose built landing area, it must be established before marking that the

selected area can withstand the dynamic loads of the types of helicopter for which it is intended. 4.2 ENVIRONMENTAL EFFECTS

4.2.1 General Considerations

When considering the location of a landing area or a winching area, due account should be taken

of the potential effects on helicopter operations of both aerodynamic factors (see Section 4.2.2) and wave motion (see Section 4.2.3). It is unlikely that a location can be found that will be free of

the influence of any aerodynamic and wave motion effects and in reality the objective should be to select an appropriate area that, as far as possible, minimises these effects. The principles and good practice in the following paragraphs will assist in this regard, always bearing in mind the need for

clear access to the operating area and exit from it, preferably to the ship's side.

Note: For further information on relevant ship design considerations, readers are referred to UK Civil Aviation Authority (CAA) Paper 2008/03 Helideck Design Considerations -

Environmental Effects, available from the Publications section of the website at

https://www.360docs.net/doc/c314657416.html,

4.2.2 Aerodynamic Effects

There are three principal aerodynamic effects to be considered:

a. The flow of air around the hull, which has the potential to create areas of distorted and

disturbed airflow.

b. The flow of air around large items of the ship's superstructure, such as the accommodation

block, which can create turbulence in their wake.

c. Hot gas flows emanating from funnel or exhaust outlets, which can create turbulence and

have thermal effects.

The impact of such turbulence and thermal effects can be reduced by a number of design

considerations. For example:

a. In the case of a landing area located above the ship's structure, an air gap separating the

landing area from the structure below should be provided to promote beneficial wind flow

over the landing area.

b. The layout of the ship will usually include a number of tall, solid structures that rise above the level of the operating area. These structures can generate significant wake downwind of the source. The operating area should therefore ideally be located upwind of significant sources of turbulence, and any obstructions that have to be located upwind of the operating area should be as far away from it as possible.

c. Increases in ambient air temperature are a potential hazard to the performance capability of

helicopters and so the aim should be to minimise the occurrence of temperature changes over the operating area. This can be achieved by ensuring that, wherever possible the operating

area is maintained upwind of significant thermal sources. Where significant thermal sources

such as engine exhausts are located upwind of the operating area, they should be as far away as possible from the operating area and the helicopter flight path.

d. Cold gas emissions, even in small concentrations, can have an adverse effect on helicopter

engine performance and, where cold gas release points are present on a ship, they should be as remote as possible from the operating area and away from the helicopter flight path.

4.2.3 Wave Motion Effects

The dynamic motions on ships caused by ocean waves - pitch and sway, roll and surge, and heave and yaw - are a potential hazard to helicopter operations. Consideration should therefore be given to establishing motion limits acceptable for executing a safe landing or winching operation. These

limits will depend on the following:

●The wave conditions and relative heading of the ship

●The size of the ship

●The motion characteristics of the ship

●Whether the ship is moored or underway

●Whether operations occur by day or night (see Section 4.6).

The principal factors in establishing motion limits for a safe helicopter landing are the vertical

motions of the ship (i.e. rate of heave) in combination with its pitch and roll. The heave motions at the landing area depend largely on the location of the landing area and how the vessel's heave,

roll and pitch motions combine at this location. The suitability of the landing area will therefore be influenced by its location on the ship both longitudinally and transversely. The pitching of a ship is such that the vertical (heave) motion experienced at the landing area will generally be greatest if

the landing area is located on the bow or stern of the ship, and least for a landing area located

amidships. Bow located landing areas can also be particularly vulnerable to damage from heavy seas unless mounted high above deck level. Landing areas located on or over a ship's side may

experience large heave motions due to vessel roll, which will be more pronounced the further the landing area is cantilevered off the ship's side. Landing or winching areas located on the bow or

stern of the ship often present special difficulties for visual positioning especially during night time

operations (see also paragraph 4.5 (h) regarding visual estimates).

Motion monitoring equipment is available that is compatible with the requirements of civil aviation authorities and will detect, monitor, display and transmit motions experienced at the ship's helicopter operating area including heave, roll and pitch. It is strongly recommended that serious consideration is given to the fitting of such equipment, which by an automated means can also record and process climatic information (see paragraph 4.5 (g)) in order that objective data is available to support and inform operational decision making. Some authorities may also require systems for collection, retention and standard reporting of meteorological information by trained meteorological observers.

4.3 DETAILS OF LANDING AREA

4.3.1 General Guidance on Markings

Sections 4.3.2 and 4.3.3 provide guidance on the markings required for a helicopter landing area on the ship's side and amidships respectively. The recommended colours of the markings reflect

current international standards and best practice. However, as the colour of the main deck may

vary from ship to ship, there is some discretion in the selection of deck paint schemes, the

objective always being to ensure that the markings are conspicuous against the surface of the ship and the operating background.

Note: Non-slip paint should be used for all markings.

4.3.2 Markings for a Landing Area Located at the Ship's Side

This section provides guidance on the markings applicable to a helicopter landing area on the

ship's side, and should be read in conjunction with Section 4.1.2.1 and Figure 4.1.

A Touchdown/Positioning Marking (TD/PM) circle, denoting the touchdown point for the

helicopter, should be located centrally within the clear zone. The diameter of the clear zone should be 1 x D (D being the extent of the available operating area), while the inner diameter of the

TD/PM circle should be 0.5 D. The thickness of the TD/PM circle should be at least 0.5 m in width and painted yellow. The area enclosed by the TD/PM circle should be painted in a contrasting

colour, preferably dark green. A white "H" should be painted in the centre of the circle, with the

3 m wide, the width of the marking itself being 0.75 m.

The boundary of the clear zone, capable of enclosing a circle with a minimum diameter of 1 x D

and extending to a total distance of 1.5 D at the ship's side, should be painted with a continuous

0.3 m wide yellow line. The actual D value, expressed in metres rounded down to the nearest

whole number should also be marked in three locations around the perimeter of the clear zone in a contrasting colour, preferably white. The height of the numbers so marked should be 0.6 m, i.e.

twice the width of the line itself.

The boundary of the manoeuvring zone, located beyond the clear zone, and extending to a total distance of 2 D at the ship's side, should be marked with a 0.3 m wide broken yellow line with a

mark to space ratio of approximately 4:1. Where practical, the name of the ship should be painted in a contrasting colour (preferably white) on the inboard side of the manoeuvring zone in

(minimum) 1.2 m high characters.

Some additional considerations are found in Section 4.5.

4.3.3 Markings for Amidships Centreline Landing Area with or

without Restricted Access from the Ship's Side

This section provides guidance on the markings applicable to an amidships centreline landing area, and should be read in conjunction with Section 4.1.2.2 and Figures 4.2 and 4.3.

The landing area should be painted in a colour, preferably dark green, that contrasts clearly with the colour of the ship's deck. The perimeter of the landing area should be clearly marked with a

0.3 m wide continuous white line.

The D value of the landing area, expressed in metres rounded down to the nearest whole number, should be marked in port and starboard locations within the perimeter line in a contrasting colour

(preferably white), the characters themselves having a height of 0.6 m.

A Touchdown/Positioning Marking (TD/PM) circle, with a thickness of 1.0 m painted yellow and

with an inner diameter of 0.5 D, should be centrally located within the landing area. A white "H"

should be painted in the centre of the circle with the cross bar of the "H" running parallel to the

centreline of the ship. The dimensions of the "H" marking should be 4 m high x 3 m wide, the width of the marking itself being 0.75 m.

Where practical, the name of the ship should be painted in a contrasting colour (preferably white) within the landing area, aligned across the centreline (see Figure 4.3). The minimum height of the painted characters should be 1.2 m.

Some additional considerations for helicopter operating areas are found in Section 4.5.

4.4 DETAILS OF WINCHING AREA

4.4.1 Positioning a Winching Area

With the increasing use of helicopters for routine operations to ships, it is strongly recommended that, where it is impractical to provide a designated landing area, a winching area is provided over which the helicopter can hover safely while winching personnel or stores to or from the ship. The

the ship. The winching area should be located so as to minimise the aerodynamic and wave motion effects described in Sections 4.2.2 and 4.2.3. Generally, it is not recommended to locate the

winching area near the bow of the ship. In addition, it should not be located on the bridge wing in the absence of a thorough risk assessment acceptable to the ship's master and the helicopter

operator (see Section 4.4.2). The winching area should, if possible, be clear of accommodation spaces and provide adequate deck area adjacent to the manoeuvring zone where personnel can muster, and provide for safe access to the area from different directions. In selecting a winching

area, the desirability of keeping the winching height to a minimum should also be borne in mind.

To reduce the risk of the winching hook and cable becoming fouled, all guard rails, awnings,

stanchions, antennae and other obstructions in the vicinity of the manoeuvring zone should, as far as possible, be removed or retracted (see paragraph 4.5 (i) for marking of obstructions, paragraph

4.6 (d) for night operations and Figure 4.5 for obstruction lighting).

4.4.2 Winching Area on the Bridge Wing

The bridge wing will never be the ideal location for a winching area. However, there may be

circumstances where there is no practical alternative to use of the bridge wing, and in such cases a thorough risk assessment of the operation must be conducted. Only if the results are acceptable to, and approved by, both the ship's master and the helicopter operator should winching to the

ship's bridge wing be permitted.

4.4.2.1 Risk Assessment

Guidance on conducting a bridge wing risk assessment has been developed by a working group of marine and aviation experts established by ICS. The resulting document, "Bridge Wing Operations for Marine Pilot Transfer - A Risk Assessment", has been included at Appendix H. Further

information regarding marine pilot transfer may be found in Appendix E.

The guidance in Appendix H contains a risk assessment for the transfer, by helicopter hoist, of marine pilots to the bridge wing (BW) of ships under conditions where the size of the operational site precludes the application of the advice in this ICS Guide and the ICAO standards. The

assessment applies both to the helicopter and ship elements of BW operations. It represents a

generic risk assessment of BW operations and does not make any assumptions about any specific national operational requirements, helicopter operator, type of helicopter, shipping line or ship.

Threats and controls are discussed in the general text but are considered in greater detail in the

Model Risk Assessment Matrix of Annex 1 of Appendix H.

BW operations can be conducted safely provided the controls, in the form of equipment, procedures and conditions, are applied as recommended. The risk assessment guidance document does not remove the necessity for individual risk assessments by ships and helicopter operators to ascertain whether such operations can meet the standard intended by their Safety Management Systems.

Area

Winching

a

4.4.3 Marking

This section provides guidance on the markings applicable to winching areas, and should be read in conjunction with Section 4.1.3 and Figure 4.4.

The clear zone of the winching area, a central circle with a minimum diameter of 5 m, should be

painted in a conspicuous colour, preferably yellow, to contrast with the surrounding paintwork of

the ship. The perimeter of the outer portion of the manoeuvring zone should be marked with a

conspicuous broken yellow line 0.3 m in width, the ratio of the solid line to spaces being

Within the inner portion of the manoeuvring zone, based on a circle of diameter 1.5 D but outside the clear zone, should be painted the words "WINCH ONLY" in suitably large and conspicuous

lettering (ideally 2 m - 5 m white characters). The inner portion of the manoeuvring zone may be indicated by painting a thin white line no more than 0.1 m wide.

Note: Markings outside the clear zone could be obscured by temporary obstacles which

should not exceed the height limits of Section 4.1.3 and Figure 4.4.

Some additional considerations are found in Section 4.5.

4.5 ADDITIONAL CONSIDERATIONS FOR

HELICOPTER OPERATING AREAS

In addition to the marking arrangements described in Sections 4.3 and 4.4, the ship operator

should ensure that:

a. Provision is made to keep the landing or winching area free of contaminants, including

surface water.

b. An overall coating of a non-slip material is applied over the whole of the marked area for the

benefit of helicopters and personnel.

c. Where appropriate, safety nets for personnel protection are installed around the landing area.

The outboard edge of the safety netting should not rise above the level of the landing area.

d. If it is anticipated that the helicopter may shut down its engines, flush fitting or removable

semi-recessed tie-down points should be considered, adequate to secure the largest helicopter for which the landing area is designed.

e. If possible, a minimum of two access/egress routes to and from the landing area are available,

to ensure that, in the event of an incident on the landing area, helicopter passengers and crew can escape upwind of the incident.

f. Any handrails exceeding the height limitations set out in Section 4.1.2 are made retractable,

collapsible or removable and do not impede access/egress routes. Such handrails should be

painted in a contrasting colour scheme and procedures should be in place to retract, collapse or remove them prior to the arrival of the helicopter.

g. The ship has a means of ascertaining, recording and reporting wind speed and direction, air

temperature and pressure settings used by pilots, visibility, cloud base, present weather and

sea state (see also Section 3.7).

h. The ship has a means of obtaining accurate pitch, roll and heave measurements at the landing area. It is strongly recommended that the ship is equipped with motion sensing systems,

which will produce accurate pitch, roll and heave information at the landing area (see also

Section 4.2.3). The use of visual estimates is not recommended. (See also Section 3.7.)

i. Obstructions close to or within the operating area, which may present a hazard to helicopter

operations, need to be readily visible from the air and should be highlighted. Painting of

obstructions should follow the scheme advised in Appendix F, Sections 4, 5 or 6 as appropriate.

4.6 NIGHT OPERATIONS: LANDING AND WINCHING

AREA LIGHTING

The following points should be taken into account for night operations:

a. The landing or winching area should be adequately lit for night operations. This can be

achieved either by the use of flood lighting or by other appropriate lighting methods1.

Note: Unless adequate lighting is provided, landing/winching operations should be

confined to daylight only.

b. A wind direction pennant should be provided to indicate the wind conditions at the operating area. The pennant should be illuminated for night operations. Some vessels may benefit from a second device to indicate when the wind over the operating area differs from that generally over the ship.

c. The use of flash photography should be avoided during the landing or take off of helicopters and during winching operations to avoid distracting the flight crew.

d. The ship's master should ensure that floodlights are arranged to illuminate the whole of the

structure they are intended for, and are angled and shielded (as necessary) to ensure that they do not dazzle the pilot on his approach to or take off from the operating area. Figure 4.5 shows an example of an overall lighting scheme required for night helicopter operations.

ICS-无线数字直放站

ICS-无线数字直放站 摘要:ICS直放站采用了软件无线电及数字信号处理技术,实现有一定的技术门槛。ICS技术主要采用干扰自适应消除技术来达到消除干扰的目的。自适应滤波能有效地在未知环境中跟踪时变的输入信号,使输出信号达到最优。 关键词:ICS 消除干扰覆盖 Abstract: ICS repeater adopts the software radio and digital signal processing technology to achieve a certain technical threshold. And ICS technology maily adoptsinterfere technology to eliminate the interference. Adaptive filter can be effectively track time-varying input signal in an unknown environment to make output signal optimal. Key words: ICS; interference elimination; coverage 概述 随着我国移动通信事业的飞速发展,移动通信用户量正不断地增加,以至蜂窝规划越来越小,基站位置越来越低;另一方面,随着城市建设的高层化,高层建筑正不断涌现,由于无线传播的阴影效应,在这些高层建筑的背后或中间常形成移动通信信号的盲区。另外,蜂窝移动通信基站在建造过程中,由于考虑到邻近小区的干扰问题,其天线的辐射场方向图主瓣有较大的下倾角,以至高层建筑中上部一般不能有效接收到信号。此外,由于建筑物等对电磁波的屏蔽效应,使得隧道、地铁、地下商城、娱乐城、停车场以及酒店、写字楼等一些封闭的大型建筑物内也无法正常接收移动通信信号。因而各移动运营商将工作重点逐步的由网络建设转移到对网络的优化。无线直放站以其低成本,适应能力强、产品多样化,成为了网络优化产品中重要的一员。 直放站是一种用于弥补移动网络中基站覆盖不足,扩大基站覆盖范围,填充覆盖盲区的一种极其有效的设备。为了降低覆盖系统成本,最好的方法是建设直放站系统。严格来讲,直放站系统造价要比基站低得多,因此选用直放站是移动通信建设中比较好的解决方案。但是由于常规无线同频直放站由于隔离度有限,其施主天线从空中接收的信号中,将不可避免的包含一些重发天线发出的覆盖信号又通过各种途径反馈回来形成同频干扰信号,这些信号对直放站造成干扰,影响其输出波形质量,甚至容易引起直放站自激,由于这些干扰信号是直放站自身的产物,其频率就是直放站的工作频率,因而这种干扰问题无法通过常规的无源射频滤波器技术手段在频域上解决。因此产生了一种新的无线直放站—ICS。 ICS技术 ICS的干扰主要是指从直放站的施主天线引入的非基站覆盖信号,包括来自直放站重发天线的反馈干扰信号以及空间多径反射的干扰信号。施主天线接收到的信号包括基站无线覆盖信号,重发天线反馈信号,建筑物、树木、车辆等反射

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版权声明 武汉虹信通信技术有限责任公司对本手册保留一切权利。 本手册受到著作权法的保护,未经武汉虹信通信技术有限责任公司的书面许可,任何单位和个人不得以任何方式对本手册的全部或任何部分(包括电子版本)进行复制、影印、删减、编译为机读格式。 版权所有,侵权必究。

说明 本手册介绍了武汉邮电科学研究院(WRI)武汉虹信通信技术有限责任公司生产的GZFT800-IIIA和GZFT800-IIIB直放机的安装、使用和维护方法。 使用GZFT800-IIIA和GZFT800-IIIB直放机设备的用户,在安装、使用该设备之前,请认真阅读本手册。 我们已经对本手册进行了严格仔细的校对,但我们不能保证本手册完全没有错误和疏漏。武汉虹信通信技术有限责任公司有对本手册的内容随时进行改进或修改的权利,若有更改,恕不另外通知。 欢迎对本手册提出修改意见。 本手册适用于数字集群移动通信系统 下行工作频段:851MHz~866MHz。 上行工作频段:806MHz~821MHz。

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