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　　马自达3两厢：综合油耗6.8-7.9L
两厢油耗一览表
　　进口马自达3采用马自达家族近来流行的设计风格，夸张的大嘴配合两旁雾灯的装饰框，时尚之余也充满着大气之风。内饰设计流露出更多的运动感，全黑色的真皮内饰酷感十足。新马自达3两厢动力系统没有变化，仍然搭载老款的2.0升，不过经过重新，最大功率108，最大182N.m。
　　新一代进口3两厢配备了DSC（动态稳定控制系统），不过该配置仅在2.0L的两款车型上是标配，1.6L车型并无此配置。此外，6个安全气囊、3.5吋多功能信息显示屏、雨量感应式雨刷、自动头灯、双区独立控制自动、运动型真皮座椅等也是2.0L车型的标准配置。
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综合热门车系Raytheon AIM-9 Sidewinder
Copyright &
Raytheon (Philco/General Electric) AAM-N-7/GAR-8/AIM-9 Sidewinder
The AIM-9 Sidewinder is the world's most successful short-range air-to-air missile, and will remain the U.S.
military's main "dogfight" AAM for the foreseeable future.
Development of Sidewinder began in 1950 at the NOTS (Naval Ordnance Test Station) - later renamed as NWC (Naval
Weapons Center) - at China Lake. The idea was to create a very simple heat-seeking air-to-air missile by equipping
a 12.7 cm (5 in) air-to-air rocket with a lead sulphide (PbS) photo cell in a hemispherical glass nose to detect IR radiation.
Another simple, yet effective, idea was the use of "Rollerons" (sliptream-driven wheels at the fin trailing edges acting as
stabilizing gyros) as roll-stabilizing devices. The first test missiles were fired in 1951, and on 11 September 1953, the
first air-to-air hit on a drone was scored. In the same year, the prototype missile received the offical designation XAAM-N-7.
General Electric began low-rate production in 1955, and in May 1956, the AAM-N-7 Sidewinder I entered U.S. Navy
service. Only 240 Sidewinder I missiles were built, and full-rate production missiles (built by Ford Aerospace (Philco) and
General Electric) were known as AAM-N-7 Sidewinder IA. I have found no evidence that the AAM-N-7 designations ever used suffix
letters (like AAM-N-7a, etc.). For ease of reference, I will use the post-1963 designations of AIM-9A (Sidewinder I)
and AIM-9B (Sidewinder IA) throughout this text, even when referring to pre-1963 events.
The AIM-9A/B used a 4.5 kg (10 lb) blast-fragmentation warhead. This was triggered by an IR proximity or
contact fuze, and had an effective kill radius of about 9 m (30 ft). The uncooled PbS seeker of these early missiles had a 4&
angle of view and a tracking rate of 11&/s, and the missile itself could turn at 12G. Propulsion was provided by a Thiokol
MK 17 solid-fuel rocket motor (17.8 kN (4000 lb) thrust for 2.2 s), which could propel the missile to a speed of Mach 1.7 above launch
speed. Because of the limitations of the seeker, the AIM-9A/B could only be used for tail-on engagements of
non-manoeuvering(!) targets at ranges between 900 m (3000 ft) and 4.8 km (2.6 nm). The missile was also very susceptible to other
heat sources (sun, ground reflections).
Because of the usual inter-service rivalry, the USAF did not adopt the Sidewinder, until a "fly-off" against the
in June 1955 showed the superiority of the Sidewinder.
The USAF subsequently procured the AIM-9B under the designation GAR-8. More than 80000 AIM-9B missiles were produced until 1962.
On 24 September 1958, the Sidewinder achieved the world's first successful use of air-to-air guided missiles, when
Taiwanese F-86Fs shot down Communist Chinese MiG-15s using AIM-9Bs supplied by the U.S. Navy.
Photo: via Jane's
From top: AIM-9B, AIM-9D, AIM-9C
The limited performance of the AIM-9B prompted the Navy to look for improvements. The AAM-N-7 Sidewinder IC was developed
in two version: a semi-active radar homing version (called Sidewinder IB in source [1]), designated AIM-9C in 1963,
and an IR guided version, later designated as AIM-9D. Improvements common to both IC versions include a new Hercules MK 36
solid-fuel rocket motor for significantly increased speed and 18 km (9.7 nm) range, a larger MK 48 continuous-rod warhead, and slightly
larger fins.
The SARH AIM-9C was only used with the Navy'S F8U Crusader fighters to provide these with an all-weather capability without
having to fit a Sparrow-compatible radar. However, the AIM-9C was not very successful, and only 1000 were built by Motorola
between 1965 and 1967. Many were later converted into
anti-radiation missiles.
The IR seeker of the AIM-9D (in a more pointed nose) featured a new nitrogen-cooled PbS seeker, which had field of view of
only 2.5& (reduced background noise) and a higher traking rate of 12&/s. However, only about 1000 AIM-9D missiles were
built (by Philco-Ford and Raytheon) between 1965 and 1969.
The following table summarizes the redesignations of the Sidewinder variants in June 1963:
Old Designation
New Designation
AAM-N-7 Sidewinder I
AAM-N-7 Sidewinder IAGAR-8
AAM-N-7 Sidewinder IC (SARH)
AAM-N-7 Sidewinder IC (IR)
A training version of the AIM-9D for captive flight target acquisition, which had the warhead replaced by a WDU-9/B dummy
warhead, was later designated as ATM-9D. The WDU-9/B is also used in all subsequent inert ATM/CATM/NATM-9 versions.
Early training Sidewinders for firing practice were designated GDU-1/B.
The AIM-9E was the first version specifically developed by the USAF. It was an improved AIM-9B with a new seeker
with thermoelectric (Peltier) cooling, and a higher tracking rate of 16.5&/s. The Peltier cooling method allowed unlimited
cooling time while the missile was on the launch rail. Externally, the AIM-9E differed from the AIM-9B by its longer conical nose
section. About 5000 AIM-9Bs were converted to AIM-9E. The AIM-9E-2 is a variant with a reduced-smoke motor.
The AIM-9F (also known as AIM-9B FGW.2) was a European development of the AIM-9B, of which 15000 were built by
Bodensee Ger&tetechnik (BGT) in Germany. It featured a now CO2-cooled seeker, some solid-state electronics, and a
new nose dome. This version entered service in 1969, and most European AIM-9Bs were converted to AIM-9F standard.
Another Navy variant was the AIM-9G, an improved AIM-9D. It featured SEAM (Sidewinder Expanded Acquisition Mode), which
allowed the optics either to be slewed through a search pattern, or to be slaved to the aircraft's radar to acquire a target.
2120 AIM-9G were built by Raytheon from 1970 to 1972. Equivalent to ATM-9D, there was also an ATM-9G training version of
the AIM-9G.
The Sidewinder was of course used extensively over Vietnam by both the USAF and the Navy. The Air Force scored 28
AIM-9 air-to-air kills using the AIM-9B/E versions, achieving a kill probability for this missile of about 16%. The USN's most
successful Sidewinder variants in Vietnam were the AIM-9D and -9G, which were resposible for the majority of
USN air-to-air kills in this conflict. A total of 82 air-to-air kills over Vietnam are attributed to the AIM-9.
To increase the reliability of the AIM-9G, the Navy developed the AIM-9H. The main difference to the AIM-9G were solid-state
electronics in the guidance and control system. The seeker tracking rate was also increased to 20&/s to complement the more
powerful actuators. Only a few AIM-9Hs were fired over Vietnam, but they were credited with a higher kill rate than any other AIM-9 version
in Vietnam. About 7700 AIM-9Hs were produced by Philco-Ford and Raytheon between 1972 and 1974. The ATM-9H was a training
version for captive flight target acquisition.
The USAF's AIM-9J was an improved AIM-9E. It had partial solid-state electronics, a longer-burning gas generator
(increasing flight time), and more powerful actuators which drove new square-tipped double-delta canards. The latter feature
doubled the single-plane "G"-capability of the missile. About 10000 AIM-9Js were eventually built from 1972 on, mostly by converting
existing AIM-9B/E missiles.
Photo: via
AIM-9J/N/P (exact model unknown)
The designation ZAIM-9K was allocated by the U.S. Navy to a planned upgraded AIM-9H, but development was cancelled
in favor of the joint USAF/USN AIM-9L.
In 1971, the USAF and U.S. Navy agreed to jointly develop the AIM-9L, a vastly improved Sidewinder based on the
AIM-9H. Major development goals were ALASCA (All-Aspect Capability) and effective use against violently manoeuvering and high-speed
targets at all ranges.
The AIM-9L had new long-span pointed double-delta canards, a modified MK 36 solid-fuel rocket motor (MODs 8 through
11), and a new AN/DSQ-29 solid-state guidance and control section. Additional improvements include a completely new Argon-cooled
Indium Antimonide (InSb) seeker, a DSU-15/B AOTD (Active Optical Target Detector) laser proximity fuze, and an improved
9.4 kg (20.8 lb) WDU-17/B annular blast-fragmentation warhead.
All AIM-9L features resulted in a vastly improved missile which could acquire targets at all aspects, and had a much improved tracking,
manoeuvering, terminal homing, and killing performance. Production started in 1978, and more than 16000 AIM-9Ls have been built by
Philco-Ford, Raytheon, BGT (Germany), and Mitsubishi (Japan). The AIM-9L was used very successfully by the Royal Navy in the Falklands War
during 1982.
Photo: U.S. Navy
AIM-9L/M (exact model unknown)
Training versions of the AIM-9L are the ATM-9L for firing practice, the captive (non-launching) CATM-9L,
and the non-flying DATM-9L for handling and loading practice. There is also a version designated NATM-9L,
which is equipped with special test and evaluation equipment. There is also a loading practice version of the AIM-9L known
as GDU-6/C. This may be just another (earlier) designation for the DATM-9L.
The AIM-9M is a development of the AIM-9L and replaced the latter on the production line. It features a
reduced-smoke rocket motor, an improved guidance section designated WGU-4/B, better countermeasures resistance (IRCCM -
Infrared Counter-Countermeasures), and improved overall reliability. Production began in 1982, and so far more than 7000 missiles
have been built by Raytheon in subtypes numbered AIM-9M-1 through AIM-9M-10. The principal current production versions are
the AIM-9M-8 (USN) and AIM-9M-9 (USAF). They have further improved IRCM detection circuitry, and the latest versions of the
rocket motor (MK 36 MOD 11), guidance section (WGU-4E/B), and AOTD (DSU-15B/B). The AIM-9M-10 is a slightly modified -9M-8 for
use by the F/A-18E/F Hornet. Most existing AIM-9Ms will be upgraded to -9M-8/9 standard. In Operation Desert Storm in 1991,
13 air-to-air kills were attributed to the Sidewinder, all of which were probably AIM-9M missiles.
Photo: via
There seem to be no special ATM-9M launch training and DATM-9M ground handling training versions for the AIM-9M. Probably
the equivalent -9L versions are used for these purposes. However, there is the CATM-9M captive-carry
version, which exists in many subvariants. Variants known to me are the CATM-9M-1/2/4/6/8 (for AIM-9M-1/3 training),
CATM-9M-12/14 (for AIM-9M-8/9 training), and CATM-9M-27 (for AIM-9M-10 training). The NATM-9M is a version equipped with special
test and evaluation equipment (variants include NATM-9M-1 through -4).
The AIM-9N (originally designated AIM-9J-1) is an improved AIM-9J with all three major circuit boards redesigned for
improved seeker performance. Around 7000 were built by Philco-Ford, mainly for export.
The AIM-9P is a USAF-sponsored development of AIM-9J/N, mainly intended for export to countries which can't afford, don't
need, or are not allowed to receive the AIM-9L/M. The AIM-9P-1 introduced the DSU-15/B AOTD laser proximity fuze, and the AIM-9P-2
adds a reduced-smoke rocket motor. The AIM-9P-3 has the reduced-smoke motor, a new insensitive munitions warhead, and an improved
guidance and control section. Some sources say the -9P-3 retains the original IR fuze of the AIM-9J, while others say that it also
uses the new DSU-15/B like the -9P-1. The designation AIM-9P-4 applies to variants with
an ALASCA seeker using some of the technology of the AIM-9L/M, and the AIM-9P-5 adds improved IRCCM. Externally, the AIM-9P remains
almost identical to the AIM-9J/N. More than 21000 AIM-9Ps have been built so far, many being rebuilt AIM-9B/E/J missiles. Although
originally intended for export only, many AIM-9Ps are in the USAF inventory.
The designation AIM-9Q was applied by the U.S. Navy to an AIM-9M development with an upgraded guidance and control section.
I have no further information about this version, and it was probably either cancelled or redesignated as an AIM-9M subvariant.
In 1986, development of the AIM-9R began. It was derived from the AIM-9M and equipped with a completely new
WGU-19/B IIR (Imaging Infrared) seeker, offering much improved detection and tracking performance in daylight.
The first live firing occurred in 1990, but in 1992, the planned production was cancelled due to lack of funding.
The AIM-9S is a stripped-down version of the AIM-9M without the IRCCM system. It is intended for export, and the first
customer will be Turkey.
Since the 1980s, the DOD has been searching for a new missile to replace the AIM-9 as its standard short-range "dogfight"
air-to-air missile. Original plans to procure the European
(Advanced Short-Range Air-to-Air
Missile) were dropped, and various test programs were conducted during the late 1980s/early 1990s, including Have Thrust (USAF, classified),
Top Hat (USAF/Hughes), Box Office (Loral/Raytheon) and Boa (NWC China Lake). From 1991 on, efforts to develop a Sidewinder follow-on
were generally known as "AIM-9X".
Following cancellation of the AIM-9R, development of a future dogfight missile based on the AIM-9M began in earnest.
In 1994, a Dem/Val (Demonstration/Validation) program for the AIM-9X started, with Hughes and Raytheon as
competitors, and in December 1996, Hughes was announced as winner. However, because Raytheon has since acquired the Hughes
missile division, Raytheon is now prime contractor for the AIM-9X. The new missile is also officially designated as AIM-9X,
so that suffixes -9T/U/V/W are all skipped. Test firings of the AIM-9X began in 1998, and in June 1999, the
first guided live firing succeeded to hit a QF-4 target drone. Low-rate initial production was authorized in September 2000,
and the first production AIM-9X reached the USAF and USN evaluation units in summer 2002. Initial operational
capability with the U.S. Air Force was officially achieved in November 2003, and in May 2004 full-rate production
of the missile was approved. By mid-2008, about 3000 AIM-9X missiles had been delivered.
Image: Raytheon
The AIM-9X retains the MK 36 motor and the WDU-17/B warhead of the AIM-9M. The airframe is new, however, and has much
smaller fins and canards for lower drag and higher flight performance. The guidance section is completely new, and features
an IIR (Imaging Infrared) seeker. The new WPU-17/B propulsion section has a jet-vane steering system for significantly enhanced
agility. The missile is compact enough to fit into the internal weapons bays of stealthy fighters like the F/A-22 Raptor and
the F-35 Joint Strike Fighter, but can also be used on existing AIM-9 launchers (like the LAU-7/A series, and the LAU-127/A, -128/A and
-129/A series of Common Rail Launchers). The AIM-9X is also fully compatible with the new JHMCS (Joint Helmet-Mounted Cueing System) for
target acquisition. Non-tactical versions of the AIM-9X include the captive (non-launching) CATM-9X,
the non-flying DATM-9X for handling and loading practice, and the NATM-9X, which is equipped with special test and
evaluation telemetry equipment.
Until 2001, more than 150000 AIM-9 Sidewinder missiles of all variants have been built in the USA by Raytheon
(current prime contractor), Ford Aerospace (Philco), General Electric, and Motorola. Foreign built missiles raise this
number to more than 200000, and production will almost certainly continue for many years.
About 270 air-to-air kills worldwide are attributed to the AIM-9.
The graph below summarizes the development line of the AIM-9 missile family. The view of the various AIM-9 variants seems
to contain a few minor inaccuracies, but does nevertheless show the major external differences.
Drawing: Pete West/Key Publishing
AIM-9 developmentAIM-9 variants
Derivatives of the AIM-9 missile are the , the
, and the .
Specifications
Note: Data given by several sources show slight variations. Figures given below may therefore be inaccurate!
Data for AIM-9B/D/E/G/H/J/L/M/N/X:
&AIM-9BAIM-9D/G/HAIM-9E
AIM-9J/NAIM-9L/MAIM-9X
Length2.83 m (111.5 in)2.87 m (113 in)3.00 m (118 in)
3.05 m (120 in)2.85 m (112.2 in)3.02 m (118.8 in)
Finspan0.56 m (22 in)0.63 m (24.8 in)0.56 m (22 in)
0.58 m (22.8 in)0.63 m (24.8 in)0.28 m (11 in)
Diameter12.7 cm (5 in)
Weight70 kg (155 lb)AIM-9D: 88 kg (195 lb)AIM-9G: 87 kg (192 lb)AIM-9H: 84 kg (186 lb)
74 kg (164 lb)77 kg (170 lb)86 kg (191 lb)85 kg (188 lb)
SpeedMach 1.7Mach 2.5+?
Range4.8 km (2.6 nm)18 km (9.7 nm)4.2 km (2.3 nm)18 km (9.7 nm)
40+ km (22+ nm) ?
PropulsionThiokol MK 17solid-fuel rocketHercules MK 36solid-fuel rocket
Thiokol/Aerojet MK 17Hercules/Bermite MK 36
Warhead4.5 kg (10 lb)blast-fragmentation11 kg (25 lb) MK 48 continuous rod
4.5 kg (10 lb) blast-fragmentation
9.4 kg (20.8 lb) WDU-17/Bannular blast-fragmentation
Main Sources
[1] Norman Friedman: "US Naval Weapons", Conway Maritime Press, 1983
[2] Norman Friedman: "World Naval Weapons Systems, 1997/98", Naval Institute Press, 1997
[3] Bill Gunston: "The Illustrated Encyclopedia of Rockets and Missiles", Salamander Books Ltd, 1979
[4] Christopher Chant: "World Encyclopaedia of Modern Air Weapons", Patrick Stephens Ltd., 1988
[5] Hajime Ozu: "Missile 2000 - Reference Guide to World Missile Systems", Shinkigensha, 2000
[6] Malcolm English: "First Look, First Kill", article in "Air International", August 2001
[7] Carlo Kopp: , 1998
(original article published in "Australian Aviation", April 1994)
Last Updated: 9 July 2008&&&neutrophil count
的翻译结果:
查询用时：0.4秒
&在分类学科中查询
② The Spearman correlation analysis indicated that the amount of cigarette smoking was significantly associated with the total cigarettes smoked, total leukocyte count, neutrophil count, monocyte count and Gensini score (r=0.109, 0.100, 0.135, 0.139, P < 0.05-0.01).
②Spearman相关分析结果显示吸烟组患者的吸烟总数、外周血中白细胞总数、中性粒细胞计数、单核细胞计数水平与Gensini’s评分显著相关(r=0.109,0.100,0.135,0.139,P<0.05～0.01)。
(1)Aftre release of the aortic cross-clamp,neutrophil count was obviously lower in group U than that in group C(P<0.05).
结果　 (1)血中性粒细胞计数 :主动脉开放后 ,U组明显低于C组 (P <0
0 5 ) ,C组LA显著低于RA(P 0
Neutrophil count was significantly correlated with G-CSF levels(r=0.582,P<0.001)but not PDGF levels.
外周血中性粒细胞计数与G-CSF水平呈正相关(r=0.58,P<0.001),与PDGF无相关关系。
EVLWI,ELI,TNF-α and neutrophil count were also significantly lower than those of the CG group (P<0.05 ).
T组EVLWI、ELI及肺泡灌洗液中TNF—α、中性粒细胞计数均低于C组(P<0．05),而肺组织匀浆Na+-K+-ATP酶活性明显高于C组。
The median time to attain an absolute neutrophil count above 0.5×10
9 cells/L was 13.2 days (8～18). The median time to attain a platelet count above
9cells/L was 22.2 days (10～108).
中性粒细胞计数 (ANC) >0
5× 10 9L- 1 的中位时间为 13 2d(8～ 18) ,血小板 >2 0× 10 9L- 1 的中位时间为 2 2
2d(10～ 10 8)。
However, the median time to reach an absolute neutrophil count (ANC) ≥0.5 ×10
9/L was 13.3 days in group A, 17.9 days in group B on the contrary.
但中性粒细胞 (ANC)≥ 0
5× 10 9/L时间A组为13 3天 ,B组为 17 9天 ;
When the total leukocyte counts (WBC) less than 3.0×10
9/L or the absolute neutrophil count (ANC) less than 2.0×10
9/L, Lishengsu was given 75 μg/day subantaneously and the administration was stopped when the WBC counts rose up to 4.0×10
9/L or higher, or the ANC counts reached 2.5×10
9/L or more.
白细胞 <3.0× 10 9/L或中性粒细胞绝对计数 (ANC) 4 .0× 10 9/L或中性粒细胞绝对计数 >2 .5× 10 9/L时停药。
All patients were successfully engrafted. The median time of neutrophil count≥0.5×109/L was 11 days（range 10~13）and platelet count≥20×109/L was 15 days（range 12~18）after Allo-PBSCT.
结果：34例患者均获得造血重建，中性粒细胞绝对值≥0.5×109/L的中位时间为移植后+11（+10~+13）天，血小板数≥20×109/L的中位时间为+15（+12~+18）天。
3) In smoking groups from 1 week to 2 months, the level of IL-8 was positively correlated with neutrophil count in BALF (r=-0.671, P<0.05) and negatively correlated with exhaled NO (r=0.752, P<0.05).
(3)相关分析显示:吸烟1周后NO的浓度与IL8的含量成负相关(r=-0.671,P<0.05),IL8的含量与中性粒细胞数成正相关(r=0.752,P<0.05)。
② The Spearman correlation analysis indicated that the amount of cigarette smoking was significantly associated with the total cigarettes smoked, total leukocyte count, neutrophil count, monocyte count and Gensini score (r=0.109, 0.100, 0.135, 0.139, P < 0.05-0.01).
②Spearman相关分析结果显示吸烟组患者的吸烟总数、外周血中白细胞总数、中性粒细胞计数、单核细胞计数水平与Gensini’s评分显著相关(r=0.109,0.100,0.135,0.139,P<0.05～0.01)。
3) In smoking groups from 1 week to 2 months, the level of IL-8 was positively correlated with neutrophil count in BALF (r=-0.671, P<0.05) and negatively correlated with exhaled NO (r=0.752, P<0.05).
(3)相关分析显示:吸烟1周后NO的浓度与IL8的含量成负相关(r=-0.671,P<0.05),IL8的含量与中性粒细胞数成正相关(r=0.752,P<0.05)。
The level of IL-8 in the smoking group was slgnificantly increased after smoking for 1 week, 2 week and 2 months(P<0.05 ) and had a positive correlation with the neutrophil count (r=0.732, P<0.05 ).
BALF中 IL－8含量：吸烟组在 1周、2周及 2个月显著高于对照组（P＜0．05），并与中性粒细胞数呈正相关；
Neutrophil count began to be higher than
0.5×109/L
on 21st and 17th days after BMT in the two patients.
结果　 2例患者骨髓移植后的中性粒细胞数 ( >0 .5× 10 9/L)分别在第 2 1和第 17天。
Forty-six patients received granulocyte colony-stimulating factor postallograft till neutrophil count above at least 0.5×109/L.
46例移植后白细胞降至最低时开始用GCSF5μg/(kg·d),直至中性粒细胞数(ANC)≥0.5×109/L;
Results The median follow-up period was20(5～31) all patients achieved complete engraftment. The median period to gain absolute neutrophil count>0.5×10 9 /L was15(11～20)d and that for platelet count>20×10 9 /L without transfusion was20(10～35)d.
结果 11例患者均获供髓植入 ,中性粒细胞数大于0.5×109/L中位时间15(11～20)d ,血小板数大于20×109/L中位时间20(10～35)d。
Multivariate analyses showed that leukocyte count >11
958) and neutrophil count>12.0×10
895) were the independent predictors of inhospital heart failure.
WBC计数 >11 0× 10 9/L(χ2 =4
0 0 7,P =0
0 31,OR =0
2 35 ,CI=0
95 8)以及NER绝对值 >12
0× 10 9/L(χ2 =4
6 14 ,P =0
0 32 ,OR =2
4 6 9～ 11 895 )为心衰的独立预测因素。
The lowest value of the neutrophil count and platelet count was 0.05
9/L and 7×10
9/L～8×10
9/L respectively.
血小板降到 7× 10 9/L～ 8× 10 9/L ;
The median times to achieve WBC count of 1.0×10￣9/L,neutrophil count of 0.5× 10￣9/L and unsupported platelet count of 20× 10￣9 /L were 30 d (14～58d),376(14～79 d)and 616(20 ～230d),respectively。
移植后WBC＞1．0×10￣9／L、ANC＞0．5×10￣9／L、BPC＞20×10￣9／L和胸骨髓增生活跃的中位时间分别为30，37，61和50天。
When absolute neutrophil count(ANC) fell below 0.5×10
9/L,the patients were isolated in a laminar airflow unit or strictly sterilized room,and were given granulocyte colony
stimulating factor(G
CSF) and antibiotic until white ANC rose over 2.0×10
方法　化疗后当绝对粒细胞计数 (ANC)≤ 0 .5× 10 9/L时 ,对患者采取保护性隔离 ,应用粒细胞刺激因子 (G CSF)、抗菌素等直至血象恢复至ANC≥ 2 .0× 10 9/L。
The median time to recover a neutrophil count greater than 0.5×10
9/L was 14 days and a platelet count greater than 50×10
9/L was 17 days.
粒细胞恢复到 >0 .5× 10 9/L的时间平均为 14 血小板恢复到 5 0× 10 9/L的时间平均为 17d。
查询“neutrophil count”译词为用户自定义的双语例句&&&&我想查看译文中含有：的双语例句
为了更好的帮助您理解掌握查询词或其译词在地道英语中的实际用法，我们为您准备了出自英文原文的大量英语例句，供您参考。&&&&&&&&&&&&&&&&&&&& Fourty-nine cases of neonatal sepsis due to staphylococcus albus were reported. Out of 49 cases 37 were males. The chief clinical features were poor feeding, weak crying, apathy, pallor and mild fever (59.2%). Thirty-seven of the 49 cases(75.5%) had an absolute neutrophil count over 7000/mm~3 and 17 of the 37 cases(46.9% )had both elevated white blood count and neutrophil percentage. Infection originated from omphalitis in more than half of the cases (55.1%). There were 3 cases compl... &&&&&&&&&&&&本组病例男性占75.5%,临床主要表现有吃奶少、哭声小、反应下降、面色灰白、体温异常(多呈微热,占59.2%)等。分叶核粒细胞绝对值大于7,000占75.5%,白细胞总数及分叶均升高者44.9%。脐炎为主要感染途径,占55.1%。抗生素敏感过半数的有先锋、白、新生、新、庆大霉素及多粘菌素等。凝固酶阴性抗药性大于阳性(P<0.01)。病死率为12.2%。鉴于国内尚无诊断标准,本文提出:凡具备主要临床表现及下述一项即可诊断。(1)血培养2次以上阳性;(2)血培养1次阳性,但在病灶中培养出相同菌株;(3)血培养1次阳性,但临床症状及周围血象改变明显,用敏感抗生素有效。&&&&&&&& T2 toxin is one of the most toxic member among trichotheccnes (Ts)family produced by fungi.It is responsible to intoxication found in human being and animals following ingestion of mouldy grain,and alimentary toxic aleukia (ATA)is the common but important problem in intoxication.The follows are some events in hcmotological toxicology of this toxin.Under a single dose (2.3mg/ kg ip,equal to LD30),T2 toxin decreased mice peripheral WBC count and a similar decline of circulating lymphocyte (L)also happen... &&&&&&&&&&&&T2毒素2.3 mg/kg(相当LD_(30))单次ip后测定小鼠外周血象,BMNC及骨髓CFUs、CFU—GM、CFU—E和BFU—E的改变以了解T2毒素血液毒理的特征.外周血中WBC总数明显减少,RBC和pt无变化.T2毒素虽不影响CFUs的数量,但对CFU—GM、CFU—E和BFU—E均有杀伤作用,中毒后2 h三种细胞存活率达最低值分别为正常的27％、48％和57％,恢复速度甚快,5 d内全部正常.三种细胞的T2毒素剂量活存曲线均为指数坪型.分析了各类造血干细胞对T2毒素敏感性不同的原因可能与各种细胞固有特性和细胞增殖状态有关。&&&&&&&& The study on the plasma endotoxin level and the change of leukocyte number in Wen Bing patients shows that the plasma endotoxin is positively correlated with the total leukocyte count(r=0.467)and differential neutrophil count(r=0.631). The total leukocyte and neutrophil numbers can reflect the degree of infection, and, like the plasma endotoxin, can act as an objective index for Wen Bing endotoxemia. &&&&&&&&&&&&温病患者血浆内毒素与白细胞变化的研究结果表明,血浆内毒素与白细胞总数(r=0.467)及中性粒细胞(r=0.631)呈中度正相关关系。白细胞总数及中性粒细胞是机体感染轻重的反映,与血浆内毒素一样,可作为温病毒的客观指标。&nbsp&&&&&&&&相关查询:
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