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11. position [ p zin ] n. 位置; 地點
12. accomplish [ k mpli ] vt. 完成
13. stage [ steid ] n. 級
14. turbine-air motor 空氣渦流發動機(馬達)
15. convert…into… 把…轉變(化)成…
16. energy [end i ] n. 能(量)
17. sufficient [ sfint ] a. 足夠的; 充分的
18. require [ rikwai ] v. 要求; 需要
19. ground source [ s :s ] 地面源(電源,氣源, 信號源…)
20. crossbleed [ kr sbli:d ] 交叉引氣
21. another [nð ] a. ; prep. 另一個
22. related to… [ rileitid ] 與…有關的
23. spark [ spa:k ] n. 火花
24. ignite [ ignait ] v. 點火
25. mixture [mikst ] n. 混合物
26. takeoff [ teik :f ] n. 起飛
27. landing [ lændi ] n. 著陸
28. adverse [ ædv:s ] a. 有害的; 不利的
29. weather [ weð ] n. 天氣; 氣象
30. condition [ kndin ] n. 情況; 條件
31. exciter [ iksait ] n. 勵磁機; 激勵器
32. triaxial [ traiæksil ] a. 三維的; 三線的
33. shield [ i:ld ] v. ; n. 屏蔽; 保護; 隔離
34. lead [ li:d ] n. 引線; 導線
35. inlet cowl [ kaul ] 入口整流罩
36. precooler [pri:ku:l ] 預冷器
37. limit [limit ] n. ; vt. 限制; 極限; 限定
38. temperature [temprit ] n. 溫度
39. manifold [ mænifould ] n. 總管道
40. revers [ ri v:s ] v. 相反; 倒過來; 反向
41. direction [ di rekn ] n. 方向
42. sleeve [ sli: v ] n. 套筒; 外殼
43. remote [ ri mut ] a. 遙控的
44. deploy [ dipl i ] v. 展開; 打開
45. prior to [ prai ] 在…之前
46. deployment [ dipl imnt ] n. 展開; 打開
47. blocker door [ bl k ] 阻流門
48. arrange [ reind ] v. 排列;安裝
49. is attached to [tæt ] 連接在…上
50. bolt [ bult ] n. 螺栓
51. drag link [dræg] [lik] 阻力連桿
52. fitting [fiti ] n. 裝置; 裝配部件
53. translate [ trænsleit ] v.移動; 平移
54. forcing [f :si ] n. ; a. 強迫(的)
55. cascade [ kæskeid ] n. a. 級聯(的); 葉柵
56. segment [ segmnt ] n. 部分; 段
57. form [ f :m ] v. 形成; 構成
58. parameter [ præmit ] n. 參數
59. instrument [instrumnt ] n. 儀表
60. LED = Light Emitting Diode 發光二極管
61. percent [ psent ] n. 百分比
62. EGT = Exhaust Gas Temperature 排氣溫度
63. exceed [iksi:d ] v. 超出;超限
64. redline [redlain ] n. 紅線
65. weight [ weit ] a. 重量
66. total [ tutl ] a. 總的;全體(部)的
67. consume [ k nsjum ] v. 消耗
68. sequence [si:kwns ] n. 順序;程序
69. reset [ri: set ] vt. 復位
70. vibration [ vaibrein ] n.振動
71. maximum [ mæksimm ] n. ; a. 最大(的); 最高(的)
TEXT
[1] The engine starting system provides air ,fuel, ignition and torque for rotating the
engine to an rpm at which the engine can accelerate to idle rpm. The system consists
of the starters, start valves, start bleed valves, pneumatic ducting, control and power
circuitry, start levers and start selector switches. The start valve and starter are
located on the forward side of the engine accessory gearbox, the start bleed valve is
located on the left side of the HPC case at the 11 oclock position, the start levers,
start selector switches and start valve open light are in the flight compartment.
Engine starting is accomplished by supplying air from the pneumatic system
through the start valve to the starter.
[2] The engine starter is a single-stage, axial flow, turbine-air motor, the starter
converts compressed air pressure into rotational mechanical energy sufficient to
accelerate the engine to starting speed. Pressurized air and electrical power are
required for starter operation. The engine may be started with air from the APU (we
will introduce APU in the next lesson ) ,from a ground source, or by using engine
crossbleed. Another important system related to engine operation is the ignition
system. The purpose of the ignition system is to produce a high current electrical
spark to ignite the fuel/air mixture in the engine combustion chamber during
starting and to provide continuons ignition during takeoff, landing and operation in
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航空工程英語基礎(中英文對照)(22)